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 SWAA2015050739403Tail Cone · delaminatedLEFT VERTICAL STABILIZER DELAMINATED ON THE TAIL CONE. REPAIRED STABILIZER IAW EA.SDR DALA2015041502785Fastener · looseVERTICAL FIN L/E MID SPLICE HAS MANY FASTENERS LOOSE. R & R IAW SG0955004. LP 1905434.SDR VNAA2015040300010Drag Angle · crackedLEFT AND RIGHT VERTICAL STABILIZER LOWER FUSELAGE ATTACHMENT DRAG ANGLES AT 67.5 PERCENT REAR SPAR DATUM, ARE CRACKED. C/W REO 670-55-31-018, REV DATED 4/16/07.SDR DXTR2015041401Pivot · crackedVERTICAL SPAR PIVOT FITTING LOWER LT SIDE BOTTOM STRINGER CLIP CRACKED. R & R VERTICAL STABILIZER PIVOT CLIP REF SRM 55-30-01 AND REPAIR DEFINITION S-560XL-5240/05RD DATED 04/10/15.SDR K11A2015052725002Beam · crackedVERTICAL STAB KICKLOAD BEAM LT WEB POST CRACKED WERE IT ATTACHES TO STRINGER 11 IAW SB 727-55-0093, FIG 3, SHEET 4 FOR LOCATION.SDR DALA2015040202562Attach Angle · crackedVERTICAL STABILIZER LT SIDE INTERNAL ATTACH ANGLE IS CRACKED AT STA 1475. REPLACED ANGLE IAW SRM 51-30-00.SDR DALA2015032502397Angle · crackedCRACK ON LT/RT INTERNAL VERTIACL STABILIZER ATTACH DORSAL ANGLES BETWEEN STA Y=1458 TO 1486. DORSAL ANGLES WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-02 AND 51-30-05.SDR DALA2015031502150Former · crackedCRACKED FORMER ON TIP FAIRING STA YV 172. REPAIR WERE FABRICATED IAW SRM 55-01 IG 4. DOUBLERS AND FILLERS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14-21. REPAIR INSTALLED IAW SRM 51-302.SDR DALA2015031702209Doubler · crackedCRACKED INTERNAL DOUBLER ON VERTICAL STABILIZER ACCESS PLATE 370 BL CUTOUT. REPAIRED CRACK IAW SRM 5330-05, FIG 3.SDR SWIA201540928Panel · crackedDORSAL STRAKE PANEL 321 CT IS CRACKED AT AFT SIDE. REPAIRED THE PANEL IAW EA.
SDR SWIA201540927Panel · delaminatedDORSAL STRAKE PANEL 321 BT IS DELAMINATED ON BOTTOM SIDE, C-CHECK, RO 3/24/15, REPAIRED DELAMINATION ON PANEL 321BT, REF STS EA.SDR VNAA201503100017Drag Angle · crackedLEFT FWD VERT STAB DRAG ANGLE IS CRACKED APPROXIMATELY .25 ON AFT END. PERFORMED A MAJOR REPAIR TO THE LT VERTICAL STABILIZER FUSELAGE ATTACHMENT DRAG ANGLE AT 67.5 PERCENT REAR SPAR DATUM IAW REO 670-55-31-018, REV-DATED 16-APR-07.SDR DALA2015031002028Fairing · damagedFWD TOP END OF UPPER RT BANANA FAIRING DAMAGED. REMOVED PREVIOUSLY INSTALLED DOUBLER, REMOVED DAMAGE MATERIAL FROM FAIRING REF ERA 464895-14MA. ACCOMPLISHED HFEC NDT SPM 06-10-01-001. DAMAGED CONTAINED. TRIMED AND PILOT DRILLED DOUBLER FROM PN 55-0018-003.SDR DALA2015030401943Attach Angle · crackedLEFT VERTICAL FIN ATTACH ANGLE HAS LONG CRACK IN RADIUS, NEAR FIN AFT SPAR. REMOVED DAMAGE AND INSTALLED DOUBLER IAW PRI/ERA 533587-14, REV O.SDR DALA2015022601668Angle · crackedCRACKED 2 ANGLES BETWEEN UPPER FUSELAGE SKIN AND DORSAL FIN BASE AT L/E RAM AIR SCOOP AREA STA Y= 1407 TO Y= 1427.SDR DALA2015022301580Access Panel · crackedCRACKED SETTLEMENT AREA, BOTH SIDES OF ACCESS PANEL 6301B AT DORSAL FIN L/E. DORSAL ANGLES WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PARA 14 & 21, AND DWG 5912188 REV BD.SDR CA150223008Fitting · cracked(CAN) DURING ANNUAL INSPECTION, FOUND CORROSION ON THE FITTING HOLDING VERTICAL STAB TO HORIZONTAL STAB. WHEN CORROSION WAS REMOVED, FAINT LINES WERE NOTICED. UNDER 10X MAGNIFICATION A CRACK WAS DETECT ON FORWARD VERTICAL SECTION OF FITTING APPROX 1/2" LONG. FSDR DALA2015022301577Structure · damagedLOOSE FASTENERS ON LOWER EDGE RT SIDE ABOVE LOWER SPLICE OF VERTICAL STABILIZER REMOVABLE L/E. HOLES, 17E/AS WERE REWORKED AND BUSHINGS WERE FABRICATED, PROTECTED ALSO INSTALLED IAW SRM 55-03D.SDR WVER0217201500003Drag Angle · crackedVERTICAL STABILIZER FORWARD DRAG ANGLE LT SIDE IS CRACKED APPROXIMATELY .5" IN LENGTH.SDR WVER0217201500002Drag Angle · crackedVERTICAL STABILIZER FORWARD DRAG ANGLE RT SIDE IS CRACKED APPROXIMATELY .5" IN LENGTH.SDR DALA2015021001109Channel · crackedCRACKED Z CHANNEL ON VERTICAL STABILIZER T/E BETWEEN ZRS 38.2 AND ZRS 57.7. Z-CHANNEL REPAIRED IAW SRM 55-01, FIG 2.SDR DALA2015012000417Attach Angle · crackedLEFT INTERNAL VERTICAL STABILIZER ATTACH ANGLE IS CRACKED IN RADIUS. R & R IAW DWG 5912188.SDR WVER2015011700002Drag Angle · crackedLEFT AND RT VERTICAL STABILIZER FORWARD DRAG ANGLES ARE CRACKED.SDR DALA2015012000511Plate · corrodedCORROSION ON BORE OF PLATES, ZRS=173 AND XH=5 LT SIDE LOCATED ON VERTICAL STAB REAR. BORE OF PLATES WAS REMOVED. HOLD WAS REWORKED WITH MEASURED HOLE LT OTBD: O 1.435 AND HOLE. LT INBD: O 1.435, THEREFORE WITHIN LIMIT. REPAIR AND BUSHING WAS FABRICATED, AREA SDR IPXA2015013085497Intercostal · crackedINSPECTION TYPE: 4C, LOWER VERTICAL REAR CENTER SPAR TO REAR SPAR, RT AFT INTERCOSTAL CRACKED STA Y=2164 AT X =-8.5. ACCOMPLISHED PERMANENT REPAIR ON LOWER VERTICAL REAR CENTER SPAR TO REAR SPAR RT INTERCOSTAL STA Y=2164 AT X = -8.5 IAW SRM 55-30-02, REPAIR 7SDR DXTR2015020401Bracket · crackedLOWER CLIP ON VERTICAL STABILIZER HAS 2 SMOKED HI-LOCKS ON OTBD EDGES ON FWD SIDE. FOUND A CRACK PROTRUDING FROM THE LT OTBD LOWER PIVOT FITTING FLANGE TRAVELING UP & OTBD APPROX .5" FOUND 2 CRACKS TRAVELING FROM THE RT OTBD HOLE, ONE TRAVELING UP & OTBD APPRSDR SCNA20141223254Stiffener · crackedRIGHT STABILIZER NR 1 SPAR RIB STAB STA 92.7 FWD VERTICAL STIFFNER CRACKED AT LOWER FLANGE, REPAIRED.SDR SCNA20141223255Stiffener · crackedRIGHT STABILIZER NR 1 INSPAR RIB AT STA 92.7 AFT VERTICAL STIFFNER CRACKED AT LOWER FLANGE, REPAIRED.SDR CA141201002Adapter · cracked(CAN) WHILE COMPLETING SB 6/454, THE RT REAR STABILIZER ATTACHMENT ADAPTER FOUND CRACKED.(P/N C6FSM 1820-33). THE ATTACHMENT ADAPTOR WAS REPLACED WITH NO ADDITIONAL DEFECTS NOTED.SDR DALA2014112206313Structure · damagedELONGATED HOLES ON REMOVABLE L/E STA ZFS=52.267 AT VERTICAL STABILIZER. REMOVABLE L/E WAS REPAIR IAW CARD 5530- 01045-08 AND SRM FIG 30.SDR WVER2014111700004Drag Angle · crackedFWD DRAG ANGLE ON RT SIDE OF VERTICAL STABILIZER HAS A CRACK.SDR ASOA2014120511817Drag Angle · crackedLT VERTICAL AFT DRAG ANGLE CRACKED. REMOVED THE DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-10-001-01-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-22-001-001-A01 AND DWG BA670-35002.SDR ASOA20141114338Drag Angle · crackedDURING C-CHECK DRAG ANGLE AT LT FWD CORNER OF VERTICAL STAB IS CRACKED. MAINTENANCE R & R DRAG ANGLE AT LT FWD CORNER OF VERTICAL STAB IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20141114337Drag Angle · crackedDURING C-CHECK DRAG ANGLE AT FWD RT CORNER OF VERTICAL STAB IS CRACKED. MAINTENANCE R & R RT FWD DRAG ANGLE ON VERTICAL STAB IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA2014120234604Structure · delaminatedVERTICAL STABILIZER LE DELAMINATED APPROX 4 INCHES FROM LOWER EDGE. REPAIRED STABILIZER IAW EA.SDR ASOA20141110328Drag Angle · crackedDURING C-CHECK, DRAG ANGLE AT FWD RT CORNER OF VERTICAL STAB IS CRACKED. MAINTENANCE R & R DRAG ANGLE AT FWD RT CORNER OF VERTICAL STAB IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA2014102905824Skate Angle · crackedFORWARD RT INNER VERTICAL STABILIZER ATTACH ANGLE HAS A FOUR INCH CRACK. R & R INNER SKATE ANGLE IAW DWG 5912188.SDR CA141120011Bolt · broken(CAN) FIN SPAR RT MAIN ATTACH BOLT WAS FOUND TO BE BROKEN OFF. HEAD OF BOLT WAS STILL IN ATTACH FITTING NUT AND LOWER PORTION OF BOLT WERE MISSING, BOTH BOLTS REPLACED.SDR WVER102220140001Drag Angle · crackedLEFT AND RT VERTICAL STABILIZER FORWARD DRAG ANGLES ARE CRACKED.SDR DXTR2014102101Fitting · crackedHORIZONTAL STABILIZER FITTING ASSY CRACKED ABOVE CLIP ATTACH POINT.SDR A6WA201442107Hinge Bracket · deformedON VERTICAL STAB AFT SPAR, UPPER CTR RUDDER HINGE BRACKET LOWER HALF BORE MALFORMED.SDR SWIA201439679Fairing · damagedLIGHTNING STRIKE DAMAGE TO VERTICAL STABILIZER BULLET FAIRING AND AFT FAIRING ASSY. REPAIRED IAW EA.SDR DALA2014100805480Angle · damagedDURING C-CHECK, ELONGATED HOLES WERE FOUND COMMON TO THE LT ANGLE OF THE VERTICAL STABILIZER FRONT SPAR. FOUR OF THE HOLES ARE THE FIRST, FOURTH, FIFTH, AND SIXTH ABOVE ZFS=52. ONE OF THE HOLES IS THE FOURTH HOLE BELOW ZFS=52. ER/A 529591-14AD SECT I WASDR WVER1006201493802Drag Angle · crackedLEFT VERTICAL STABLIZER FORWARD DRAG ANGLE IS CRACKED APPROXIMATELY 2" LONG.SDR WVER1006201493801Drag Angle · crackedLEFT VERTICAL STABLIZER AFT DRAG ANGLE IS CRACKED APPROXIMATELY 2 " LONG.SDR WVER201409240003Drag Angle · crackedVERTICAL STABILIZER RT AFT DRAG ANGLE IS CRACKED.SDR DALA2014092405233Angle · crackedCRACKED LT/RT ANGLES FWD UPPER SECTION STA YV=170 AT VERTICAL STABILIZER TIP FAIRING. CLIPS 2EA WERE REMOVED FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-10-3, DWG 9911962.SDR WVER0923201450702Drag Angle · crackedRIGHT FORWARD VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY TWO INCHES IN LENGTH ON AFT END.SDR WVER0923201450701Drag Angle · crackedLEFT FWD VERTICLE STABALIZER DRAG ANGLE IS CRACKED APPROXIMATELY 2" IN LENGTH ON AFT END.SDR 7AHR2014092300002Structure · gougedGOUGED AREAS WERE FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER AND LOWER BANANA FAIRING. GOUGED AREAS WERE FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR TO TIP PLATING IAW FLIGHT VEHICLE CONSULTING DWG NR 55-14233-1, REV-NEW, DATED SE
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