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 AT0100081Attach Angle · crackedFOUND RIGHT DORSAL FIN ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW EO 09-5350-29-E1645.Dec 26, 2000 · N846AT · Doug DC932SDR MWEA001245Fairing · crackedRH VERTICAL STAB SKIN UNDER AFT LOWER HORIZONTAL STAB FAIRING IS CRACKED. -- REPLACED SKIN.Dec 13, 2000 · N202ME · Doug DC932SDR DHL200080233CAngle · crackedAT C CHECK; VERTICAL STAB. L/E INTERIOR ANGLE CRACKED (1/2 INCH) AT STA ZFS 179.750. PERFORMED STOP DRILL IAW SRM 55-2-0 FIG 2, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-0, FIG 2. REF: N/R 2811.Dec 6, 2000 · N802DH · Doug DC873FSDR QXEA0003364Skin · dentedPDX- LEFT HAND VERTICAL STABILIZER OUTBOARD SKIN DENTED 17 INCHES AFT OF FRONT SPAR AND 12 INCHES AFT OF BEACON RIB 3.4. REPAIRED IAW FOKKER SRM 51-70-0, 55-01-01, AND HORIZON AIR EA 4-55-270.Dec 3, 2000 · N492US · Fokker F28MK4000SDR QXEA0003362Skin · damagedPDX- VERTICAL STABILIZER OUTER SKIN HAS 4 WORKING FASTENERS AT INTERMRDIATE SPAR 1 BOTTOM RIGHT HAND SIDE. REPAIRED IAW FOKKER SRM 51-30-02.Nov 30, 2000 · N492US · Fokker F28MK4000SDR QXEA0003249Angle · crackedPDX- VERTICAL STABILIZER LEFT HAND LOWER CONNECTION ANGLE AT INTERMEDIATE SPAR II HAS A CRACK RUNNING THROUGH HI-LOCK HOLE ON UPPER FLANGE OF ANGLE. REPAIRED IAW FOKKER SRM 55-31-00 PAGE 2.Nov 30, 2000 · N492US · Fokker F28MK4000SDR L1GA200000385Fairing · crackedCRACK FWD UPPER EDGE OF LT LWR HORIZ STAB FAIRING PANEL. INSTALLED STACKED ANGLE REPAIR.Nov 14, 2000 · N12510 · Doug DC932SDR L1GA200000384Fairing · chafedLOCALIZED CHAFING VERTICAL STAB TIP CAP FAIRING LT END. BLENDED, TREATED AND PRIMED.Nov 14, 2000 · N12510 · Doug DC932SDR COMA0060918Bushing · wornVERTICAL STABILIZER RIGHT HORIZONTAL STABILIZER PIVOT BUSHING WORN. REMOVED WORN BUSHING. VERIFIED RT VERT LUG BORE TO BE IN TOLERANCE AT 1.7001 INCH. MACHINED FLANGE OF BUSHING P/N 600-21061-7 TO .070 INCH IAW WVAC EO 601R-55-1903A. INSTALLED BUSHING IAW Nov 13, 2000 · N936CA · Cndair CL6002B19SDR COMA0060916Bushing · wornVERTICAL STABILIZER LEFT HORIZONTAL STABILIZER PIVOT BUSHING WORN. REMOVED WORN BUSHING. VERIFIED LT VERT LUG BORE TO BE OUT OF LIMITS AT 1.7020 INCH. TOOK 1ST OVERSIZE BUSHING P/N 601R55-31-002-5 AND MACHINED AND CAD PLATED IAW REO 601R-55-31-026 CHANGING Nov 13, 2000 · N936CA · Cndair CL6002B19SDR CALA0001682Attach Angle · crackedINSPECTION FOUND A 1.125 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1463. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23.Nov 2, 2000 · N14814 · Doug DC982SDR LR7A00200Skin · corrodedDURING SCHEDULED C2 CHECK PER JOB CARD HC2704, FOUND FS 1066 LOWER HORIZONTAL STAB SKIN CORRODED AT LBL 6 - RBL 28. REPAIRED IAW LAC MEA 382-55-00-135.Nov 1, 2000 · N403LC · Lkheed 382GSDR AWXA0000808Angle · chafedC-CHECK, FUSELAGE TO VERTICAL STAB SUPPORT ANGLE, LEFT HAND SIDE, 19 INCHES FWD OF RUDDER, CHAFED BEYOND LIMITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS IAW 737 SRM 51-70-11, FAB''D REPAIR PARTS IAW 737 SRM 51-40-08, TREATED AND PRIMED PARTS IAW 737 SOct 31, 2000 · N155AW · Boeing 7373G7SDR COMA0060845Bushing · dislodgedLEFT HAND AND RIGHT HAND VERTICAL STABILIZER BUSHINGS ARE MIGRATED AT HORIZONTAL STABILIZER PIVOT POINT. REMOVED MIGRATED BUSHINGS. INSTALLED NEW BUSHINGS P/N 600-21061-7 (THAT WERE MACHINED IAW WVAC EO 601R-55-1834) IAW CRJ AMM 20-26-00-910-803. REAMED TO Oct 24, 2000 · N960CA · Cndair CL6002B19SDR COMA0060844Bushing · scoredLEFT HAND AND RIGHT HAND VERTICAL STAB TOP BUSHINGS ARE SCORED, WHERE HORIZONTAL STABILIZER ATTACHED. REMOVED SCORED BUSHINGS AND INSTALLED NEW BUSHINGS ON LEFT HAND AND RIGHT HAND SIDES IAW CRJ AMM 20-16-00-910-803. BUSHINGS WERE MACHINED IAW WVAC EO O 601ROct 24, 2000 · N927CA · Cndair CL6002B19SDR F3LA200000252Web · chafedDURING C-5 CHECK, INSPECTION REPORTED VERTICAL STABILIZER FORWARD BULKHEAD AT STA 1010 DAMAGED. REMOVED AND REPLACED DAMAGED WEB PER SRM 51-30-2 AND BOEING DRAWING 65-52913.Oct 23, 2000 · N237TR · Boeing 737228SDR QXEA0002984Angle · crackedPDX- LEFT VERTICAL STABILIZER CONNECTION ANGLE IS CRACKED AT INTERMEDIATE SPAR 2. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, AND SRM 51-31-01.Oct 19, 2000 · N483US · Fokker F28MK4000SDR QXEA0002983Angle · crackedPDX-LEFT SIDE VERTICAL STABILIZER CONNECTION ANGLE IS CRACKED IN RADIUS BELOW INTERMEDIATE SPAR 1. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, SRM 51-31-01.Oct 19, 2000 · N483US · Fokker F28MK4000SDR C2XAOOIA391Bearing · corrodedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED BEARING IN ACCORDANCE WITH EMB145 MM55-37-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 18, 2000 · N12934 · Emb EMB145SDR CALA0001597Attach Angle · crackedINSPECTION FOUND A .5 INCH CRACK AT AFT END OF RT VERTICAL STABILIZER ATTACH ANGLE, STA 1485. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.Oct 18, 2000 · N16883 · Doug DC981SDR C2XAOOIA394Skin · crackedREFERENCE OPEN SDR C2XAOOIA383 DURING C-CHECK INSPECTION, THE LEFT HAND SKIN ON THE VERTICAL STABLILIZER WAS FOUND TO BE CRACKED. MX PERFORMED AN INSERTION REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANMGE EC5530-01045, AND A/C WAS APPROVED FOROct 17, 2000 · N12934 · Emb EMB145SDR C2XA00IA394Skin · crackedREFERENCE OPER SDR C2XA00IA383-DURING C-CHECK INSPECTION, THE LEFT HAND SKIN ON THE VERTICAL STABILIZER WAS FOUND TO BE CRACKED. MX PERFORMED INSERTION REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING EC5530-01045, AND A/C WAS APPROVED FOR RETURN TO SOct 17, 2000 · N12934 · Emb EMB145SDR COMA0060826Bushing · shiftedDURING REMOVAL OF HORIZONTAL STABILIZER, FOUND LEFT HAND VERTICAL STAB BUSHING MIGRATED. PERFORMED A MAJOR REPAIR BY REPLACING LEFT HAND VERTICAL STAB BUSHING IAW CRJ REO 601R-55-31-013, 601R-55-31-002 AND CRJ AMM 20-26-00-910-803.Oct 17, 2000 · N987CA · Cndair CL6002B19SDR COMA0060825Bushing · shiftedRIGHT HAND VERTICAL STAB BUSHING WAS FOUND MIGRATED .012 INCH DURING ACCOMPLISHMENT OF COMAIR EO 55-007R1. PERFORMED A MAJOR REPAIR BY INSTALLING BUSHING (P/N 600-21061-7) IN RT VERTICAL STAB LUG IAW WVAC EO 601R-55-1774 AND CRJ AMM 20-26-00-910-803.Oct 17, 2000 · N987CA · Cndair CL6002B19SDR QXEA0002988Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING LEFT UPPER LUG HAS FRETTING CORROSION ON BOTH SIDES OF LUGS. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND HORIZON AIR EA 4-55-493.Oct 15, 2000 · N483US · Fokker F28MK4000SDR QXEA0002987Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING LEFT LOWER LUG HAS FRETTING CORROSION ON INBOARD SIDE OF LUG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND HORIZON AIR EA 4/55/493.Oct 15, 2000 · N483US · Fokker F28MK4000SDR QXEA0002986Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING RIGHT UPPER LUG HAS FRETTING CORROSION ON BOTH SIDES OF LUG. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-55-493.Oct 15, 2000 · N483US · Fokker F28MK4000SDR QXEA0002985Fitting · corrodedPDX- HORIZONTAL STABILIZER JUNCTION FITTING RIGHT LOWER LUG HAS FRETTING CORROSION ON BOTH SIDES OF LUG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND HORIZON AIR EA 4-55-493.Oct 15, 2000 · N483US · Fokker F28MK4000SDR COMA0060824Bushing · shiftedRIGHT HAND VERTICAL STAB BUSHING WAS FOUND TO BE MIGRATED AND LEFT HAND VERTICAL STAB BUSHING WAS FOUND TO BE STRIPPED. PERFORMED A MAJOR REPAIR BY REPLACING BUSHINGS IN VERTICAL STAB WITH (P/N 600-21061-7) IAW WVAC EO 601R-55-1769A.Oct 14, 2000 · Cndair CL6002B19SDR P5CA0000329Structure · corrodedLEVEL 1 CORROSION FOUND ON VERTICAL FIN 4TH BALANCE WEIGHT (COUNTING FROM TOP TO BOTTOM). CORROSION TREATMENT PER CPM PART 1, 20-40-00 P.24 C/OUT WEIGHT REINSTALLED, MM 20-51-01.Oct 13, 2000 · N806FT · Boeing 747249FSDR DHL200080736CFitting · crackedAT C-CK; VERTICAL STAB INTERNAL FITTING CRACKED 2 INCHES AT STA ZR320.23G. REMOVED CRACKED FITTING IAW SRM 51-1-21, PG 1, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-21, PG 1. REF: N/R 0792.Oct 11, 2000 · N807DH · Doug DC873SDR DL72L002084Web · crackedAT HMV, THE WEB ON THE VERTICAL FIN WAS FOUND CRACKED. REMOVED FASTENERS AND BEGAN FABR DOUBLER PER SRM 53-10-4D FIG 802D. STOP DRILLED CRACKS, COMPLETED FABR OF DOUBLER, DYE CKED, INSTALLED DOUBLER PER SRM 53-10-4D FIG 802D.Oct 5, 2000 · N508DA · Boeing 727232SDR ASAA0080632Attach Angle · crackedOAK - DURING SCHEDULED C-CHECK, A CRACK FOUND IN THE LEFT HORIZONTAL LEG OF THE LEFT DORSAL FIN ATTACH ANGLE AT STATION 1485. REPAIRED PER EA 5530-01065. (M)Oct 3, 2000 · N934AS · Doug DC982SDR 20001026SH030Angle · crackedDURING A ROUTINE MAINTENANCE C-CHECK, A CRACK WAS FOUND ON THE RIGHT SIDE OF THE VERTICAL STABILIZER CHINE ANGLE AT STA 16128.0, .250 INCH LONG AT ONE. (X)Sep 29, 2000 · N232AS · Emb EMB120RTSDR 20001013SH008Fitting · crackedTEE SHAPED FITTING ON THE TRAILING EDGE OF THE FIN WAS CRACKED ON THE RIGHT SIDE IN THE RADIUS. (X)Sep 21, 2000 · N4713B · Cessna 152SDR CALA0001399Angle · crackedINSPECTION FOUND FOUR VERTICAL STABILIZER DOGHOUSE ANGLES CRACKED. LOCATIONS WERE RT AND LT FWD LOWER AND RT AND LT AFT LOWER AREA. THE CRACKS WERE .5 INCH LONG. THE ANGLES WERE REPAIRED IAW SRM 55-01, FIGURE 2, 55-10-4, 51-10-3, AND 51-30-2.Sep 5, 2000 · N15841 · Doug DC982SDR P2EA00247Fitting · gougedMCI - DURING COMPLIANCE OF VANGUARD EO NR 993753A43, FOUND THE LEFT INBOARD 1088 VERTICAL LUG FITTING LOWER INBOARD HOLE WITH STEEL BUSHING INSTALLED. REPAIRED THE LEFT INBOARD 1088 VERTICAL LUG FITTING LOWER INBOARD HOLE IAW BOEING MESSAGE NR VAG-MCI-00-0009Sep 2, 2000 · N620PC · Boeing 737244SDR P2EA00246Fitting · gougedMCI - DURING COMPLIANCE OF VANGUARD EO NR 993753A43, FOUND THE LEFT OUTBOARD 1088 VERTICAL LUG FITTING UPPER OUTBOARD HOLE GOUGED, LEFT .392 INCH, WIDTH .156 INCH, DEPTH .030 INCH. REPAIRED THE LEFT OUTBOARD 1088 VERTICAL LUG FITTING UPPER OUTBOARD HOLE IAW BSep 2, 2000 · N620PC · Boeing 737244SDR USAA001433Angle · crackedPIT - FOUND DRAG ANGLE CRACKED .25 INCH, VERT FIN LEFT DOOR DRAG ANGLE HORIZ LEG STATION 1463. INSTALLED DOUBLER PER SRM 53-05 FIG 23A. (M)Aug 24, 2000 · N800US · Doug DC981SDR USAA001434Angle · crackedPIT - FOUND DRAG ANGLE CRACKED .75 INCH AND 2 INCHES, LEFT DRAG ANGLE VERT LEG AND HORIZ LEG DORSAL FIN. INSTALLED DOUBLER PER SRM 53-05 FIG 23A. (M)Aug 24, 2000 · N800US · Doug DC981SDR DL72K001632Angle · crackedFOUND ON C2 LETTER CK,1 INCH CRACK IN BULKHEAD TO STR ATTACH ANGLE INSIDE VERT STAB AT STR 9L. REPAIRED PER MM 55-30-0.Aug 23, 2000 · N523DA · Boeing 727232SDR USAA001299Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, AFT SPAR, AFT OUTBOARD CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7SDR USAA001297Clevis · corrodedCLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, AFT CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7SDR USAA001296Clevis · corrodedCLT - FOUND AFT SPAR CLEVIS CORRODED .013 INCH BY .028 INCH, VERT FIN, AFT SAPR, AFT OUTBOARD CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)Aug 22, 2000 · N282AU · Boeing 7372B7SDR COMA0060691Bushing · wornTHE VERTICAL STABILIZER LEFT HAND AND RIGHT HAND PIVOT BUSHINGS (P/N 600-21061-5) WERE FOUND WORN DURING ACCOMPLISHMENT OF COMAIR EO 55-007. PERFORMED A MAJOR REPAIR BY INSTALLING BUSHINGS (P/N 600-21061-7) TO LEFT HAND AND RIGHT HAND VERTICAL STABILIZER PIVOAug 22, 2000 · N810CA · Cndair CL6002B19SDR GAIA00498Rib · damagedFOUND DURING ROUTINE SCHEDULED MAINTENANCE AT TIMCO/OSC, VERTICAL STAB CLOSURE REQUIRES SPOT FACING IAW S/B 727-55-071, REF NR 20880. REWORKED STAB CLOSURE RIB IAW B727 S/B 55-0071. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 7, 2000 · N279US · Boeing 727251SDR COMA0060637Bushing · scoredVERTICAL STABILIZER HINGE BUSHINGS P/H 600-21061-5 WERE FOUND SCORED DURING INCORPORATION OF COMAIR EO 55-007 (HORIZONTAL STABILIZER PIVOT POINT LUBRICATION). PERFORMED A MAJOR REPAIR BY INSTALLING BUSHINGS 2 EA P/H 600-221061-7 IN VERTICAL STABILIZER HINGES Aug 7, 2000 · N806CA · Cndair CL6002B19SDR RRXA003823Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H SIDE VERTICAL STAB. BASE, 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, 55-2-Aug 4, 2000 · N811AL · Doug DC871SDR UPS00434127Beam · crackedINSPECTION TYPE:C, VERTICAL STABILIZER T/E CRACK ON TRAILING EDGE BEAM AT FIN STA 245 RT. REPAIRED TRAILING EDGE BEAM WEB IAW SRM 55-30-06.Aug 4, 2000 · N691UP · Boeing 747121SDR CALA0001198Web · crackedINSPECTION FOUND A .25 INCH CRACK IN WEB SKIN AT RT SIDE OF TAIL COMPARTMENT STA 1485, JUST FORWARD OF RUDDER TRIM. THE WEB AND ANGLE WERE REMOVED AND THE CRACKED AREA WAS REMOVED IAW SRM 51-30-2 AND 55-01, FIGURE 4. DOUBLERS AND AN ANGLE WERE INSTALLED IAW Aug 2, 2000 · N72825 · Doug DC982
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