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 USAA960704Angle · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1.5 INCH CRACK IN LEFT VERTICAL FIN DRAG ANGLE AT FS 1132. INSTALLED REPAIR DOUBLERS PER SRM 53-05 FIG 23 AND 23A. (M)SDR USAA960703Angle · crackedPIT - DURING Q-4/C-6 CHECK, FOUND 1.25 INCH CRACK IN RIGHT DRAG ANGLE AT FS 1132 VERTICAL FIN DRAG ANGLE. INSTALLED DOUBLERS PER SRM 53-05 FIG 23 AND 23A. (M)SDR ABXA9700386Fitting · corrodedDURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT FORWARD ATTACH FITTING CORRODED. REMOVED FITTING, REPLACED BUSHING IAW YS-11 OHM 53-40-3, CLEANED CORROSION IAW YS-11 CCM 20-40-0, REINSTALLED FITTING IAW YS-11 M.M. 55-30-0.SDR UPS96221447Fitting · crackedINSPECTION TYPE: SI. POSSIBLE CRACK IN ATTACH FITTING COMMON TO STR 11 UNDER PANEL 9780 RT VERT STAB (MARKED). REMOVED AND REPLACED ATTACH FITTING AT RT VERT STAB STR 11 PER 51-30-2 OF THE SRM.SDR 9622169618Fitting · crackedDURING M-CHECK, FOUND CORROSION ON THE VERTICAL STABILIZER LEFT RUB STRIP ATTACH FITTING AND A CRACK IN THE RIGHT RUB STRIP ATTACH FITTING. REPLACED BOTH FITTINGS PER SRM 51-30-5.SDR TAOA109608Fitting · exceeded limitsDURING D-CHECK, THE VERTICAL STABILZIER TENSION TIES REQUIRED REWORK ACCORDING TO BOEING SB 55-0071. THE REWORK DIMENSIONS SET FORTH EXCEEDED THE SB LIMITS. REWORK DIMENSIONS WERE APPROVED BY BOEING. (X)SDR DL72P962325Stringer · crackedFOUND DURING HMV, STRINGER 6L FIN STA 157.2 IS CRACKED. INSTALLED NEW ANGLE PER M/M 55-30-0.SDR DL72P962324Stringer · crackedFOUND DURING HMV, STRINGER 10L FIN ST 133.80 IS CRACKED. INSTALLED REPAIR ANGLE PER M/M 53-30-0 FIG 803.SDR DL72P962323Stringer · crackedFOUND DURING HMV, STRINGER 6L FIN ST IS CRACKED. INSTALLED NEW ANGLE PER M/M 55-30-0.SDR CKSA96161Bracket · crackedDURING B-CHECK INSPECTION, FOUND INTERNAL VERTICAL STABILIZER STA 1342 FIN REAR SPAR CHORD BRACKET CRACKED IN RADIUS APPROXIMATELY 6 INCHES LONG LEFT HAND SIDE. REMOVED AND REPLACED PART IAW 727 SRM 51-10-1 AND ENGINEERING REPORT NR 96 AIA-132. TASK CARD NR SDR CKSA96160Stiffener · crackedDURING B-CHECK INSPECTION, FOUND INTERNAL VERTICAL STABILIZER STA 1342, VERTICAL STIFFENER CRACKED LEFT HAND SIDE. REMOVED AND REPLACED VERTICAL STIFFENER STA 1342 IAW B727 SRM 51-10-1 AND ENGINEERING REPORT NR 96 AIA-132. TASK CARD NR 86459 CORRSION CARD NRSDR HEEA968115Support Assy · chafe wiresON JULY 5, 1996 AT AIRCRAFT TOTAL TIME 214:10 3 WIRE CABLES WERE INSTALLED IN VERTICAL FIN AS THE OTHERS WERE SEVERELY CHAFED. THE NEW CABLE WAS REPAIRED 2 OR 3 TIMES. THEN ON JULY 22, 1996, THE CABLE WAS REPLACED AGAIN BECAUSE IT IS CHAFING SEVERELY WHERE TSDR 97ZZZX1447Stringer · crackedDURING C-10 INSPECTION, A CRACK WAS NOTED ON VERTICAL STABILIZER, STR 8L AT RIB NR 7.SDR ABXA9700670Angle · crackedDURING C-CHECK, THE VERTICAL STABILIZER INTER SPAR BOX FORWARD LOWER ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW REA D955-16656-MR.SDR UPS96221393Chord · corrodedINSPECTION TYPE-C, VERT FIN TORQUE BOX LT HORIZ CHORD FS 1342 FIN STA 0 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPLACED CHORD AT STA 1342 FIN STA 0 PER DHC SK 950-435.SDR DL72K962175Stringer · crackedCRACK IN VERTICAL STAB STRINGER AT RIB CHORD ATTACH POINT RT SIDE STR 8 FIN STA 157.2, REF EO 4-59253-12. INSTALLED DOUBLER PER M/M 55-30-0.SDR USAA960607Frame · crackedPIT - DURING Q-3/C2 CHECK FOUND .5 INCH CRACK AT LOWER FIXED LEADING EDGE FRAME 4 OF VERTICAL STABILIZER. REPLACED DEFECTIVE PART WITH IDENTICAL PART NR 991188411. (M)SDR USAA960606Frame · crackedPIT - DURING Q-3/C2 CHECK, FOUND .5 INCH CRACK IN LOWER FIXED LEADING EDGE FRAME 5 OF VERTICAL STABILIZER. REPLACED DEFECTIVE PART WITH IDENTICAL PART NR 991188511. (M)SDR 96FDEA01489Hi-Lock Collars · missingSNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STABILIZER TO LOWER VERTICAL STABILER. REF LAX C-CH-02, SNRM NR 0352.SDR MWEA96456Center Hinge · crackedDURING INSPECTION, VERTICAL STAB REAR SPAR CENTER HINGE FOR THE RUDDER FOUND CORRODED ON RT ATTACH LEG. REMOVED THE HINGE AND FOUND CORRODED LEG CRACKED. REPLACED HINGE IAW DAC MM 20-16-0, PG. 209, FIG. 205.SDR DL72S962044Stringer · crackedTHE VERTICAL STABILIZER STRINGER 9L WAS FOUND CRACKED AT FIN STA 157.2, DURING EXECUTION OF EO 4-59253-12AD. THIS EO CALLS FOR A REPAIR PER B727 SRM 55-30-4, HOWEVER STR 9L CANNOT BE REPAIRED PER SRM PROCEDURE DUE TO SPACE LIMITATION ON INBOARD FLANGE. STRINSDR 9619109756Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE VERTICAL STABILIZER FRONT SPAR GUSSET FITTING LEFT SIDE AT FS 155. REPLACED FITTING PER SRM 51-30-2, 51-30-5.SDR 96ZZZX5994Fitting · corrosionVERTICAL STABILIZER HINGE FITTINGS HAVE CORROSION DAMAGE AT THE BEARING HOLES. REPAIRED FITTINGS PER DALFORT AVIATION XEA NR X1-55-130.SDR 96ZZZX5993Fitting · corrosionVERTICAL STABILIZER HINGE FITTINGS HAVE CORROSION DAMAGE AT THE BEARING HOLES. REPAIRED FITTINGS PER DALFORT AVIATION XEA NR X1-55-130.SDR 97ZZZM100Structure · wornVERTICAL STABILIZER LEADING EDGE, BOTH LEFT AND RIGHT DE-ICE SUPPLY DUCT WEARING INTO AUXILLIARY STRUCTURE. REMOVED DUCTS AND REPAIRED AUX STRUCTURE AT VERTICLE STAB RIB 1 AREA IAW AVRO FAX DJR/RJ0930-96. NEW W/C GENERATED FOR DUCT INSTALLATION.SDR 96ZZZX5533Cap Angle · corrodedMAJOR INSPECTION, FOUND VERT PYLON CAP ANGLE CORRODED BEYOND LIMITS, INNER GRANULAR CORROSION, IMPROPER CORROSION PREVENTION, NORMAL WEAR AND TEAR.SDR 96ZZZX5532Web · crackedMAJOR INSPECTION, FOUND VERT PYLON WEB CORRODED AND CRACKED, NORMAL WEAR AND TEARSDR 96ZZZX5531Web Doubler · crackedMAJOR INSPECTION, FOUND VERT PYLON WEB DOUBLER CORRODED AND CRACKED, NORMAL WEAR AND TEAR.SDR 96ZZZX5530Bulkhead · corrodedMAJOR INSPECTION, FOUND VERT PYLON BULKHEAD CORRODED BEYOND LIMITS, INNER GRANULAR CORROSION, NORMAL WEAR AND TEAR.SDR 96ZZZX5529Doubler · crackedMAJOR INSPECTION, FOUND VERT PYLON DOUBLER CRACKED, NORMAL WEAR AND TEAR.SDR 96ZZZX5528Bulkhead · crackedMAJOR INSPECTION, FOUND VERT PYLON BULKHEAD CRACKED, NORMAL WEAR AND TEAR.SDR 96ZZZX5526Angle · corrodedMAJOR INSPECTION, FOUND VERT PYLON LT ANGLE CORRODED BEYOND LIMITS, INNER GRANULAR CORROSION, NORMAL WEAR AND TEAR.SDR 96ZZZX5525Angle · corrodedMAJOR IN SPECTION, FOUND VERT PYLON ANGLE CORRODED BEYOND LIMITS, IMPROPER CORROSION PREVENTION, INNER GRANULAR CORROSION, NORMAL WEAR AND TEAR.SDR 96ZZZX5524Fitting · defectiveMAJOR INSPECTION, VERT PYLON FITTING BOLT HOLE DIAMETER BEYOND LIMITS. NORMAL WEAR AND TEAR.SDR 96ZZZX5523Shear Deck · crackedMAJOR INSPECTION, FOUND VERTICAL PYLON SHEAR DECK CRACKED, NORMAL WEAR AND TEAR.SDR 97ZZZX287Bolts · corrodedVERTICAL STABILIZER TRAILING EDGE; TOP AND CENTER HINGE BOLTS HAVE INDICATIONS OF CORROSION. REMOVED FOR DV. CORRECTIVE ACTION: REMOVED, CLEANED, AND INSTALLED VERTICAL STABILIZER TO RUDDER, TOP, AND CENTER HINGE BOLTS. NO CORROSION NOTED ON BOLTS.SDR UPS96220830Midspar Chord · corrodedINSPECTION TYPE SI, CORROSION LT FIN MIDSPAR HAS CORROSION AT ACCESS PANEL 9601 FIN STA 226.7, FIN WL 168.39. REAMED HOLES, INSTALLED FREEZE PLUGS, CUTOUT DAMAGED AREA AND REAMED PER ENG FILE NR 727-55-0331.SDR UPS96220829Web · crackedINSPECTION TYPE SI. WHILE WORKING RUDDER TRIM ACTUATOR DISCOVERED WEB CRACKED AT CUTOUTS FOR RTA AND RTB CABLES UNDER PRESSURE SEALS AT FIN STA 87.0 IN FIN TUNNEL. REPAIRED FIN STA 87.0 WEB IN FIN IAW TRAMCO EWO 96-2442, UPS FILE NR 727-55-0332.SDR AALA961178Stringer · crackedTUL - FOUND VERT FIN INTERIOR, STRINGER 9L, CRACKED AT BOLT ATTACH POINT TO RIB NR 2. REPAIRED WITH DOUBLER PER ESO 11697, DATED 7-1-96. (M)SDR SWAA960736Doubler · gougedDURING SCHEDULED D-CHECK, FOUND DOUBLER ON LT VERTICAL STAB AFT T-BEAM HAS A DEEP GOUGE, 10 INCHES FROM TOP OF BODY. REPLACED DOUBLER PER BOEING SRM.SDR MWEA96315Fitting · crackedDURING D-CHECK, THE RT FWD VERTICAL STAB ATTACH FITTING WAS FOUND CRACKED BETWEEN BOLT HOLES AT STA 1087. INSTALLED A NEW ATTACH FITTING IAW SRM 55-01, PG 1.SDR UPS96220943Horiz Chord · corrodedINSPECTION TYPE-C, VERT FIN TORQUE BOX RT HORIZ CHORD CORRODED OUT OF LIMITS STA 1342 FIN STA 0. REMOVED DAMAGED SECTION OF CHORD, FAB'D AND INSTALLED REPAIR PARTS PER DHC SK 951-021.SDR CA970311019Vertical Stab · insert failed(CAN) INSERT FAILURE AND SURROUNDING HONEYCOMB DAMAGED.SDR DL72S961780Web · crackedFOUND CRACK AT 1303 B/H STR CUTOUT LEFT SIDE INSIDE VERTICAL STABILIZER JUST ABOVE 'S' DUCT. REPAIRED PER SRM 53-10-4.SDR CALA9601143Attach Angle · crackedINSPECTION FOUND RT DORSAL FIN ATTACH ANGLE CRACKED. THE ANGLE WAS REPAIRED IAW EA 5340-01012.SDR USAA960507Drag Angle · crackedPIT - DURING Q3/C5 CHECK, FOUND 1 INCH CRACK THROUGH RIVET AT LT VERTICAL STABILIZER DRAG ANGLE AFT SIDE CANTED STATION 1388. INSTALLED REPAIR STRAPS AND ANGLES PER SRM 55-02 FIG 26 CONFIG 7001. (M)SDR CA960802201Tail Strut · broken(CAN) PILOT NOTICED VIBRATION FROM THE TAIL SECTION AND LANDED WITHOUT INCIDENT. INVESTIGATION FOUND A BROKEN STRUT WIRE AND REPLACED IT. THE FLYING WIRE BROKE AT THE THREADS APPROXIMATELY 1.250 INCHES FROM THE END.SDR 97ZZZX324Rivets · looseATW - LAST 3 RIVETS ON THE VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE ARE SMOKING (RT). CORRECTIVE ACTION: REMOVED AND REPLACED RIVETS. ON LAST RIVET (MOST AFT) INSTALLED HI LOC BOLT. HLT900-6. GENERATED W/C FOR REINSP PER FAX DJH/RJ0768-96.SDR 96ZZZX3782Tailpost · crackedTAILPOST DISCOVERED TO BE CRACKED AROUND THE CIRCUMFERENCE JUST ABOVE THE TAILSPRING PAD. SUBMITTER SUGGESTS CAUSE FOR CRACK DUE TO GROUND HANDLING OVER THE YEARS AND HIGH TIME ON THE AIRFRAME. THIS POINT IS STRESSED WHEN SWIVELLING THE TAILWHEEL DURING GROSDR DL72L961582Stringer · crackedVERTICAL STABILIZER STRINGER 9R WAS FOUND CRACKED OUTSIDE RIB 7 AT STA 133.8 DURING EXECUTION OF EO 4-59253-12 AD. EO CALLS FOR A REPAIR PER B727 SRM 55-30-4, HOWEVER STR 9R CANNOT BE REPAIRED PER THIS SRM PROCEDURE DUE TO SPACE LIMITATIONS ON IBOARD FLANGE.
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