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 MWEA00779Rib · damagedMKE - FOUND LEFT ELEVATOR HAS TOOLMARKS ON 21ST LEADING EDGE RIB, INBOARD SIDE, UPPER FLANGE. REMOVED RIB, LOCATED, DRILLED, AND INSTLALED NEW RIB. (M)SDR MWEA00780Rib · misdrilledMKE - FOUND LEFT ELEVATOR HAD A MISDRILLED HOLE IN THE 26TH LEADING EDGE RIB. REMOVED RIB AND ANGLE. FABRICATED ANGLE, LOCATED, DRILLED NEW RIB AND ANGLE. INSTALLED BOTH. (M)SDR UPS00434092Rib · wornINSPECTION TYPE:C, TAIL VERTICAL FIN LWR L/E SECTION OF RIB WORN AT CONTACT AREA WITH DORSAL FIN. RIB REPLACED IAW SRM 51-30-02.SDR CA000713011Bearing · loose(CAN) - ON INSPECTION, FOUND BEARING TO BE LOOSE IN ITS BORE. BEARING IS AT ATTACH POINT FOR CONTROL INPUT LEVER/ROD. BEARING RE-BONDED IN BORE PER PILATUS TECH MEMO EF-12-TM-778.SDR 20000711SH003Spar · crackedDURING A C-CHECK INSPECTION, THE TRIM ACTUATOR BRACKET OF THE RT ELEVATOR WAS FOUND DISLODGED FROM THE SPAR. FOUR OF SIX FASTENERS HAD FAILED AND THE SPAR IS CRACKED IN NUMEROUS PLACES NEAR THE BRACKET ATTACH POINT. NO FURTHER DAMAGE WAS NOTED ON ELEVATOR ORSDR 0002342292Web · damagedDURING H CHECK FOUND SEVERAL FASTENERS PULLED THROUGH RT ELEVATOR INBOARD CLOSURE WEB. REPAIRED PER EA 22-175173.SDR RAAAOOB1060Stringer · looseDURING SCHEDULED C2 CHECK, FOUND STRINGER REPAIR LOOSE AND WORKING PANEL 9412 STA 110 LT ELEVATOR. REPLACED PREVIOUS REPAIR IAW SRM 55-20-3.SDR L1GA200000142Fitting · corrodedLEVEL 2 CORROSION LT ELEV UPPER FWD SPAR FITTING AT XE230.SDR SWAA000908Spar · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT ELEVATOR REAR SPAR CRACKED NEAR SECOND I/B TAB HINGE. REMOVED AND REPLACED LT ELEVATOR ASSY PER MM.SDR MWEA00398Rib · crackedLEFT ELEVATOR RIB AT STATION 180 IS CRACKED AT THE TRAILING EDGE. FABRICATED AND INSTALLED REPAIR.SDR CALA0000420Spar · crackedINSPECTION FOUND A 1.3 INCH CRACK IN LT HORIZONTAL STABILIZER REAR SPAR CAP AFT BARREL NUT BORE. THE LT HORIZONTAL STABILIZER UPPER AFT SPAR CAP SECTION WAS REPLACED IAW ECRA 5511-01015.SDR CA000324001Spar · cracked(CAN) ON INSPECTION WITH ELEVATOR REMOVED, CRACK WAS FOUND BEGINNING UNDER END OF ANGLE BRACKET LEADING UPWARDS TO UPPER FLANGE. CRACK APPROXIMATELY 2 .50 INCHES LONG.SDR CALA0000197Rib · gougedINSPECTION FOUND LEFT ELEVATOR L/E RIB NR 11 GOUGED AND DENTED. THE RIB WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.SDR CA000301020Spar · cracked(CAN) PILOT REPORTED SUBTLE PITCH FLUTTER. MAINTENANCE FOUND LT ELEVATOR SPAR CRACKING AT OUTBOARD HINGE ATTACH POINT. BOTH ELEVATORS REMOVED AND MODIFIED PER PIPER S/B 1032.SDR CA000215014Rib · cracked(CAN) WHILE DISASSEMBLING THE ELEVATOR TO CARRY OUT INSPECTION REFERENCED IN CF 89-20R1, IT WAS FOUND THAT THE RIB LOWER FLANGE WAS CRACKED. MOD 3/935 SB 3/50 WILL BE INCORPORATED.SDR AT0000048Spar · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK ON RIGHT ELEVATOR SPAR AT ES 76-75. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLES AT ES 76-75 IAW EO 12-5520-29-B1092, DC9 SRM 51-20, 51-30-02, 51-20-03, AND 55-02.SDR UPS00431710Rib · crackedINSPECTION TYPE:C 44, TAIL, LEFT INBOARD ELEVATOR UPPER RIB CRACKED AT STA 82. REPAIR AS PER SRM. RIB REPLACED IAW 51-30-02 AND 51-10-01.SDR TWAA0000606Spar · lightning strikeDURING OP 16 MAINT CHECK, FOUND LT ELEVATOR REAR SPAR LOWER SURFACE APPROX 14 IN FROM OTBD END WITH SKIN BURNED FROM LIGHTNING STRIKE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 55-03, FIG 15 PAGE 32.SDR TWAA0000605Spar · crackedDURING OP 16 MAINT CHECK, FOUND RT ELEVATOR FRONT SPAR CRACKED APPROX 120 IN FROM INBD END. REPAIRED PER DWG 5934866-503.SDR CA991208068Spar · cracked(CAN) INSPECTION AS INDICATED IN PIPER S/B 1032. LEADING EDGE SKIN REMOVED AND FOUND 2 CRACKS ON OUTBOARD END OF SPAR. ONE CRACK WAS ON TOP IN THE BEND RADIUS AND EXTENDING 1 INCH INBOARD BEHIND THE HINGE. THE OTHER CRACK EXTENDED 1 INCH INBOARD ON THE LOWESDR ABXA9900772Rib · crackedDURING C-CHECK, FOUND LEADING EDGE RIB CRACKED ON LEFT ELEVATOR. REPLACED RIB IAW DC9 SRM 51-30-2.SDR 99ZZZX3167Spar · crackedC/W PIPER SB 998A. FOUND LEFT ELEVATOR SPAR CRACKED. BOTTOM, OUTBOARD LOCATION IN BEND ABOUT 1.25 INCHES LONG. SUBMITTER STATED THEY HAVE FOUND CRACKS EVERY TIME THEY C/W SB 998A, AND HAVE FOUND MORE CRACKS IN RIBS AND STIFFENERS AT REPLACEMENT OF SPAR.SDR 99ZZZX2794Spar Assy · mismanufacturedRECEIVED ONE NEW SPAR ASSY ON OR ABOUT 7-15-99. WHEN PART WAS INSPECTED PRIOR TO USE, IT WAS OBVIOUS THE HINGE BRACKET WAS CROOKED AS INSTALLED. THIS PART IS RIVETED TO THE SPAR BY CESSNA. THE PART WAS RETURNED TO KANSAS CITY AVIATION CENTER AND A NEW ONE WSDR DL72L991624Spar · crackedSTABILIZER / LT ELEVATOR / REAR SPAR : CRACK REPAIR. THE L/H ELEVATOR WAS FOUND WITH CRACK EXTENDING.125 INCH BEYOND THE 2ND FROM I/B END HINGE BRACKET. THE CRACK IS TYPICAL OF B727 S/B 55-0089 AND AD 96-06-05. THE CRACK WAS STOP DRILLED PER ER/A 367822-14SDR CA990728099Gusset · damaged(CAN) DEFECT WAS FOUND DURING CARRYING OUT INSPECTION OF AREA WITH BORESCOPE PER S/B 998A VIA INSPECTION HOLE. NO OTHER DEFECT, CRACK, ETC. IT APPEARS FAULTY RIVET WAS NOT BUCKED TIGHT ENOUGH AT A PREVIOUS MODIFICATION INSTALLATION AND FRETTED LOOSE. NEW RISDR 99ZZZX2204Spar · crackedRIGHT ELEVATOR OUTBOARD HINGE ATTACH POINT CRACKED AROUND RIVETS ON SPAR. POSSIBLE CAUSE IS OIL CANNING OF ATTACH POINT ON SPAR.SDR 99ZZZX2019Elevator · misrepairedNOTED THAT RIGHT AND LEFT ELEVATORS APPEARED TO BE MISALIGNED WITH EACH OTHER. UPON FURTHER INSPECTION, FOUND LEFT ELEVATOR HAD BEEN IMPROPERLY REPAIRED IN THE PAST WITH A TWIST BEING BUILT IN. UPON DISASSEMBLY, FOUND MAIN SPAR BROKEN AT TIP OF ATTACH POINT.SDR QXEA9900839Rib · crackedPDX - FALSE RIB ASSEMBLY FOR LEADING EDGE 51E HAS .5 CRACK UNDER CORNER OF FLANGE. REPAIRED IAW HORIZON AIR EA 4-55-121.SDR ABXA9900538Spar · crackedTOP OF LEFT ELEVATOR SPAR CRACKED IN 8 PLACES, STATION 204 TO 220. REPLACED ELEVATOR SPAR IAW DC9 DWG 9918450.SDR CALA9900285Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT ELEVATOR LOWER SKIN JUST I/B AND AFT OF PANEL NR 9311. THE CRACK WAS STOP DRILLED IAW SRM 55-20-3. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, 51-10-2, AND 51-30. A CALCULATED BALANCE WAS PERFORMED IAW SRM 51-80-7 AND WASDR 99ZZZX1197Spar · crackedDURING ANNUAL INSPECTION, FOUND RT ELEVATOR OUTBOARD HINGE P/N 043200171 BOLT HOLE ELONGATED. AFTER REMOVING THREE FOR REPLACEMENT, FOUND ELEVATOR SPAR, PN 0432001-21 CRACKED AT HOME ATTACHMENT RIVET HOLES. THERE IS NO WAY TO INSPECT THE SPAR WITHOUT DE-RIVESDR HEEA060210Bushing · wornRIGHT ELEVATOR ASSEMBLY HAS SEPARATED SPAR SPLICED AND BUSHING WORN.SDR HEEA060209Bushing · wornLEFT ELEVATOR ASSEMBLY HAS SEPARATED SPAR SPLICED AND BUSHINGS WORN.SDR UPS99228557Rib · crackedINSPECTION TYPE-SI, RT ELEVATOR 2 CRACK INDICATIONS NOTED ON X-RAYS VIEW 14 AT ELEV STA 99 8 AND 10 FROM LEADING EDGE. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.SDR UPS99228556Rib · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 7 ON 1ST RIB AFT OF FRONT SPAR AT ELEV STA 40. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.SDR UPS99228555Rib · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY AT VIEW 16 10 AFT OF LEADING EDGE AT ELEV STA 125. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.SDR UPS99228554Rib · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 20 ELEV STA 130, 6 AFT OF FRONT SPAR. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.SDR UPS99228553Spar · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAYS VIEW 22 FRONT SPAR OUT OF FASTENER HOLE AT ELEV STA 150. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.SDR UPS99228552Spar · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATIONS NOTED ON X-RAY VIEW 24, 8 AFT OF FRONT SPAR ELEV STA 167. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.SDR UPS99228551Spar · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 28, 8. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.SDR UPS99228550Rib · crackedINSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 31 ON 1ST RIB FWD OF REAR SPAR AT ELEVATOR STATION 200. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.SDR UPS99228549Rib · crackedINSPECTION TYPE-SI, RT ELEVATOR 4 CRACK INDICATIONS NOTED ON X-RAYS VIEW 13 ALONG LEADING EDGE 79 TO 99 ELEV STA. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.SDR CA981230041Spar · cracked(CAN) INSPECTION PER SB 998A. LEFT HAND SPAR FOUND CRACKED AT THE VERY TIP, OUTBOARD RIB CONNECTION. NEW SPAR, NR 40075-020 INSTALLLED.SDR CKSA98678Spar · corrodedRT ELEVATOR REAR OUTBD SPAR, ZONE 300, HAS 6 AREAS 6 TO 8 INCHES OF SEVERE CORROSION WITH EXFOLIATION. REMOVED AND REPLACED SPAR IAW BOEING DWG ASA CKF-EXB-217 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OSDR ABXA9801108Spar · crackedWHILE COMPLYING WITH AD 79-19-02, FOUND LEFT ELEVATOR CRACKED IN FRONT SPAR AREA. REPLACED ELEVATOR IAW DC9 MM 27-30-02 AND 27-30-03.SDR ABXA9801157Spar · crackedLEFT ELEVATOR SPAR CRACKED IN 4 PLACES. REPAIRED UNIT IAW DC9 SRM.SDR CALA9802018Spar · crackedINSPECTION FOUND A .5 INCH CRACK IN LT ELEVATOR REAR SPAR. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1, PAGE 401 AND 402. RIG AND OPERATIONAL CHECK WAS ACCOMPLISHED IAW MM 27-30-81 PAGE 507.SDR CZMA061348Rib · crackedPART WAS PURCAHSED NEW AND USED AS A SPARE WHILE ORIGINAL AIRCRAFT EQUIPMEMT ELEVATOR WAS BEING REPAIRED. PART WAS THEN SENT TO HELIPRO FOR EMBODIMENT OF T.B. 412-83-31. RIB WAS DISCOVERED AS BEING CRACKED AT HELIPRO AND WAS RETURNED TO CUSTOMER FOR WARRANTYSDR DL72L981760Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR WAS FOUND WITH A .1875 INCH TYPICAL CRACK AT CENTER HINGE BRACKET SHEAR PLATE. THE CRACK WAS STOP DRILLED PER THE REQUIREMENTS OF AD 96-06-05 AND S/B 727-55-0089. THE REPAIR WAS DOCUMENTED PER ER/A 365499-14AD WHICH ESTABLISHSDR DL72L981596Spar · crackedA TYPICAL CRACK WAS FOUND IN THE REAR SPAR OF THE LT ELEVATOR EXTENDING FROM UNDER THE SHEAR PLATE OF THE MIDDLE TAB FITTING. THE CRACK EXTENDS .125 LONG BEYOND THE FITTING. THE CRACK WAS STOP DRILLED PER BAC S/B 727-55-0089 AND WILL BE RE-INSPECTED WITHIN 1
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