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 06FDEA1185Shear Tie · damagedWHILE WORKING CARD 73C023-00, FOUND VERT FIN AFT SHEAR TIE FITTING TO HAVE MECHANICAL DAMAGE ON LOWER SURFACE AT LEFT AFT VERT BOLT HOLE. *S/D* REPAIRED VERT FIN AFT SHEAR TIE FITTING LWR SURFACE IAW FEDEX EA 7-5530-96604.SDR SWAA060850Drag Brace · corrodedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL STAB RT DRAG BRACE CORRODED AT BOTH ENDS. REMOVED AND REPLACED DRAG BRACE PER SRM.SDR SWAA060849Drag Brace · corrodedDURING SCHEDULED 10Y CHECK, FOUND VERTICAL STAB LT DRAG BRACE CORRODED AT BOTH ENDS. REMOVED AND REPLACED DRAG BRACE PER SRM.SDR 06FDEA1054Shear Tie · corrodedFOUND VERT FIN TENSION TIE RIB, AFT SHEAR FITTING, LWR SURFACE HAS CORROSION. *S/D* REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.SDR 06FDEA1053Rib · gougedVERTICAL FIN TENSION TIE RIB, RIGHT FWD VERTICAL BOLT HOLE IS GOUGED. REPAIRED PER FED EX EA 7-5530-99604 MAJOR REPAIR.SDR 06FDEA1049Shear Tie · corrodedWHILE WORKING CARD NO. N00718, FOUND VERT. FIN AFT SHEAR TIE FITTING, UPPER SURFACE HAS CORROSION. REPAIRED PER FED EX EA 7-5530-96604 REPAIR CONSIDERED A MAJOR.SDR QXEA200600678Hinge Fitting · damagedYYC C4, VERTICAL STABILIZER FORE RUDDER ATTACHMENT BOTTOM MID HINGE ASSEMBLY LOWER FITTING HAS DAMAGE ON THE UPPER FACE. REPAIRED IAW HORIZON AIR EA 2-55-129, RD 8-55-1669, ISS 1, DHC-8-200 AMM TASK 27-20-00-830-801, PAGES 513-514 AND AMM TASK 27-20-00-710-80SDR QXEA200600675Hinge Fitting · damagedYYC C4, VERTICAL STABILIZER FORE RUDDER ATTACHMENT TOP MID HINGE ASSEMBLY LOWER FITTING HAS DAMAGE ON THE UPPER FACE. REPAIRED IAW RD 8-55-1669, DHC-8-200 AMM TASK 27-20-00-830-801, PAGES 513-514, 27-20-00-710-801. HORIZON AIR EA 2-55-129.SDR QXEA200600676Fitting · damagedYYC C4, VERTICAL STABILIZER FORE RUDDER ATTACHMENT BOTTOM MID HINGE ASSEMBLY UPPER FITTING HAS DAMAGE ON THE TOP AND BOTTOM FACES. REPAIRED IAW HORIZON AIR EA 2-55-129, RD 8-55-1669, DHC-8-200 AMM TASK 27-20-00-830-801, PAGES 513-514 AND AMM TASK 27-20-00-710SDR GUUA03090601Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, VERTICAL FIN UPPER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED UPPER HINGE BRACKET.SDR MALA060123Skin · lightning strikeDURING N4K BRIDGE CHECK IN YQB, FOUND LIGHTNING STRIKE DAMAGE ON THE LT VENTRAL FIN AND ON THE LT WING AT STATION 415.20. THE REPAIR WILL BE CARRIED OUT IAW MESABA EO S51031 FOR THE VENTRAL FIN AND ON MESABA EO S57112 FOR THE LT WING. REPAIR WILL BE CARRIED SDR 06FDEA0431Web · damagedWHILE WORKING FED EX CARD N00897 FOUND AN EXTRA HOLE ON WEB UNDER UPPER PANEL SUPPORT CHORD ON VERTICAL STAB AT FIN STA 247 UPPER RIGHT SIDE. *S/D* REPAIRED PANEL SUPPORT CHORD ON VERTICAL STAB IAW FED-EX EA 7-5530-96566.SDR 06FDEA0307Beam · damagedWHILE WORKING CARD N01210 (TAIL 5142), FOUND VERTICAL FIN T/E BEAM, UPPER SPICE FITTINGS, 8 EA I/B BUSHINGS WORN. REPAIRED VERTICAL FIN T/E BEAM IAW FED-EX EA 7-5530-96556.SDR 06FDEA0306Beam · damagedWHILE WORKING CARD N01209, FOUND VERTICAL FIN UPPER SPLICE BEAM, BUSHING BORE OVERSIZED & GOUGED. REPAIRED VERT. FIN UPPER SPLICE BEAM BUSHING BORE IAW EA 7-5530-96537.SDR 06FDEA0305Tie · misalignedFOUND THE AFT VERTICAL BOLT HOLES IN THE TENSION TIE AND ATTACH FITTING TO BE MISALIGNED. REPAIRED THE AFT VERT. BOLT HOLES IN THE TENSION TIE AND ATTACH FITTING IAW EA 7- 5530-96550.SDR USAA060117Bushing · migratedVERTICAL STAB, LEFT FWD CENTER LUG BUSHING MIGRATED. REMOVED MIGRATED BUSHING AND REPLACED WITH NEW FABRICATED BUSHING IAW EA 97296, DEFECT SIZE: .010 INCH.SDR USAA060087Bushing · migratedFOUND LUG BUSHING MIGRATING VERTICAL STAB LEFT FWD CENTER LUG BUSHING. REMOVED MIGRATED BUSHING AND REPLACED WITH NEW FABRICATED BUSHING IAW EA 97296, DEFECT SIZE:SDR QXEA200600063Spar · unknownPDX - UPPER RADIUS , FORWARD ATTACH POINT BRACKET HAS STEP WEAR ON INNER CIRCUMFERENCE OF BOLT HOLE BRACKET, IS ATTACHED TO AFT SPAR OF VERTICLE STABILIZER. REPAIRED IAW DASH8-200 SMM 27-20-011-030-801 AND SRM 51-40-00, 51-40-11.SDR C2XA06TY003Housing · gougedLT HORIZ STAB SPERICAL BEARING HOUSING GOUGED. REWORKED HOUSING TO 1ST OVERSIZE W/ENGINEERING APPROVAL. ALL WORK C/W IAW EC5510-01130, EC5510-01080, EMB145-AMM55-37-00.SDR DHL2006752507Frame · crackedVERT STAB BS 1303 FRAME ABOVE ENG INLET PIPE HAS WEB WITH 1" CRACK ON RT LWR CORNER. STOP DRILLED CRACK AS REQUIRED IAW S/B 727-53-0094 REV 3 DATED 4-26-90 ACCOMPLISHED COTNEY AEROSPACE EA: EAZ04-5 REV IR W/8110-3 DATED: 1-12-06. THIS REPAIR IS CAT. "B" VISSDR USAA051320Angle · damagedFOUND VERT STAB TRANSITION ANGLE LEFT SIDE AFT OF REAR ATTACH POINT. FABRICATED AND INSTALLED NEW ANGLE IAW TR 53-20-05A, DEFECT SIZE: 12".SDR SIMA200531506Bearing · corrodedFOUND VERTICAL STABILIZER SPHERICAL BEARINGS CORRODED. REPLACED BOTH VERTICAL STABILIZER SPHERICAL BEARINGS IAW EMB AMM 55-37-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR QXEA200501403Intercostal · brokenYYC - VERTICAL STAB TAIL CONE ASSY HAS A BROKEN INTERCOSTAL. MAINTENANCE REPLACED INTERCOSTAL IAW CRJ-700 SRM 51-42-27-001-001-A01.SDR SWAA053250Beam · crackedDURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER LEFT T/E BEAM CRACKED AT NR 2 RUDDER HINGE ATTACHMENT. REMOVED AND REPLACED BEAM PER SRM.SDR ASAA0580523Angle · crackedOKC - DURING HV CHECK, FOUND VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR ANGLE. (M)SDR DL76S100221Bolt · unknownJOINT BARREL NUT/BOLT ASSY OF VERTICAL FIN REPLACEMENT IAW EO 01-074297-12 ME05.SDR 05FDEA02857Web · crackedVERTICAL STABILIZER MAIN BOX WEB IS CRACKED AT FIN STA 133 JUST BELOW ACCESS CUTOUT. *S/D* INSTALLED DOUBLER AT FIN STA 133 PER EA 7-5530-91356.SDR SWAA052625Angle · crackedDURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER RT T/E ANGLE CRACKED AT RS 23.37. REMOVED AND REPLACED ANGLE PER SRM.SDR USAA051041Bushing · corrodedVERTICAL FIN AFT JUGS RT BUSINGS AFT FACES CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-55274, DEFECT SIZE: 1 X 2 INCH TYPICAL.SDR USAA051044Fitting · corrodedO/B ATTACH HOLE IN RT AFT DRAG BRACE ATTACH FITTING OFR VERTICAL FIN CORRODED. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED IAW EA 96816, DEFECT SIZE: 1 X 2 INCH TYPICAL.SDR USAA051042Bushing · corrodedVERTICAL FIN, AFT MOUNT LUGS LT SIDE BUSHINGS, FWD FACE CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA.SDR USAA051040Bushing · corrodedVERTICAL FIN AFT ATTACH LUGS RT SIDE FWD FACES. REMOVED CORROSION MACHINED & INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-52274 DEFECT SIZE: 1 X 2 INCHES TYPICAL.SDR USAA051037Attach Fitting · corrodedRIGHT AFT O/B VERTICAL FIN ATTACH LUG ON FUSELAGE. MACHINED AFT CHAMFER AND BOR TO CLEAN UP CORROSION & INSTALL NEW BUSHING IAW EA 96788, DEFECT SIZE .080 INCH DEEP.SDR USAA051043Bushing · corrodedVERTICAL FIN LT MOUNT LUGS, AFT FACE CORRODED. REMOVED CORROSION, FABRICATED & INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA.SDR SWAA052143Angle · corrodedDURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LEFT FWD AND RIGHT AFT DRAG ANGLES FACES CORRODED. REMOVED AND REPLACED DRAG ANGLES PER SRM.SDR DHL2005746521Structure · crackedC-CHECK VERTICAL FIN STA 133 LT STR 9 IS CRACKED AT ATTACH BOLT TO FRAME. REMOVE FASTENERS IAW B727 SRM 51-30-2, CUT OUT DAMAGE AREA DIM 9 1/2"X 3" AND FABBED FILLER FROM BAC15171367 PO 501963 DIM 9 1/2"X 3" AND ANGLE FROM 10134-1201 PO 501962 DIM 23"X 1 1/4"SDR DHL2005746522Structure · crackedVERTICAL STAB FIN STA 180 LT STR 9 IS CRACKED AT ATTACH BOLT TO FRAME. CUT OUT CRACKED SECTION OF STR 9 DI 4 1/2". FABBED FILLER P/N BAC1517-1367 PO 501963 4 1/2" 2EA ANGLE DOUBLERS P/N AND 10134-1201 PO 601952 18" IAW B727 SRM 55-30-4 FIG 1. TREATED AND PRSDR 2005FA0000886Shear Web · damagedREPAIRED FORWARD VERTICAL SHEAR WEB ASSY OF THE VERTICAL STABILIZER DUE TO HOLE ELONGATION. (K)SDR QXEA200500870Track · looseYYC - HORIZONTAL STABILIZER STEADY BLOCK FOR STAB TRIM TRACK IS LOOSE. REPAIRED IAW REO 670-55-11-024, HORIZON AIR EA R-55-34 AND CRJ-700 MM TASK 27-40-00-710-801-A01.SDR 05FDEA01055Fitting · corrodedVERTICAL FIN TENSION TIE RIB LEFT AFT VERT BOLT HOLE CORRODED A/C AND TENSION TIE SIDE. REPAIRED VERT FIN TENSION TIE RIB LT AFT VERT BOLT HOLE PER FED EX EA 7-5530-86280SDR 05FDEA01056Fitting · corrodedCORROSION VERT STAB TENSION TIE AFT SHEER FITTING UPPER SURFACE. REPAIRED VERTICAL FIN TENSION TIE AFT SHEAR FITTING PER FED EX EA. 7-5530-86280.SDR 05FDEA01045Shear Tie · tool damageVERTICLE STAB TENSION TIE FWD SHEAR TIE FITTING HAS PREVIOUS TOOLING MARKS. REPAIRED PER EA 7-5530-86281.SDR QXEA200500545Skin · gougedYYC - VERTICAL STABILIZER, SKIN BELOW BOTTOM AFT CORNER OF PANEL 325FR IS GOUGED IN TWO PLACES. REPAIRED IAW CRJ700 SRM 51-25-01-001-01-A01.SDR DHL2005782548Bracket · crackedVERT STAB FRAME CLIP CRACKED FIN STA 157.2 BETWEEN STR 8L AND 9L. REMOVED DAMAGED CLIP AT FIN STA 157.2 BETWEEN STR 8-9L IAW 727 SRM 51-30-2. FABBED NEW FROM 7075 T6 .050 PO NR 90014147 DIM 6 5/8" BY 3" IAW 727 SRM 55-30-2 FUG 2 NEW CLIP TREATED PRIMED AND ISDR DHL2005782544Web · crackedCRACKS IN WEBBING OF RIB LOCATED INSIDE THE BOTTOM END OF THE VERTICAL FIN BS 1303 (MARKED IN RED). JFEC INSPECTED WEB CRACK TERMINATED AT 1ST FASTENER HOLE IAW B727 NDT MAN PT 6 51-00-00 IIS 23, FABRICATED NEW DOUBLER REPAIR MATERIAL USED 7050 T6 .050 PO NR SDR DHL2005782504Stringer · crackedSTRINGER 9L CRACKED AT FIN STA 180.6 INSIDE VERTICAL FIN. REMOVED FASTENERS, CUTOUT DAMAGED AREA, FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 5 1/2" BY 3", SPLICE FROM AND 10133-1401 PO NR 501952 DIM 19 1/8" BY 2" SPLICE FROM 10134-1201 PO NR 501SDR DHL2005781549Stiffener · crackedDURING A C-CHECK,THE FOLLOWING DISCREPANCIES WERE NOTED; VERT STA FIN STA 180, STR 5-8 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGE, DIM 5 X 3 STIFFENER AND REMOVED FILLER IAW B 727 SRM 55-30-4 FIG 1. FABRICATED STIFFENESDR DHL2005781548Stiffener · crackedDURING A C-CHECK, VERT STAB FIN STA 180, STR 5-8 RT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED STIFFENERS AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1 (5 X 3). FABRICATED STIFFENER REPAIR P/N BAC1517-1367 PO 501953 DIM 5 SDR WRLA2005045Skin · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST RT BARREL NUT HOLE NR 29. (OPEN)SDR DHL2005781529Panel · dentedDURING A C-CHECK, VERT STAB RT SIDE TRAPIZOIDAL PANEL HAS 3 SHARP DENTS BELOW PREVIOUS REPAIR. CUT OUT DENTED AREA ON RT VERT TRAPAZOID PANEL APPROX 2 INCH DIA AND REMOVED PREVIOUS REPAIR APPROX 3 X 3.5 INCH, FABRICATED FILLERS, 1- APPROX 2 INCH DIA AND 2 - A
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