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.

SDR COMA0060622Bushing · damagedDURING ACCOMPLISHMENT OF BOMBARDIER AEROSPACE IN-SERVICE LETTER RJ-SL-55-001, FOUND LT & RT VERTICAL STABILIZER BUSHINGS TO BE DAMAGED (SCORING AND CALLED). PERFORMED A MAJOR REPAIR BY REPLACING LT & RT VERTICAL STABILIZER BUSHINGS IAW CRJ AMM 20-26-00-910-80Aug 2, 2000 · N812CA · Cndair CL6002B19SDR QXEA0002227Angle · loosePDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE HI-LOKS AT FRONT SPAR. REPAIRED IAW FOKKER SRM 51-30-02.Jul 30, 2000 · N484US · Fokker F28MK4000SDR QXEA0002226Angle · loosePDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE AND SMOKING HI-LOKS AT SPAR 1. REPAIRED IAW FOKKER SRM 51-30-02.Jul 30, 2000 · N484US · Fokker F28MK4000SDR QXEA0002224Angle · crackedPDX- RIGHT VERTICAL CONNECTION ANGLE CRACKED AT HI-LOK HOLES AT SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00.Jul 30, 2000 · N484US · Fokker F28MK4000SDR QXEA0002222Angle · crackedPDX- LEFT HAND VERTICAL CONNECTION ANGLE CRACKED AT HI-LOK HOLES AT SPAR 1. REPAIRED IAW FOKKER SRM 55-31-00.Jul 30, 2000 · N484US · Fokker F28MK4000SDR QXEA0002221Angle · crackedPDX- LEFT VERTICAL CONNECTION ANGLE CRACKED AT HI-LOK HOLES AT SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00.Jul 30, 2000 · N484US · Fokker F28MK4000SDR RRXA003822Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BASE OF VERTICAL STAB. R/H SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 55Jul 27, 2000 · N811AL · Doug DC871SDR UPS00434083Beam · crackedINSPECTION TYPE:C, TAIL VERTICAL STABILIZER T/E BEAM SUPPORTS FOUND CRACKED AT RUD STA 132 LT, RT, 157 LT, 267 LT RT ,282 LT & RT, 307 LT & RT, 332 RT AND 367 RT. REPAIRS TO STAB (VERTICAL) T/E BEAM SUPPORTS REPAIRED IAW SRM 51-40-03 AND Q/NOTE 54/2000 CLOSUJul 26, 2000 · N691UP · Boeing 747121SDR UPS00833604Fitting · corrodedINSPECTION TYPE:C123, VERTICAL STAB NR 3 RUDDER DAMPER ATTACH POINT FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3651256, AND SRM 51-3-0.Jul 24, 2000 · N806UP · Doug DC873FSDR UPS00833535Frame · crackedINSPECTION TYPE:C123, VERTICAL STAB L/E FORMER IS CRACKED AT ZFS 171 LEFT SIDE. REPAIRED FORMER IAW SRM 55-2-0 FIG 2.Jul 23, 2000 · N806UP · Doug DC873FSDR COMA0060593Bushing · wornHORIZONTAL AND VERTICAL STABILIZER BUSHINGS ARE WORN. REPAIRED HORIZONTAL AND VERTICAL STABILIZER BUSHINGS IAW REO 601R-55-11-22 REV A AND WVAC EO 601R-55-1521.Jul 22, 2000 · N809CA · Cndair CL6002B19SDR TWAA0011602Attach Angle · misrepairedDURING CHECK-C MAINT, FOUND THE VERTICAL STABILIZER ATTACH ANGLE PARTIALLY REPAIRED PER SRM 53-05, FIG 23A, AND REQUIRED PERMANENT REPAIR ATTACH ANGLE PER SRM 53-09 FIG 23A AT NEXT OP 15 PER ARA 15695 DATED 6-23-98. REPAIRED PER SRM 53-05, FIG 23A.Jul 19, 2000 · N901TW · Doug DC982SDR AT0000351Structure · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND VERTICAL STABILIZER TOP FAIRING LOWER FORWARD MOUNT POINTS CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-04, 51-10-03, 53-11-01, AND 51-30-05.Jul 18, 2000 · N845AT · Doug DC932SDR USAA001058Attach Fitting · gougedPIT - FOUND FORWARD ATTACH LUG GOUGED, 1 INCH SEMI CIRCLE .025 INCH DEEP, FS 81.10 STANDBY ACT FORWARD ATTACH BOLT FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)Jul 17, 2000 · N517AU · Boeing 7373B7SDR CA000731015Fitting · cracked(CAN) AN A INSPECTION WAS BEING ACCOMPLISHED ON THE AIRCRAFT. DURING THIS INSPECTION, A CRACK WAS FOUND ON THE AFT VERTICAL STABILIZER ATTACH FITTING. THE CRACK WAS CONFIRMED USING EDDY CURRENT INSPECTION METHOD. AFTER THE FITTING WAS REMOVED FROM THE STABIJul 17, 2000 · Piper PA60600SDR 00FDEA00482Fitting · oversizedEMPENNAGE, WITH REF E1-5510-7-3304 1 PT2 STEP 9 & 18, (FIG 3, SHT 6, CIRCLE STEP 6) 6 HOLES (3 PLACES LT, 3 PLACES RT) FOUND WITH EXISTING COUNTERSINK 100 X 0.610 DIAMETER (100 X 0.512 DIAMETER REQ''D). REPAIRED PER EA 1-5530-52023. STAB - VERT STAB LT AND RTJul 12, 2000 · N584FE · Doug MD11SDR 20000810SH018Angle · crackedDURING A ROUTINE MAINTENANCE C-CHECK, CRACKS WERE FOUND ON THE LEFT SIDE OF THE VERTICAL STABILIZER CHINE ANGLE BETWEEN STA 16128.0 AND STA 16144.9 AT 3 WORKING RIVETS. POSSIBLE CAUSE. FATIGUE/VIBRATION. SUBMITER RECOMMENDED A DETAILED INSPECTION CALL OUT DJul 11, 2000 · N260AS · Emb EMB120RTSDR DHL200070919CHousing · crackedVERT STAB RT SIDE DUCT HOUSING STA 1307 APPROX HAS SEVERAL CRACKS (DUCT MATES TO VERT STAB FRONT SPAR). CUT OUT DAMAGED AREA PER SRM 51-40-2. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 55-30-3. ALODINED AND PRIMED PER SRM 51-10-2.Jul 11, 2000 · N709DH · Boeing 72782CSDR QXEA0001901Fastener · loosePDX- LOOSE AND SMOKING HI-LOKS AND CRACKS IN FASTENER HOLE AT LEFT HAND VERTICAL CONNECTION ANGLE SPAR 1. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.Jul 9, 2000 · N491US · Fokker F28MK4000SDR QXEA0001900Fastener · loosePDX- LOOSE AND SMOKING HI-LOKS AND CRACK IN RADIUS OF LEFT HAND VERTICAL STABILIZER CONNECTION ANGLE FRONT SPAR. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.Jul 9, 2000 · N491US · Fokker F28MK4000SDR QXEA0001904Fastener · loosePDX- LOOSE AND SMOKING HI-LOKS AT RIGHT VERTICAL CONNECTION ANGLE FRONT SPAR. REPAIRED IAW FOKKER SRM 51-30-02 AND HORIZON AIR EA 4-55-233.Jul 7, 2000 · N491US · Fokker F28MK4000SDR 0002469938Angle · crackedCRACK .5 INCH LONG OMITTING FROM FASTENER HOLE. REPAIRED PER EA 99-172550 L/P 1462156.Jul 6, 2000 · N1798U · Doug DC931SDR SWAA001193Drag Brace · corrodedDURING SCHEDULED D CHECK, FOUND RT VERTICAL STAB AFT SPAR, FWD AND AFT DRAG BRACES CORRODED. R&R DRAG BRACES PER MM.Jun 30, 2000 · Boeing 7372H4SDR QXEA0001905Fastener · loosePDX- LOOSE AND SMOKING HI-LOKS AT RIGHT VERTICAL CONNECTION ANGLE SPAR 1. REPAIRED IAW FOKKER SRM 51-30-02.Jun 29, 2000 · N491US · Fokker F28MK4000SDR QXEA0001903Fastener · loosePDX- LOOSE AND SMOKING BUTTON HEAD AND HI-LOK RIVETS LEFT SIDE AFT SPAR VERTICAL CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02.Jun 29, 2000 · N491US · Fokker F28MK4000SDR QXEA0001902Fastener · loosePDX- LOOSE AND SMOKING HI-LOK AT LEFT VERTICAL CONNECTION ANGLE SPAR 2. REPAIRED IAW FOKKER SRM 51-30-02.Jun 29, 2000 · N491US · Fokker F28MK4000SDR SWAA001181Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING LT FWD LUG, AND LT / RT AFT LUGS CORRODED. REPAIRED FITTING PER ER NR 00-657.Jun 29, 2000 · Boeing 7372H4SDR QXEA0001907Fastener · loosePDX- LOOSE AND SMOKING BUTTON HEADS AND HI-LOKS AT RIGHT VERTICAL CONNECTION ANGLE AFT SPAR. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02.Jun 28, 2000 · N491US · Fokker F28MK4000SDR QXEA0001906Fastener · loosePDX- LOOSE AND SMOKING HI-LOKS AT RIGHT VERTICAL CONNECTION ANGLE SPAR 2. REPAIRED IAW FOKKER SRM 51-30-02.Jun 28, 2000 · N491US · Fokker F28MK4000SDR UPS00233224Support Fitting · corrodedINSPECTION TYPE: C+SI, RT STABILIZER HINGE BEARING OB SUPPORT LUG SHOWS CORROSION INDICATION DURING HFEC INSPECTION. CORROSION REMOVED AND LUG REWORKED, COMPLETED IAW EO B727-5510-2284 APPEX B.P6 3-7 (F)-(J).HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-0 Jun 15, 2000 · N954UP · Boeing 727185CSDR UPS00833309Stiffener · corrodedINSPECTION TYPE:C123, VERTICAL STAB TOP STA ZY284 T/E WEB STIFFENER L-ANGLE HAS CORROSION FWD SIDE OF WEB. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. MAT ID PO 331530 S1646835 PER DC8 DRWG 5611400. FAB STIFFENER IAW DC8 DRWG 5611400. Jun 12, 2000 · N708UP · Doug DC871FSDR QXEA0001743Angle · crackedPDX-LOOSE HI-LOKS AT RIGHT HAND VERTICAL CONNECTION ANGLE AT SPAR 1, POSSIBLE CRACKS AT FASTENER HOLE. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.Jun 9, 2000 · N496US · Fokker F28MK4000SDR QXEA0001742Angle · crackedPDX- LOOSE HI-LOKS AND POSSIBLE CRACK AT HOLES RIGHT HAND VERTICAL CONNECTION ANGLE, SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.Jun 9, 2000 · N496US · Fokker F28MK4000SDR QXEA0001741Angle · crackedPDX- LOOSE HI-LOKS AND CRACK IN RADIUS AT FRONT SPAR RIGHT SIDE VERTICAL CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.Jun 9, 2000 · N496US · Fokker F28MK4000SDR QXEA0001739Angle · crackedPDX- LOOSE HI-LOKS AND POSSIBLE CRACKS AT FASTENER HOLES LEFT HAND VERTICAL CONNECTION ANGLE, SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2.Jun 9, 2000 · N496US · Fokker F28MK4000SDR QXEA0001744Rivet · loosePDX- ELEVEN RIVETS ALONG THE AFT SPAR OF VERTICAL STAB AFT OF PANEL 56A ARE LOOSE. REPAIRED IAW FOKKER SRM 51-31-01.Jun 8, 2000 · N496US · Fokker F28MK4000SDR QXEA0001740Angle · crackedPDX- LOOSE HI-LOKS AND POSSSIBLE CRACKS AT FASTENER HOLES LEFT HAND VERTICAL CONNECTION ANGLE, SPAR 1. REPAIRED IAW FOKKER SRM 55-31-00.Jun 8, 2000 · N496US · Fokker F28MK4000SDR RAAA00B1067Angle · corrodedDURING SCHEDULED C2 CHECK, FOUND CORROSION VERTICAL FIN STA 87.00 TRAILING EDGE CHORD LT AND RT SKIN ATTACH ANGLES. CORROSION BEYOND LIMIT. REPAIRED EXTRUDED PARTS IAW SRM 51-40-4, 51-30-2 & 3.Jun 2, 2000 · N831RV · Boeing 72722CSDR QXEA0001627Rivet · looseYYC- VERTICAL STABILIZER TRAILING EDGE HAS LOTS OF LOOSE RIVITS. REPAIRED IAW FOKKER SRM 51-31-01 AND 55-31-01 FIGURE 1.May 24, 2000 · N480AU · Fokker F28MK4000SDR AWXA0000329Structure · crackedC-CHECK, VERT STAB UPPER RUDDER HINGE POINT RT STRUCTURE HAS CRACK AT CORNER. REMOVED DAMAGED CORNER COVER, FABRICATED REPAIR COVER IAW 737 SRM 51-30-30, 51-20-02, AND 51-40-02, TREATED AND PRIMED IAW 737 SRM 51-20-06, INSTALLED IAW 737 SRM 51-40-02.May 23, 2000 · N304AW · Boeing 7373G7SDR C2XA00IA135Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01032May 21, 2000 · N14960 · Emb EMB145SDR C2XA00IA134Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01032,May 21, 2000 · N14960 · Emb EMB145SDR RRXA002773Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERT STAB LOWER L/E FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0, 51-1-4 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871FSDR RRXA002772Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERT STAB CENTER L/E FRAME AT ZFS 267, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871FSDR RRXA002771Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERT STAB CENTER L/E FRAME AT ZFS 1797, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 55-2-0 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871FSDR C2XA00IA122Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EA5330-01032May 12, 2000 · N14950 · Emb EMB145LRSDR C2XA00IA121Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINGEERING CHANGE AND REPAIR AUTHORIZATION EA5330-01032May 12, 2000 · N14950 · Emb EMB145LRSDR ABXA000256Angle · crackedRIGHT DORSAL FIN ATTACH ANGLE CRACKED FORWARD OF AFT END OF ANGLE, 12 INCHES LONG. REPAIRED ANGLE IAW DC9 SRM 53-05, FIGURE 23.May 10, 2000 · N951AX · Doug DC941SDR 00FDEA00321Fitting · crackedSNRM 587 CRACK AT LT SIDE FWD RADIUS. SNRM 588 RT SIDE FWD RADIUS. *S/D* REMOVED AND REPLACED PER SRM 55-20-00 FIG 3 VOL 1 AND EA 1-5530-49647.May 3, 2000 · N601FE · Doug MD11FSDR CALA0000608Clip · crackedVERTICAL STAB LOWER AFT SPAR LEFT SIDE CLIP IS CRACKED (1). REMOVED AND REPLACED CLIP PER SRM 51-30 AND 51-30-05.May 2, 2000 · N71828 · Doug DC982
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