JASC 5553
Service difficulty reports · 586
Reports filed under 5553 · Vertical Stabilizer, Attach Fittings, 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 = '5553' 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 = '5553' 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 ASOA201710143299Drag Angle · crackedLEFT VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE IAW EC/TC REO 670-55-31-018.SDR ASOA201710143298Drag Angle · crackedRIGHT VERTICAL TO FUSELAGE ATTACH DRAG ANGLE IS CRACKED. REPAIRED.SDR ASOA201710143297Drag Angle · crackedLEFT REAR VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. MAINTENANCE REPLACED CRACKED DRAG ANGLE.SDR ASOA201710143296Drag Angle · crackedRIGHT REAR VERTICAL TO FUSELAGE ATTACH DRAG ANGLE IS CRACKED. MAINTENANCE REPLACED CRACKED DRAG ANGLESDR DALA2017101207487Attach Angle · gougedDEEP GOUGE AT BOTTOM OF VERTICAL STAB LT SIDE LOWER FWD ATTACH ANGLE. REPAIRED THE ATTACH ANGLE IAW ERA 562481-14, REV 0.SDR A6WA2017101145352Attach Bracket · crackedFWD ATTACH BRACKET FOR VERTICAL STAB ACCESS PANEL 326CR IS CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-20.SDR SWIA2017100243816Drag Angle · crackedFWD AND AFT CRACKS ON THE RT SIDE VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLES CRACKED. REPAIRED THE DRAG ANGLES IAW REO.SDR SWIA2017100243815Drag Angle · crackedFWD AND AFT LT SIDE VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLES CRACKED. REPAIRED IAW REO.SDR ASOA201709023248Attach Fitting · crackedLEFT VERTICAL STAB ATTACHMENT TO FUSELAGE DOUBLER CRACKED. COMPLIED WITH REO 670-55-31-078, REV A.SDR FDEA201708172245Fitting · crackedDURING HFEC INSPECTION AT THE LT FWD FLANGE, LOCATED AT THE UPPER SECTION REAR SPAR CAP OF THE NR 4 BANJO FITTING OF THE VERTICAL STABILIZER , BS 2164. A CRACK WAS FOUND APPROXIMATELY 0.50 INCH LENGTH. REPAIRED IAW EA 1-5530-T0335146, P1. CLASSIFIED AS MAJSDR DALA2017061604851Angle · crackedCRACKED RIGHT HAND INNER DORSAL FIN JOINT ANGLE STA 1478-1468. REPLACED IAW SRM 51-30-05 AND 51-30-02.SDR WVER2017052500006Drag Angle · crackedLEFT VERTICAL STABILIZER TO FUSELAGE FWD ATTACHMENT DRAG ANGLE IS CRACKED.SDR SIMA20170521005Drag Angle · crackedLEFT VERTICAL TO FUSELAGE DRAG ANGLE CRACKED AT APPROXIMATELY FRAME 76. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.SDR ASOA201705183164Fitting · corrodedVERTICAL STAB TO HORIZONTAL STAB LT SPHERICAL BEARING HOLE CORRODED. CORROSION REMOVED IAW SRM 54-30-02, TABLE 201, REWORK 1.SDR AALA20170516007Angle · crackedCRACKED J ANGLE ON THE RIGHT FORWARD MOUNT OF THE VERTICAL STABILIZER. REMOVED AND REPLACED THE ANGLE IAW 55-30-09-3 AND SRM 51-40-02.SDR DALA2017040402830Attach Fitting · crackedRIGHT VERTICAL STABILIZER ATTACH ANGLE CRACKED. BS 1458-1486. REMOVED AND REPLACED IAW SRM 51-30-02 AND DWG 5912188, REV BD.SDR DALA2017040202673Attach Angle · crackedLEFT VERTICAL STABILIZER ATTACH ANGLE, BS 1458 - 1486 CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02, 51-30-05, AND DWG 5912188, REV BD.SDR SIMA20170208002Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED, ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.SDR SIMA20170208001Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE APPEARS TO BE CRACKED APPROX. ONE INCH IN LENGTH. REPAIRED IAW EO-CR-55MR-038.SDR V0XD20161212004Drag Angle · crackedVERTICAL STABILIZER TO FUSELAGE, LT FWD DRAG ANGLE IS CRACKED.. CUT OUT DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-31-018.SDR V0XD2016121001Drag Angle · crackedRT AFT DRAG ANGLE IS CRACKED WHERE VERTICAL STABILIZER MEETS FUSELAGE. REPAIRED RT AFT DRAG ANGLE IAW REO 670-55-31-018 REV A DATED 2016-11-10, AND REO 670-55-31-092 DATED 2016-12-06. NDT PERFORMED.SDR DALA2016101307218Lug · corrodedAFT SUPPORT RIGHT FITTING ON HORIZONTAL SUPPORT OUTBOARD LUG CORRODED. COMPLIED WITH PRI/ERA 551207-14. (LP# 270936)SDR DALA2016083106339Attach Fitting · crackedCRACKED LOWER DORSAL ATTACH FITTING AT STA Y=1494 AND LONGERON PROJECTION 3 LT IN AFT ACCESSORY COMPARTMENT. FITTING WAS REPLACED IAW DWG 9953016, REV AU AND SRM 51-30-05.SDR DALA2016081006068Attach Angle · brokenVERTICAL STABILIZER LEADING EDGE LOWER RIGHT INNER ATTACH ANGLE BROKEN. REPLACED THE ATTACH ANGLE IAW DWG 5912188.SDR DALA2016081006034Attach Angle · brokenVERTICAL STABILIZER LOWER LEFT INNER ATTACH ANGLE IS BROKEN. REPLACED IAW DWG 5912188.SDR WVER0716201600008Drag Angle · crackedLT AND RT VERTICAL STABILIZER FUSELAGE ATTACHMENT DRAG ANGLES ARE CRACKED.SDR AALA20160714008Attach Angle · crackedLEFT VERTICAL STABILIZER LOWER ATTACH ANGLE IS CRACKED AT AFT END. REMOVED AND REPLACED ANGLE IAW SRM 51-01-00 AND BOEING DRAWING 5912188.SDR V0XD20160703145Drag Angle · crackedRIGHT VERTICAL STABILIZER FORWARD DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW REO 670-55-31-018 REV.SDR JR2R06142016291Angle · crackedLEFT DORSAL FIN ANGLE CRACKED ON UPPER EDGE THROUGH RIVET HOLE. R & R LT DORSAL FIN ANGLE IAW DWG SRO9530162 AND SRM 51-30-5.SDR WVER0612201610Drag Angle · crackedLEFT FUSELAGE TO VERTICAL FWD DRAG ANGLE AT VS 67.5 PERCENT REAR SPAR DATUM CRACKED IN AFT RADIUS.SDR WVER0612201609Drag Angle · crackedRIGHT FUSELAGE TO VERTICAL FWD DRAG ANGLE AT VS67.5 PERCENT REAR SPAR DATUM CRACKED IN AFT RADIUS.SDR DALA2016052704287Attach Angle · crackedCRACKED ANGLE FOUND ON INSIDE RT OF DORSAL FIN ATTACHMENT TO FUSELAGE. FABRICATED NEW ANGLE IAW DWG 5912188.SDR P5CA2016051000101Attach Fitting · crackedUPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING RT RADIUS UPPER LOBE DOUBLER FOUND CRACK APPROXIMATELY 80MM LONGERON STABILIZER 2403-2524. RT UPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING AREA IS REPAIRED SDR WVER2016041500001Drag Angle · crackedLEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE AT 67.5 REAR SPAR DATUM IS CRACKED.SDR ASOA2016040514742Attach Angle · crackedRT VERTICAL STABILIZER TO FUSELAGE ANGLE APPEARS CRACKED. ALL STEPS OF REO 670-55-31-082 HAVE BEEN COMPLIED WITH & COMPLIED WITH ECTC REO 670-55-31-082.SDR FDEA201603311130Drag Angle · crackedLEFT VERTICAL TO EXT FUSE DRAG ANGLE HAS 2.5 IN CRACK. MARKED BELOW NR 2 BANJO FITTING. REPAIRED CRACKED ANGLE LT VERTICAL BELOW NR 2 BANJO FITTING IAW SRM 55-20-00 V I FIGURE 3.SDR FDEA201603051131Drag Angle · crackedRIGHT VERTICAL TO FUSE EXT DRAG ANGLE HAS 1 INCH CRACK. MARKED AREA BELOW NR 2 BANJO FITTING. REPAIRED IAW SRM 55-20-00 FIG 3 SHEET 1-3.SDR SWAA2016040750676Drag Link · corrodedVERTICAL STABILIZER LT AFT OTBD MOUNTING POINT, AFT DRAG LINK FITTING CORRODED PIT ON BOTTOM SURFACE. R & R DRAG LINK ASSEMBLY IAW DWG.SDR IPXA2016021599346Mount · corrodedINSPECTION TYPE: 3C, SURFACE CORROSION ON THE LOWER VERTICAL STAB UPPER MOUNTING FRAME FOR PANEL NR 361AL. REMOVED CORROSION IAW SRM 51-21-01. ORIGINAL MATERIAL THICKNESS .063 IAW DWG AJC7328, FOUND WITHIN LIMITS IAW SRM 55-00-00, PAGE 206. TREATED AND PRIMESDR DALA2015120407446Attach Angle · crackedCRACKS ON DORSAL FIN ATTACH INTERNAL ANGLES. R & R IAW SRM 51-30-05.SDR QMLA2015081215070Stud · shearedDURING TAKEOFF THE LT VERTICAL STABILIZER SEPARATED FROM THE ACFT, THE PIC WAS UNAWARE OF THE ISSUE UNTIL THE COMMUNICATIONS CENTER NOTIFIED HIM BY RADIO. NO EFFECT WAS FELT DURING THE REST OF THE FLIGHT. THE ACFT LANDED SAFELY & DURING A POST FLIGHT INSPECTSDR 2015FA0000330Attach Fitting · gougedDURING INSPECTION OF THE HORIZONTAL STABILIZER ATTACHMENT TO THE VERTICAL STABILIZER, FOUND THE 4 BARREL NUTS FOR THE FWD 4 ATTACH BOLTS WERE INSTALLED UPSIDE DOWN IN THE FITTING HOLES IN THE VERTICAL STABILIZER FITTING. THIS CAUSED DAMAGE TO THE FITTING FROMSDR WVER061220150001Drag Angle · crackedRIGHT VERTICAL STABILIZER DRAG ANGLE IS CRACKED 1.5" LONG.SDR ASOA20150611132Drag Angle · crackedDURING C-CHECK, THE LT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAMES 75-76. MAINTENANCE R & R THE ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR NACA201505010044Fitting · corrodedCORROSION ON VERTICAL STABILIZER ON RT AFT FITTING FWD SIDE. DURING THIS INSPECTION, CORROSION WAS NOTED IN THIS FITTING AND FOUND TO BE BEYOND LIMITS. FITTING WAS REPLACED WITH NEW IAW BAC DWG 65-53744, REV C AND SRM R108, REF KFC MCO 3218, WO 1367614.SDR NACA201505010042Attach Fitting · corrodedCORROSION ON VERTICAL STABILIZER ATTACH FITTING LT AFT FWD FACE. DURING INSPECTION CORROSION WAS NOTED ON THE VERTICAL STABILIZER ATTACH FITTING, LT SIDE, AFT. FITTING WAS REPLACED WITH NEW. STABILIZER REMOVAL WAS NOT NECESSARY.SDR DALA2015030401954Attach Fitting · crackedLEFT VERTICAL FIN ATTACH ANGEL HAS 1" LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. COMPLIED WITH PRI/ERA 533587-14, REV O.SDR ABXA20150224020Angle · crackedVERTICAL STABILIZER TO SKIN ANGLE LT OTBD END CRACKED, ACCESS THROUGH PANEL 324AL. REMOVED ANGLE, FABRICATED NEW ANGLE IAW DWG 173T1302 FROM 2024-T3 .040. PERFORMED HFEC INSPECTION. INSTALLED NEW ANGLE IAW SRM 5140-02. SDR INFO, CRACKED 1.900", PN 173T1302SDR SIMA20150127008Angle · crackedRIGHT VERTICAL STABILIZER TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. REPAIRED RT VERTICAL STAB TO FUSELAGE FWD ANGLE AFT END IAW EO CR-55MR-038 & ERS CR--5500-230.SDR SIMA20150108012Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE FWD ANGLE HAS EVIDENCE OF A CRACK ON THE AFT END. APPROX 1 INCH LONG. REPAIRED IAW EO CR-55MR-038.
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