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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GLBA2012112600114Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE VERTICAL STABILIZER RT FWD SPAR CAP ANGLE CRACKED BY TOP RIVET AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO12-1900-55-060. MAJOR REPAIR.SDR ASOA20121107120VDoubler · crackedDURING C-CHECK THE VERTICAL STAB DOUBLER BETWEEN FRAMES 80-81 AND STRINGERS 1L-1R WAS FOUND TO BE CRACKED. MX R & R THE DOUBLER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2012FA0000772Fitting · crackedDURING A SCHEDULED PHASE 5 INSPECTION, FOUND FITTING CRACKED IN THE VERTICAL STAB. THE CRACK WAS FOUND USING EDDY CURRENT INSPECTION METHODS.SDR DALA1250160942Fastener · looseLOOSE FASTENERS ON VERTICAL STAB L/E AT THE SPLICE STA ZFS=52.2, 2 ROWS OF FASTENERS ABOVE AND BELOW OF SPLICE REF OP 0501, EA 09-470871-12AD.SDR ASAA2012100593058Retainer · crackedRT VERTICAL STAB ACCESS PANEL 9502 HAS CRACKED RETAINER. R & R RETAINER IAW SRM 51-40-02.SDR IPXA2M76144Fitting · crackedINSPECTION TYPE: 4C, VERTICAL STABILIZER AFT SPAR NR4 RT BANJO FITTING AFT SIDE FLANGE CRACKED. REPAIRED NR 4 RT BANJO FITTING AFT SIDE FLANGE REF STASA EA 011-5530- 01-A4354 REV I/R, EO MD11-5530-49025-A, SRM 55-30-02, REPAIR 5, FIG 202, 8100-9, SR 1- 23SDR 2012FA0000773Fitting · crackedDURING A SCHEDULED PHASE 5 INSPECTION, FOUND FITTING IN VERTICAL STAB TO BE CRACKED. OPENSDR FDEA201209063242Door · crackedSTABILIZER BAY DOOR 313AL CRACKED REPAIR IAW EA6-5241-157940 AND SRM 51-71-11, PARA 4D.SDR DALA1247389215Skate Angle · crackedLEFT SKATE ANGLE CRACKED, INBD FASTENER ROW 15 INCHES FROM AFT END. REPAIRED PER ERA 506579-14 REV ORIG.SDR IPXA2M75442Fitting · damagedINSPECTION TYPE: 4C, FOUND LOOSE FASTENERS ON LT NR 4 BANJO FITTING TO PYLON CARRY-THRU CAP. REPAIRED 6EA VERTICAL STAB AFT SPAR LT NR 4 BANJO FITTING FASTENER HOLES COMMON TO THE NR 2 PYLON CARRY-THRU CAP ATTACHMENT REF EO MD11-553 0-46641-A APPROX B AND D.SDR IPXA2M75441Fitting · damagedINSPECTION TYPE: 4C, FOUND LOOSE FASTENERS ON NR 4 BANJO FITTING TO PYLON CARRY THRU CAP. REPAIRED VERTICAL STAB AFT SPAR RT NR 4 BANJO FITTING FASTENER HOLES COMMON TO THE NR 2 PYLON CARRY THRU CAP ATTACHMENT REF EO MD11-5530-46641-A APPX C AND E.SDR USAA2012091700049Hinge Fitting · excess play2S CHECK - VERTICAL STABILIZER HINGE FITTING NR 4 AT STATION 263 HAS EXCESSIVE PLAY. REMOVED AND REPLACED HINGE FITTING IAW A319 SRM 51-72-11 AND A319 AMM 55-36-41-000-001-A.SDR USAA2012091700052Hinge Fitting · excess play2S CHECK - VERTICAL STABILIZER HINGE FITTING NR 7 AT STATION 561 HAS EXCESSIVE PLAY. REMOVED AND REPLACED HINGE FITTING IAW A319 SRM 51-72-11 AND AMM 55-36-41-0001-A.SDR IPXA12M75159Bolt · shearedINSPECTION TYPE: 4C, VERTICAL STAB LT SIDE NR 4 BANJO CARRY-THROUGH FITTING 6 SHEARED BOLTS. REPAIRED VERT STAB LT SIDE NR 4 BANJO FITTING BOLTS IAW EO MD11-5530-46641-A.SDR IPXA2M75042Intercostal · crackedINSPECTION TYPE: 4C, INTERCOSTAL CRACKED IN VERT STAB RT SIDE AT STA YTN121. REPAIRED INTERCOSTAL IN VERTICAL STAB RT SIDE IAW STASA EA 011-5530-01-A4160 REV IR, EO 5530-48139-A, & SRM 55-30-02 REPAIR 2, FIG 201.SDR IPXA2M75038Intercostal · crackedINSPECTION TYPE: 4C, INTERCOSTAL CRACKED AT STA YTN121.865 LT SIDE OF VERTICAL STAB INSIDE PANEL 363PL. REPAIRED INTERCOSTAL IAW STASA EA 011-5530-01-A4160 REV.IR, EO 5530-48139-A, AND SRM 55-30-02, FIG 201, REPAIR 2SDR IPXA2M75025Intercostal · crackedINSPECTION TYPE: 4C, VERTICAL STAB, PYLON CARRY-THRU REAR CENTER SPAR TO REAR SPAR LOWER LT PANEL INSTALLATION-INTERCOSTAL CRACKED AT FWD EDGE. REPAIRED VERT STAB CARRY-THRU REAR CENTER SPAR TO REAR SPAR LWR LT PANEL INSTALLATION. INTERCOSTAL FWD EDGE REF STSDR HNAA2012072000876Bolt · corrodedLOCK BOLTS ARE CORRODED INSIDE OF VERTICAL STAB, FORWARD TUNNEL, AT RIB 4. CLEANED OFF LIGHT SURFACE CORROSION ON LOCK BOLTS, INSIDE VERTICAL STAB, FORWARD TUNNEL AT RIB 4.SDR FDEA201207132562Fitting · misrepairedDURING ACCOMPLISHMENT OF VERTICAL STABILIZER NR 4 BANJO FITTING REPAIR AT RT SIDE FORWARD FLANGE LOWER FITTING EXISTING FASTENER AREA FOUND SHORT WITH 1 EA FASTENER AT REPAIR FITTING IAW REPAIR DWG: SR10550013. REPAIRED AS PER E.A. 1-5530-159861 PART 1. RESDR 2012FA0000774Channel · crackedDURING A SCHEDULED PHASE 17 INSPECTION, THERE WAS A CRACK DISCOVERED AT THE ATTACH CHANNEL, REPLACED IAW DWG 5531007.SDR DU4R2012004Angle · corrodedDURING SCHEDULED INSPECTION, FOUND VERTICAL STABILIZER RIGHT ATTACH ANGLE HAS CORROSION AT MATING SURFACE FS 1041 APPROX, ALSO AT UPPER SURFACE HSS 991.SDR USAA2012072000005Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON HINGE ARM FITTING NR 3 AT VERTICAL STAB STA 228, RIB 5. REPLACED HINGE ARM FITTING NR 3 AT VERTICAL STAB STA 228, RIB 5 IAW A320 SRM 51-72-11 & AMM 53-36-41-0401.SDR SIMA20120604006Hinge Fitting · excess playDURING MAINTENANCE CHECK, FOUND THE VERTICAL STABILIZER TO RUDDER LOWER MID HINGE FITTING BEARING HAS PLAY. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW HINGE FITTING. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA1234120935Hinge Bracket · corrodedFOUND CORROSION ON THE SURFACES AND BORES COMMON TO THE VERTICAL TO HORIZONTAL HINGE PLATES. THE PLATES ARE SUBJECT OF SB MD80-55-054 AD 99-07-14 AND EO 09-073278-12AD. SIX OF THE EIGHT HINGE PLATES WERE REPLACED. THE LT OUTBOARD PLATES WERE NOT REPLACED ATSDR MASA2012061134873Drag Angle · crackedRIGHT AND LEFT VERTICAL STABILIZER ATTACHMENT DRAG ANGLES CRACKED AT REAR SPAR DATUM 67.5 PERCENT. REPPAIRED IAW REO 690-55-31-013 REV A.SDR CA120501001Drag Angle · cracked(CAN) DURING A VISIT TO A PAINTING FACILITY, CRACKS WERE FOUND ON THE LT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE BRACKETS, FORWARD AND AFT. THE ACFT WAS FLOWN IAW GREO 690-55-31-010. REPAIR BEING ACCOMPLISHED IAW DWG 670-51-00-066.SDR DALA1233150940Plate · scratchedSCRATCHES ON INBD PLATES LOCATED ZRS=178 AND XH=5.5 AT VERTICAL STABILIZER. HOLES ON INBD PLATES WERE REAMED IAW SRM 55-02 PAR 24 B1. REPAIR BUSHINGS FABRICATED IAW SRM 55-02 PAR24C.SDR IPXA2M73436Fitting · shearedINSPECTION TYPE: 3C, VERTICAL STAB LT SIDE NR 4 BANJO FITTING CARRY-THROUGH CAP FASTENERS SHEARED. REPAIRED LT SIDE NR 4 BANJO FITTING FASTENERS IAW EO MD11-5530-46641-A APPX B AND D.SDR IPXA2M73435Fitting · shearedINSPECTION TYPE: 3C, VERTICAL STAB RT SIDE NR 4 BANJO FITTING CARRY THROUGH CAP FASTENERS SHEARED. REPAIRED RT SIDE NR 4 BANJO FITTING FASTENERS IAW EO MD11-5530-46641-A APPX C AND E.SDR FDEA201204031243Angle · crackedHFEC INSPECTED HORIZONTAL LEG BASE, FOUND TO BE CRACKED, LOCATED .5" FROM LT OTBD TO 1ST FASTENER, ON VERTICAL STABILIZER. LENGTH OF CRACK IS ABOUT .6250 INCHES LONG. REPLACED CRACKED BASE ANGLE IN REF TO W/C EO 8-5530-7-4303 C2, PART 2, STEP 5.SDR FDEA201204021221Support · chafedFOUND KNIFE EDGE CHAFING ON LOWER END OF SUPPORT ON VERTICAL STAB. R & R WITH FAIRING SUPPORT FABRICIATED IAW DWG 173N1300-3, SHT 1, REV B AND INSTALLED IAW DWG 173N1300 SHT 1, REV B. REPAIR IS CLASSIFIED AS MAJOR.SDR UALA2012032801956Nut Plate · brokenNUT PLATE FOR VERTICAL STABILIZER ACCESS PANEL 322FL IS BROKEN, LOCATED BOTTOM FRONT LEADING EDGE CORNER. REPLACED NUT PLATE AS REQUIRED.SDR ASOA201201014Drag Angle · crackedVERTICAL STAB CRACKED ON LT SIDE LOWER DRAG ANGLE. R & R DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-000-001-A01, 51-42-22-001-001-A01, AND DWG NR BA670-35002.SDR IPXA12572153Beam · corrodedINSPECTION TYPE: C, EVIDENCE OF CORROSION ON VERTICAL STAB T/E BEAM RUDDER STA 131 TO RUDDER STA 206. BLENDED AREA AND REPAIRED IAW EA 120227.SDR ASOA201200801Attach Angle · crackedVERTICAL STAB RT ATTACH ANGLE CRACKED AT AFT T/E AREA. REMOVED RT SIDE VERTICAL STAB AFT ATTACH ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. INSTALLED ANGLE IAW AMM 51-42-13-001-001-A01.SDR GLBA2012030502Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE LIGHTNING HOLE EXTENDING BACK AND TO THE LT, AT LT SIDE VERTICAL STAB AT 39.5 PERCENT CHORD AND CSS 69.184, 1.375" IN LENGTH. REPAIRED IAW EO 12-1900-55-006. MAJOR REPAIRSDR EE4Y20120302091Structure · contaminatedDURING THE INSPECTION PROCESS, FOUND THE VERTICAL STABILIZER, RUBBER PANEL HOIST POINT NR 3 LT SIDE WITH TRAPPED FLUID. HOIST POINT REQUIRED A MINOR REPAIR IAW GUIDELINES.SDR EE4Y20120302090Structure · contaminatedDURING THE INSPECTION PROCESS, FOUND THE VERTICAL STABILIZER, RUBBER PANEL HOIST POINT NR 2 LT SIDE WITH TRAPPED FLUID. HOIST POINT REQUIRED A MINOR REPAIR IAW GUIDELINES.SDR EE4Y20120302085Structure · contaminatedDURING THE INSPECTION PROCESS, FOUND THE VERTICAL STABILIZER, RUBBER PANEL HOIST POINT NR 1 RT SIDE WITH TRAPPED FLUID. HOIST POINT REQUIRED A MINOR REPAIR IAW GUIDELINES.SDR DXTR20120209001Bolt · looseFOUR VERTICAL ATTACH BOLTS ARE LOOSE AT THE VERTICAL STAB AFT SPAR ASSY TO WEB/RIB ASSY FS 588 - WL161.5. RETORQUED TO STANDARD PRACTICES.SDR USAA2012022200023Structure · crackedC3 CHECK - .4 INCH CRACK ON LEFT HORIZONTAL STABILIZER FORWARD CHORD INBOARD FLANGE AT BS 1809.5, RBL 65. REPAIRED LEFT HORIZONTAL STABILIZER FORWARD CHORD INBOARD FLANGE AT BS 1809.5, RBL 65 IAW EA 130806.SDR CA111107008Fairing · damaged(CAN) VERTICAL FIN AFT TIP FAIRING FOUND CONTACTING RUDDER TOP SURFACE DURING GROUND HANDLING AND PRE-FLIGHT INSPECTION. FAIRING REMOVED AND FOUND MOUNTING HARDWARE HOLE ABNORMALLY OVERSIZED ALLOWING FOR AIRSTREAM TO MOVE FAIRING BOTTOM T/E TO CONTACT RUDDERSDR USAA2011111600014Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 2 HINGE ARM FITTING AT VERTICAL STAB STA 1926 RIB 4. REPLACED NR 2 HINGE ARM FITTING IAW A320 SRM 51-72-11 & AMM 55-36-41.SDR USAA2011111600005Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON NR 7 HINGE ARM FITTING AT VERTICAL STAB STA 5605 RIB 11. REPLACED NR 7 HINGE ARM FITTING IAW A320 SRM 51-72-11 & AMM 55-36-41.SDR DALA1158770928Plate · corrodedDURING HMV AFTER REMOVAL REPAIR BUSHINGS ON INBD AND OUTBD PLATES OF VERTICAL STABILIZER CORROSION WAS FOUND IN BORES REF SRM 55-02 FIG 28 FOR REPAIR. REWORKED DAMAGED PLATES BORE AND INSTALLED BUSHINGS IAW ERA 497032-14 REV.SDR FDEA201110084383Web · crackedLOWER PART OF VERTICAL STABILIZER - LT REAR CENTER SPAR TO REAR SPAR LOWER WEB (INSIDE ACCESS PANEL NR363PL) FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG.201 REV 47 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 113.SDR FDEA201109264138Structure · corrodedVERT STAB INT. BS 1342 RT CORNER AT WL 259 AT LOWER WEB HAS EXFOLIATED CORROSION UNDER LEVELING COMPOUND. CUTOUT DAMAGED VERTICAL STAB LOWER CHORD, FABRICATED REPAIR PARTS & INSTALLED REPAIR AT VERTICAL STAB IAW FX WC 7-5530-7-2303 P6SDR FDEA201109224040Web · crackedLOWER PART OF VERTICAL STABILIZER, RT REAR CENTER SPAR TO REAR SPAR LOWER WEB FOUND CRACKED. CARRIED OUT REPAIR AS PER EA 1-5530-154227. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR DALA1143989017Structure · crackedA 5 INCH CRACK ON VERTICAL STAB STA 1418 FWD OF AIR SCOOP ON LEADING EDGE. FOUND DURING PSV VISIT MSP NON ROUTINE NR 68. REPLACED CLIP PER SRM 51-01. PART NUMBER 5912188U49.SDR FOTR2111712446Structure · crackedVERTICAL STAB, L/E HAS CRACKED DOUBLER TOP OF FWD SPAR CHORD CENTER, JUST AFT OF ELEVATOR CONTROL CABLE QUADRANT. REPAIRED ON FASI WO 21117, NR 12446.
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