JASC 5521
Service difficulty reports · 520
Reports filed under 5521 · Elevator, Spar/Rib, 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 = '5521' 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 = '5521' 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 DHL9872166DRib · crackedAT D-CHECK, X-RAY INSP SHOWS INTERNAL LOWER RIB CRACKED, DAMAGE TO THE LT ELEVATOR SKIN SEEN THROUGHT ACCESS PANEL 9309. REMOVED AND REPLACED ELEVATOR SKIN PANEL PER SRM 51-30-2. REBALANCED ELEVATOR PER SRM 51-80-7. INSTALLED ELEVATOR AND RIGGED PER MM 27-SDR SCNA98511Spar · crackedDURING HEAVY CHECK, CRACKS WERE DISCOVERED IN THE RIGHT HAND HORIZONTAL SPAR HAS A .5 INCH CRACK AT STATION XSFS 86/XE 28.42. LOCATED AND DRILLED ANGLES, DOUBLER, SHIM AND 'T' CHORD PER SRM 552000, ALODINED AND TREATED PER SRM 512101. INSTALLED ANGLES, DOUBSDR TWAA9810711Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LOWER SURFACE AT DAMPER CUT OUT LOWER RIB CAP CRACKED ON LT ELEVATOR. REPLACED LOWER RIB CAP PER DAC DWG 9918535. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR AU980632Spar · cracked(AUS) LT ELEVATOR SPAR CRACKED IN AREA OF ATTACHMENT FOR THE ELEVATOR TORQUE TUBE ASSEMBLY. FOUND DURING INSPECTION IAW PIPER SB 1008. PART TC: 9,523.SDR CA980610015Rib · corroded(CAN) WHILE CARRYING OUT AD CF-97-06 THE TIP RIB OF THE LEFT ELEVATOR WAS FOUND SEVERELY CORRODED.SDR SCNA98507Spar Cap · crackedDURING HEAVY CHECK, THE RIGHT HAND HORIZONTAL STABILIZER XFS77 XE57 WAS FOUND TO HAVE A 2 INCH CRACK AS VIEWED FROM INTERSPAR BOX ON TOP OF FORWARD SPAR AT JUNCTION OF FUSELAGE SKIN ON FORWARD SPAR. MATERIAL VERIFIED 7075 T6 .125 FOR REPAIR DOUBLER -11 AND 1SDR CA980602092Spar · cracked(CAN) ELEVATOR SPAR CRACKED AT THE OUTBOARD SECTION OF THE OUTER HINGE. LEFT ELEVATOR.SDR 98ZZZX2340Spar · crackedDURING A SCHEDULED INSPECTION, FOUND THE LT ELEVATOR REAR SPAR CRACKED , 1 INCH LONG. CRACK EMANATES FROM LOWER INBOARD CORNER OF HINGE BRACKET SHEAR PLATE AT BS 66.50 AND PROTRUDES TO UPPER OUTBOARD STIFFENER MOUNT HOLE. N/R NR J0012/128872.SDR DL72K981030Rear Spar · crackedAN .375 INCH CRACK RT ELEVATOR REAR SPAR AT 2ND FROM O/B TAB, HINGE. REPLACED REAR SPAR UNDER EO 4-70183-3AD ME 02 AND ME 03.SDR CA980506003Spar · cracked(CAN) LEFT ELEVATOR SPAR CRACKED IN 2 PLACES AT OUTBOARD HINGE ATTACH POINT UNDER HINGE. REPAIRED.SDR UPS98226475Rib · crackedINSPECTION TYPE-C, RESULTS OF X-RAY INSPECTION ON LT ELEVATOR SHOWS CRACK IN LOWER RIB REPAIR AREA BETWEEN ES 66.79 AND 69.79 AT 23 INCHES FWD OF TRAILING EDGE. DAMAGED AREA OF RIB TRIMMED OUT AND REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-10-006, UPS ENSDR UPS98226472Rib · crackedINSPECTION TYPE-C, RESULTS OF X-RAY ON LT ELEVATOR SHOWS CRACK IN LOWER RIB AREA BETWEEN ES 66.79 AND ES 71.79, 23 INCHES FWD OF TRAILING EDGE. DAMAGE TRIMMED OUT IAW SRM 55-20-1 AND REPAIR CARRIED IAW SRS ENGINEERING ORDER 98-10-006, REF UPS ENGINEERING FILESDR DL72S980657Spar · crackedHORIZ STABILIZER RT ELEVATOR REAR SPAR, REPAIR FOR TYPICAL CRACKS. THE RT ELEVATOR REAR SPAR WAS FOUND WITH TWO TYPICAL CRACKS .25 OR SMALLER EXTENDING FROM UNDERNEATH THE 2ND HINGE FITTING FROM THE OUTBD END OF THE SPAR. THE CRACKS WERE STOP DRILLED PER BACSDR 98ZZZX1331Rib · buckledUNDER SIDE OF RIGHT STABILIZER DAMAGED AT THIRD RIB OUTBOARD OF CENTER OF STABILIZER RESULTING IN RIB BUCKLING AND ALSO FORWARD SPAR AT CENTER LIGHTENING HOLE BUCKLED AND CRACKED IN THE WEB. DAMAGE POSSIBLY CAUSED BY GROUND HANDLING OF AIRCRAFT. DAMAGE FOUNDSDR DL72S980526Spar · crackedTHE LT ELEVATOR REAR SPAR WAS FOUND WITH A TYPICAL CRACK AT THE SECOND FROM THE OUTBD END HINGE. THE CRACK WAS STOP DRILLED PER THE REQUIREMENTS OF BOEING S/B 727-55-0089 AND IS BEING TRACKED PER ER/A 364195-14AD. THE PERMANENT REPAIR WILL MODIFY THE SPAR PESDR AU980299Spar · cracked(AUS) ELEVATOR SPAR CRACKED ACROSS SPAR WEB IN AREA OF OUTBOARD HINGE ATTACHMENT. CRACK ORIGINATED AT THE HINGE ATTACHMENT BOLT HOLE AND PROPAGATED IN BOTH DIRECTIONS. FACTORY FITTED DOUBLER ALSO CRACKED.SDR CA980430028Rib · cracked(CAN) TWO 1 INCH GRACKS FOUND ON ELEVATOR INPUT QUADRANT RIB. REPLACED.SDR DL72W980452Spar · misdrilledDURING ACCOMPLISHMENT OF THE REAR SPAR MOD ON THE LT ELEVATOR IT WAS NOTED THAT SEVERAL HOLES WERE OVERSIZED. REPAIRED PER ERA 331369-14AD.SDR AU980144Spar · cracked(AUS) ELEVATOR SPAR AND RIB CRACKED.SDR DL72S980246Fitting · looseHORIZONTAL STABILIZER, RT ELEVATOR, REPAIR FOR LOOSE HINGE FITTING. THE STA 81.44 HINGE FITTING ON THE RT ELEVATOR WAS FOUND. LOOSE DURING INSPECTIONS REQUIRED PER AD 96-06-05. THE LOOSE FITTING WAS TIGHTENED PER PROCEDURES IN BAC S/B 727-55-0089 AND DOCUMESDR CA980309009Rib · cracked(CAN) DURING INSPECTION CRACKS FOUND IN ELEVATOR INBOARD IN AREA OF TORQUE TUBE ATTACHMENT HOLES. ELEVATOR MUST BE REMOVED FOR VERIFICATION AND REPAIR.SDR 98ZZZM236Spar Cap · corrodedAT SCHEDULED, EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS PART NR 'S 101-920014-45, AND 101-620014-47. (M)SDR 98ZZZM217Spar Cap · corrodedAT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS, P/N'S 101-920014-45, AND 101-620014-47. (M)SDR 98ZZZX976Spar · crackedUPON C/W PIPER SB 998, BOTH ELEVATOR SPARS WERE CRACKED .50 INCH IN FROM OUTBOARD END. (BOTH SPARS REPLACED). ELEVATOR SPAR REPLACEMENT NR'S 40075-020 AND DASH 021 ARE IMPROVED DESIGNS.SDR MWEA97871Rib · crackedDURING C-CHK, FOUND CRACK AT RT ELEV NOSE RIB STA XHS106. MAINTENANCE REMOVED AND REPLACED DOUBLER IAW SRM 51-10-2A, 51-10-4, 51-30-5.SDR DL72S972586Spar · crackedHORIZONTAL STABILIZER, RT ELEVATOR, REAR SPAR, REPAIRED FOR LOOSE HINGE FITTING AND SPAR CRACKS. THE RT ELEVATOR WAS FOUND WITH ONE HINGE FITTING LOOSE. THREE (3) .125 INCH LONG CRACKS WERE FOUND IN THE REAR SPAR WEB EXTENDING FROM THE CORNERS OF THE SHEAR SDR 97ZZZX5194Spar · crackedFOUND ELEVATOR SKIN CRACKED FROM THE INSIDE. INVESTIGATION REVEALED CRACKS IN SPAR RADIUS OUTBOARD HINGE BRACKET.SDR 97ZZZX5190Spar · crackedELEVATOR SKIN CRACKED FROM THE INSIDE. INVESTIGATION REVEALED CRACKS IN LOWER SPAR RADIUS OUTBOARD HINGE BRACKET. THIS WAS ON BOTH LEFT AND RIGHT ELEVATORS.SDR HEEA0012129Spar · mis mfgR/H ELEVATOR SPAR IS TOO SHORT. IT IS 5 1/16" LONG AND SHOULD BE 5 3/4" LONG.SDR CA971219012Rib Assembly · cracked(CAN) WHEN REPLACING MAIN SPAR IN RIGHT HAND ELEVATOR PER SB 998A, THE END RIB ASSY WAS FOUND CRACKED WHERE THE SPAR ATTACHES TO THE RIB. CRACK ABOUT .50 INCH LONG. AIRCRAFT TT: 12,445 HOURS.SDR AU971448Rib · cracked(AUS) ELEVATOR RIB CRACKED. LOOSE AND MISSING RIVETS.SDR ASAA9710106Rib · chafedSEA - DURING C-CHECK, WEAR WAS FOUND AT THE HORIZONTAL STABILIZER TRAILING EDGE RIBS AT STATION 66.54, 94.07, AND 121.9. REPAIRED PER EA 5510-01066 AND BOEING TELEX ASA-SEA-91-0202RR. (M)SDR BIER970048Spar · crackedDURING COMPLIANCE WITH PIPER SB 1008, FOUND RIGHT ELEVATOR TAB ON SPAR END (TO BE REMOVED AS PART OF THE SB) CRACKED FROM THE TOP DOWN TO APPROX MID POINT.SDR DL72L972116Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER I/B SIDE OF THE SECOND FROM THE I/B HINGE FITTING. THE CRACK IS APPROXIMATELY .25 LONG. THIS CRACK LENGTH IS WITHIN THE .250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED UNSDR 97ZZZX4444Spar · crackedCOMPLIED WITH PIPER SB 998A, DATED 8-4-97. CUT OPEN AND INSPECTED ELEVATOR SPAR FOR CRACKS. FOUND .75 INCH CRACK IN TIP OF RIGHT ELEVATOR AND RIVET SHEARED ON SUPPORT TAB. SPAR REPLACED.SDR DL72S971991Rear Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR IS CRACKED IN TWO LOCATIONS. THERE IS A CRACK MEASURING .099 EMANATING FROM THE SHEAR PLATE AT THE SECOND FROM THE O/B HINGE, AND THE OTHER IS .167 EMANATING FROM THE SHEAR PLATE AT THE THIRD FROM THE O/B HINGE. THIS ER/A AUTSDR 97ZZZX4382Spar · crackedUPON COMPLYING WITH PIPER SB 998A INSPECTION OF ELEVATOR SPAR, FOUND THE SPAR CRACKED INBOARD OF THE OUTBOARD HINGE. ONLY ABOUT .25 INCH OF THE CRACK WAS VISIBLE. THE END RIB HAD A CRACK WHERE THE SKIN STIFFENER CHANNEL IS RIVETED TO IT AND ONE SKIN STIFFENESDR DL72S971824Rib · crackedAT MV2, FOUND RIB CRACKED. THE LOWER SKIN AT ELEV STA 99.79 TO 136.50 HAS A BUBBLE RIB CRACKED ON O/B END. REPAIRED PER SRM 55-20-3 FIG 3.SDR CA980616004Spar · cracked(CAN) LEFT ELEVATOR SPAR FOUND WITH .50 INCH CRACK AT OUTBOARD END NEAR THE OUTBOARD BEARING. SUBMITTER SAYS THAT PROBLEM CAUSED BY DOCKHANDS USING ELEVATOR TIP TO MANEUVER AIRCRAFT FOR DEPARTURES AND ARRIVALS.SDR DL72S971765Rear Spar · crackedTHE RT ELEVATOR REAR SPAR HAS A CRACK EMANATING .25 INCH FROM THE LOWER INBOARD CORNER OF THE SHEAR PLATE UNDER THE SECOND TAB HINGE FITTING O/B FROM THE I/B END. THIS DAMAGE WAS REPAIRED IN ACCORDANCE WITH AD 96-06-05 AND S/B 727-55-0089.SDR CA970902012Spar · cracked(CAN) IN COMPLYING WITH PIPER SB 998 INSPECTION OF ELEVATOR SPAR FOR CRACKS, IT WAS FOUND THERE WERE SEVERAL CRACKS AT THE OUTBOARD END OF THE SPAR. CRACKS OF THE SPAR WERE FOUND ON BOTH LEFT AND RIGHT ELEVATOR SPARS.SDR 97ZZZX3919Spar · crackedDURING INSPECTION PER PIPER SB 998A, FOUND CRACKS IN BOTH UPPER AND LOWER FLANGE RADIUS AS DESCRIBED. NO CRACKS IN AREA OF OUTBOARD HINGE ATTACH REINFORCEMENT.SDR 97ZZZX3918Spar · crackedDURING INSPECTION PER PIPER SB 998A, FOUND CRACKED IN UPPER FLANGE RADIUS AS DESCRIBED. NO CRACKS IN AREA OF OUTBOARD HINGE ATTACH REINFORCEMENT.SDR ASAA9710055Rib · chafedSEA - DURING 'C' CHECK, THE UPPER T-CHORD ON THE LEFT ELEVATOR BALANCE BAY 2 OUTBOARD RIB UPPER CHORD WAS FOUND CHAFED. REPAIRED PER EA 5520-01048 AND BOEING SRM. (M)SDR CALA9700990Spar · crackedINSPECTION FOUND 2 CRACKS IN REAR SPAR RT ELEVATOR AT TAB CENTER HINGE FITTING. THE SPAR WAS REPLACED IAW SRM 51-80-1.SDR 97ZZZX3076Spar · crackedWHILE DOING REPETATIVE INSPECTION OF PIPER SB 998 WITH BORESCOPE, FOUND .75 INCH LONG CRACK IN TOP OUTBOARD SPAR. CRACK WAS NOT THERE 100 HRS AGO. 100 HOURS AGO HOLES WERE CUT PER SB 998.SDR CA970630005Spar · cracked(CAN) WHILE CARRYING OUT A SKIN REPAIR A VISUAL INSPECTION OF THE ELEVATOR SPAR REVEALED A CRACK IN THE SPAR. THE CRACK WAS FOUND TO BE STARTING AT THE TOP FLANGE AND THROUGH THE UPPER RIVET HOLE, DOWN THE FORWARD FACE OF THE SPAR AND STOPPED AT THE LOWER RIVSDR 97ZZZX2875Spar · crackedAIRCRAFT ELEVATORS WERE OPENED UP IN C/W PIPER MANDATORY SB 998. THE LEFT ELEVATOR SPAR WAS FOUND CRACKED AT THE TIP AND FOUND CRACKED HALF WAY THROUGH THE SPAR JUST INBOARD OF THE VERY OUTBOARD ATTACH POINT. ELEVATOR SPARS NEED TO BE STRENGTHENED UP AT THESSDR DL72L970933Rear Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR IS CRACKED ON THE LOWER INBD SIDE OF THE SECOND FROM INBD HINGE FITTING. THE CRACK IS APPROX .25 INCH LONG. THIS CRACK LENGTH IS WITHIN THE 0.250 STOP DRILL LIMITS OF BAC S/B 727-55-0089. THE CRACK WILL BE STOP-DRILLED (TEMPSDR CA970526002Spar · cracked(CAN) AIRCRAFT EQUIPPED WITH EDO59-5250 FLOATS & TAILPLANE MOUNTED AUX.DORSAL FINS PER JOBMASTER STC 305NW.FINS ARE ATTACHED BY BRACKETS. RIBS,LEFT&RIGHT.AN .040"DOUBLER EQUIPPED WITH ANCHOR NUTS REINFORCES THE REAR SPAR.DURING INSP.THE DOUBLERS,SPARS & TAILP
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