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 CALA9801650Strap · brokenINSPECTION FOUND RT VERTICAL STABILIZER SPAR ATTACH STRAP BROKEN IN HALF AT STA 1213. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-40-2 AND MM 51-20-11.SDR RRXA991011Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, VERTICAL STABILIZER, ATTACHMENT ANGLE BETWEEN STA 1750 AND STA 1790 AND LONGERON 2 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUSDR AALA981674Plate · corrodedTUL - RIGHT OUTBOARD VERTICAL STAB LUG BORE CORRODED AND BLENDED OUT OF LIMITS. LUG REPAIRED IAW 55-30-00-4 AND ESO 80559, DATED 9-1-98. (M)SDR AALA981673Lug · gougedTUL - LEFT OUTBOARD VERTICAL STAB LUG FRACE GOUGED AND CORRODED. REPLACED DAMAGED LUG PLATE WITH NEW PLATE FROM STOCK AND WORKED PER AARD 55-30-00-4. (M)SDR AALA981672Plate · gougedTUL - FOUND VERT STAB INBOARD LUG GOUGED AND SCORED LEFT SIDE. REWORKED AND BUSHED LUGS PER AARD 55-30-00-4. (M)SDR CALA9801543Bolts · corrodedINSPECTION FOUND FOUR VERTICAL STABILIZER TENSION TIE BOLTS CORRODED AT TOP OF STABILIZER. THE FOUR BOLTS WERE REMOVED AND REPLACED IAW SRM 55-20-00.SDR CALA9801504Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT ATTACH BOLT IN STRINGER 9R AT VERTICAL STABILIZER INNER COMPARTMENT NR 9 RIB. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-4. A REPAIR WAS INSTALLED IAW SRM 55-20-4, FIGURE 1, SHEET 5, AND SRM 51-10-2.SDR DL72S981903Stringer · crackedSTRINGER CRACKED VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 180.6 STA 9L. CRACK RUNS FROM HOLE TO EDGE OF PART. NO STOP DRILL REQUIRED. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. IK INSTALL. BEGAN INSTALL OF REPAIR PER M/M 55-30-0 FIG 803. FINISSDR DL72S981902Stringer · crackedSTRINGER CRACKED. VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 157.2 STR 8L. CRACK RAN FROM CTR OF HOLE TO EDGE OF STRINGER. FABRICATED REPAIR ANGLE PER MM 55-30-0 FIG 803 OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 FIG 803.SDR RRXA98411Stiffener · corrodedDURING A MAINTENANCE VISIT, FOUND VERTICAL STABILIZER, INNER SPAR STIFFENER WITH CORROSION BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKSDR CALA9801457Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN AFT FUSELAGE LEFT VERTICAL STABILIZER ATTACH ANGLE. THE ANGLE WAS REPLACED IAW EA 5340-01012.SDR DL72L981664Stringer · crackedA 1 INCH CRACK AT BOLT TO EDGE ON STR 8 FIN STA 157.2 RT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.SDR CALA9801433Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT ATTACH BOLT IN NR 7 STRINGER OF RT VERTICAL STABILIZER INNER COMPARTMENT AT NR 4 RIB. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4.SDR 98ZZZX3516Bolt · looseON DAILY SERVICE CHECK, 4 MOUNTING BOLTS FOR VERTICAL FIN WERE FOUND TO HAVE LOST TORQUE.SDR 98ZZZX3515Bolt · looseON DAILY SERVICE CHECK, 4 MOUNTING BOLTS FOR VERTICAL FIN WERE FOUND TO HAVE LOST TORQUE.SDR 98ZZZX3514Bolt · looseON PHASE INSPECTION FOUND 3 OF THE 4 VERTICAL FIN MOUNTING BOLTS LOST TORQUE.SDR 98ZZZX3513Bolt · looseON PHASE INSPECTION FOUND 3 OF THE 4 VERTICAL FIN MOUNTING BOLTS LOST TORQUE.SDR 98ZZZX3517Bolt · looseDURING DAILY SERVICE CHECK, FOUND UPPER AND LOWER AFT BOLTS TO HAVE LOST TORQUE.SDR SWAA981475Angle · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND ANGLE CRACKED AT BS 1128 TOP HALF OF STAB LT SIDE. REMOVED AND REPLACED PER BOEING SRM.SDR DL72W981529Stringer · crackedFOUND DURING C2 LETTER CHECK, CRACK AT FASTENER, VERT STAB STA 180.6 STR 10 LEFT SIDE AND CRACK AT FASTENER, VERT STAB STA 180.6 STR 9 LT SIDE. BOTH REPAIRED PER ERA 365310-14.SDR CALA9801280Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME ATTACH ANGLE INSIDE LT SIDE OF VERTICAL STABILIZER AT STRINGER 5L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.SDR CALA9801277Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STRINGERS 6L, 8L, AND 9L AT VERTICAL STABILIZER NR 9 RIB. THE CRACKED AREAS WERE CUT OUT IAW SRM 55-30-04. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 55-30-04 AND 51-10-2.SDR CALA9801276Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER NR 7 RIB LT NR 9 STRINGER. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-2. A STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 55-30-4.SDR 98ZZZX3366Vertical Fin · damagedDURING C/W ASB 407-98-17, THE VERTICAL FIN WAS FOUND DAMAGED BEYOND THE MAXIMUM LIMIT. ACTUAL DEPTH IS APPROXIMATE DEPTH OF .027 INCH. REPLACED FIN WITH NEW FIN P/N 206-020-113-255A S/N BP-2653.SDR HEEA0015124Fin · corrodedVERTICAL FIN CORRODED AND SEPARATED NEAR OUTBOARD MOUNTING HOLES. SCREWS SHEARED OFF IN UPPER CAP AREA.SDR UPS98827163Strap · corrodedINSPECTION TYPE-C, MODERATE CORROSION ON THE LT SIDE OF THE VERTICAL STAB TO EMP BASE STRIP. REPAIRED IAW SRM 53-2-5.SDR CALA9801145Pivot Plates · corrodedINSPECTION FOUND VERTICAL FIN RIGHT SIDE INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED IN SLEEVE BORE. THE INBOARD AND OUTBOARD SET OF PIVOT PLATES WERE REMOVED AND REPLACED IAW SRM 51-30-5.SDR DL72S981321Angle · crackedANGLE CRACKED INSIDE OF VERT STAB 4TH BAY DOWN FROM OPENING STR 5 ON RT SIDE CRACK IS ON VERT LEG. REMOVED FASTENERS, DRILLED OP REPAIR PARTS PER MM 55-30-0 PG 802. INSTALLED DOUBLER PER MM 55-30-0 PG 802.SDR C2XA98IA200Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE DRAG ANGLE AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATIOSDR ABXA9800525Bracket · crackedDURING C-CHECK, FOUND THE SUPPORT BRACKET FOR THE RIGHT VOR ANTENNA IN THE VERTICAL STABILIZER LEADING EDGE ASSY CRACKED. REPLACED SUPPORT BRACKET IAW DC9 SRM 51-30-2.SDR DL72S981320Stringer · crackedSTRINGER CRACKED INSIDE VERTICAL STAB 4TH BAY UP FROM ACCESS 9504 STR 8R. STOP DRILLED CRACK, DYE CHECKED PER PS900-6-3, NR 1 FABRICATED REPAIR PER M/M 53-30-0 FIG 803. INSTALLED DOUBLER PER MM 53-30-0 FIG 803.SDR DL72S981304Web · crackedVERT WEB CRACKED INSIDE STABILIZER ABOVE S-DUCT STA 1303. REPAIRED PER SRM 53-10-4 FIG 17, LT AND RT SIDE.SDR CALA9801109Panel · crackedINSPECTION FOUND VERTICAL STABILIZER PHENOLIC PANEL CRACKED AT STA 96. THE PANEL WAS REMOVED IAW SRM 51-30-2, A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 55-01, PAGE 1 AND 51-30-2.SDR MWEA98642Skin · chafedFOUND RIGHT AND LEFT LOWER AFT SKINS ON CANOE FAIRING CHAFED BEYOND LIMITS. MTC REMOVED AND REPLACED SKIN.SDR CALA9800978Fairing · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN RADIUS OF ATTACH FLANGE ON LT VERTICAL STABILIZER LOWER FAIRING. THE CRACKS WERE STOP DRILLED IAW SRM 51-01. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.SDR 98FDEA00394Angle · crackedUPPER VERTICAL FIN BASE ANGLE HAS CRACK INDICATION BETWEEN THE NR 4, 5 FASTENER HOLES FROM THE RT SIDE REF WC 8-553074303B1 - P1 EA 8-5530-3855 DATED 6/8/98 WRITTEN BASE ANGLE WILL BE REPETITIVE INSPECTED AT INTERVALS NOT TO EXCEED 1800 HRS. BASE ANGLE TO BE SDR SWAA981077Angle · wornDURING SCHEDULED D-CHECK, FOUND RT FUSELAGE TO VERTICAL STAB SKATE ANGLE WORN. REMOVED AND REPLACED PER BOEING SRM.SDR HEEA0014588Vertical Fin · mismanufacturedVERTICAL FIN UNIT RECEIVED IN UNSERVICEABLE CONDITION.SDR UPS98827055Web · crackedINSPECTION TYPE:C+S2 VERT STAB CLOSEOUT WEB AT ST ZR297 IS CRACKED. CLEANED AREA IAW DC8 SRM 51-1-8. PERFORMED HFEC IAW MIL-STD-271F ON VENT CLOSE OUT WEB ZR297 AFTER CLEANING AREA FOUND CORROSION AROUND RIVET. REMOVED RIVET IAW DC8 SRM 51-1-21. REMOVED COSDR UPS98827054Fitting · crackedINSPECTION TYPE:C+S2 VERT STAB AFT SPAR STA ZR297 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.SDR UPS98827469Strap · crackedINSPECTION TYPE-C/CK, VERTICAL STABILIZER TO FUSELAGE STRAP, RIGHT HAND SIDE HAS A CRACK AT FASTENERS HOLE FUSELAGE STATION 1765. FABRICATED REPAIR ANGLE AND FILLERS AND ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FILLER AND REPAIR ANGLE IAW DC8 SRM 51-SDR QXEA9800758Frame · crackedFRAME 67-2 CRACKED AT RIGHTHAND SIDE OF VERTICAL FIN BASE RIB WHERE ATTACHES TO COMPOSITE TAIL CONE. STOP DRILLED BUT DAMAGE EXCEEDS 1.02 MAXIMUM CRACK LIMIT. REPAIRED IAW HORIZON AIR EA 4-53-430.SDR DL72S981170Web · crackedSTA 1303 WEB CRACKED LT AND RT SIDE AT BOTTOM INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17.SDR CALA9800895Angle · crackedINSPECTION FOUND SEVERAL .75 INCH CRACKS IN LT VERTICAL STABILIZER ATTACH ANGLE ABOVE CANTED STA 1463. THE CRACKED AREAS WERE CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 23.SDR QXEA9800763Angle · crackedRIGHT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR (16 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.SDR DHL9870648CAngle · corrodedAT C-CHECK, VERTICAL STAB LT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. VERTICAL SUPPORT ANGLE CORRODED. INSTALLED NEW ANGLE PER SRM 55-30-1. N/R 4544.SDR DHL9870647CAngle · corrodedAT C-CHECK, VERT STAB RT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. REMOVED STRIP AND FOUND VERT ATTACH SUPPORT ANGLE CORRODED. INSTALLED NEW SUPPORT PER SRM 55-30-1. N/R 4545.SDR CALA9800848Skin · wornDORSAL FIN ATTACHMENT ANGLES FUSELAGE SKIN HAS SEVERAL OVERSIZED HOLES. REPAIRED PER EC/RA 5330-02660.SDR QXEA9800764Angle · crackedAFT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR IS CRACKED AND MISSING RIVET HEAD. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.SDR QXEA9800765Angle · crackedLEFT VERTICAL STAB CONNECTION ANGLE AT REAR SPAR IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1.
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