JASC 5553

Service difficulty reports · 586

Reports filed under 5553 · Vertical Stabilizer, Attach Fittings, 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 = '5553'
  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 SWAA011115Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERT STAB FWD PRIMARY CLEVIS, FACE & BORE, CORRODED. REPAIRED FITTING PER BFG ER.Apr 10, 2001 · N355SW · Boeing 7373H4SDR SWAA011114Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND VERT STAB AFT PRIMARY CLEVIS, AFT LUG FACE AND BORE, CORRODED. REPAIRED FITTING PER BFG ER.Apr 10, 2001 · N355SW · Boeing 7373H4SDR AWXA0001571Fitting · damagedDURING MAINTENANCE CHECK REMOVAL OF BOLT, RIGHT O/B FWD VERT FIN ATTACH LUG BOLT HOLE WAS DAMAGED AT FS 1088. REMOVED AND REPLACED LUG AWA ER 15-5383-00029-JS1A.Apr 2, 2001 · N179AW · Boeing 737277SDR COMA0160353Bushing · wornRT VERTICAL STAB BUSHING IS MIGRATED AT HORIZ STAB PIVOT POINT. REMOVED MIGRATED BUSHING. MACHINED FLANGE OF NEW BUSHING P/N 600-21061-7 TO .077 IAW WVAC EO 601R-55-2353. INSTALLED MACHINED BUSHING IAW CRJ AMM 20-26-0-910-803. REAMED BUSHING TO TOLERANCE 1Mar 31, 2001 · N981CA · Cndair CL6002B19SDR COMA0160355Bushing · wornRIGHT VERT STAB BUSHING AT HORZ STAB PIVOT POINT WORN. REMOVED AND REPLACED BUSHING P/N 601R-55-31-001-5 IAW CRJ AMM 20-26-00-910-803. MACHINED BUSHING IAW WVAC EO 601R-55-2345. BORE WITHIN TOLERANCE IAW CRJ DRAWING 600-21058. REAMED BUSHING IAW CRJ DRAWINMar 28, 2001 · N941CA · Cndair CL6002B19SDR COMA0160308Bushing · out of positionRT VERT STAB BUSHING IS MIGRATED AT HORIZONTAL STAB ATTACH POINT. REMOVED MIGRATED BUSHING. INSTALLED BUSHING P/N 600-21061-7 (THAT WAS MACHINED IAW WVAC EO 601R-55-2291) IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING IAW DWG 600-21029.Mar 10, 2001 · N719CA · Cndair CL6002B19SDR AWXA0001354Fitting · corrodedRIGHT O/B FWD LUG OF AFT VERT STAB ATTACHMENT CORRODED IN BORE. VERT STAB REMOVED AND INSTALLED IAW W/C R6B55001 & F6B27001, MAIN CHORD FITTING REWORKED IAW ER 03-5384-01033-BA1 & WIP 0192290.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001353Fitting · corrodedRIGHT O/B AFT FUSELAGE LUG OF AFT VERT STAB ATTACHMENT CORRODED INBOARD (AFT FACE). AFT LUG REWORKED IAW ER 03-5384-01033-BA1.Feb 16, 2001 · N302AW · Boeing 7373G7SDR AWXA0001313Fitting · corrodedRT AFT VERT STAB I/B (FAILSAFE) LUG CORRODED/GOUGED ON ID AND CORRODED/GOUGED ON FWD FACE. LOCALLY BLENDED GOUGE AREAS IAW ER 15-5510-01023-JS3.Feb 9, 2001 · N180AW · Boeing 737277SDR AWXA0001312Fitting · corrodedLT AFT VERT STAB I/B (FAILSAFE) LUG GOUGED IN ID AND CORRODED ON FWD FACE. LOCALLY BLENDED GOUGED AREAS OF LUG FWD SPOT FACE AREA IAW ER 15-5510-0123-JS3.Feb 9, 2001 · N180AW · Boeing 737277SDR COMA0160172Bushing · wornLEFT VERTICAL STABILIZER STAB BUSHING WORN. REMOVED AND REPLACED BUSHING (P/N 600-21061-7). MACHINED BUSHING FLANGE THICKNESS TO .077 INCH AND REMOVED INSIDE DIAMETER TO 1.5002 IAW CRJ AMM 20-26-00-910-803, DRAWING 600-21061 AND WWVAC EO 601R-55-2175.Jan 29, 2001 · N937CA · Cndair CL6002B19SDR DL73K010133Fitting · corrodedCORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE LUGS. SOME OF THE BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED PER ERA 396619-14 AT HMV.Jan 25, 2001 · N312DL · Boeing 737232SDR AU010112Fitting · cracked(AUS) VERTICAL STABILISER FORWARD ADAPTER FITTING RIGHT HAND ATTACHMENT LUG CRACKED.Jan 22, 2001 · Dhav DHC6300SDR DL73K010109Fitting · corrodedCORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AT THE FRONT SPAR. THE DAMAGE WAS REMOVED AND REPAIRED BY ERA 396636-14 AT HMV.Jan 22, 2001 · N313DL · Boeing 737232SDR C2XAO1IA003Hinge · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER FITTING HINGE SUPPORT FOR THE HORIZONTAL STAB WAS FOUND TO BE CORRODED IN THE PIN BORE. MAINTENANCE OVERSIZED THE BORE ON THE FITTING HINGE SUPPORT IAW CONTINENTAL EXPRESS ENGINEERING CHANGE EC551Jan 3, 2001 · N14937 · Emb EMB145ERSDR CALA0001982Angle · crackedINSPECTION FOUND AFT FUSELAGE TO VERTICAL STABILIZER ANGLE ON RT SIDE CRACKED. THE OLD SPLICE WAS REMOVED AND A REPAIR ANGLE AND SPLICE WERE INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 23A AND 23B.Dec 21, 2000 · N16807 · Doug DC982SDR SPAA0000034Fitting · corrodedDURING THE ACCOMPLISHMENT OF SERVICE BULLETIN 737-55-1028, CORROSION WAS FOUND ON THE AFT SURFACE OF THE OUTBOARD LUG COMMON TO THE VERTICAL STABILIZER REAR SPAR FITTING. CORROSION WAS REMOVED PER ECRA N703S-55-737-002-EAC AND THE REWORK WAS FINISHED PER SB 73Dec 16, 2000 · N703S · Boeing 7372T4SDR DHL200080225CFitting · crackedAT C CHECK; VERTICAL STABILIZER REAR SPAR TO FITTING CRACKED 2 INCHES, 2 RT 320.230. REMOVED FITTING IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED FITTING IAW SRM 51-1-21 PG 1. REF: N/R 2342.Dec 6, 2000 · N802DH · Doug DC873FSDR COMA0060987Bushing · scoredVERTICAL STABILIZER HINGE BUSHING SCORED. REMOVED AND REPLACED RT VERTICAL STABILIZER HINGE BUSHING I/A/W/ W.V.A.C. E.O. 601R-55-1952B.Dec 4, 2000 · N959CA · Cndair CL6002B19SDR QXEA0003363Angle · crackedPDX- FORWARD VERTICAL STABILIZER TO FUSELAGE CONNECTION ANGLE HAS CRACKS AT RIGHT OUTBOARD TWO RIVETS. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-04 AND HORIZON AIR EA 4-55-271.Dec 2, 2000 · N492US · Fokker F28MK4000SDR COMA0060923Bushing · looseVERTICAL STABILIZER HINGE BUSHING RT SIDE AND LT SIDE WERE DAMAGED. REMOVED OLD BUSHINGS P/N 600-21061-5 AND INSTALLED NEW BUSHINGS P/N 600-21061-7 I/A/W WVAC EO 601R-55-1896A.Nov 13, 2000 · N958CA · Cndair CL6002B19SDR DL72L002152Fitting · corrodedTHE VERTICAL STABILIZER TENSION TIE FITTING FORWARD AND AFT ATTACH BOLT HOLES WERE FOUND WITH CORROSION IN THE BORES. THE BORES WERE OVERSIZED AND BUSHED PER ERA 396341-14 AT HMV.Nov 2, 2000 · N508DA · Boeing 727232SDR CA001106003Fitting · cracked(CAN) CRACK FOUND IN BRACKET THAT ATTACHES VERTICAL FIN TO FUSELAGE, AT THE REAR ATTACH POINT.Oct 23, 2000 · Cessna 152SDR AALA20001804Fitting · corrodedTUL - FOUND LEFT AND RIGHT VERTICAL STABILIZER LUG PLATES CORRODED. REMOVED, REPLACED LEFT AND RIGHT VERTICAL STABILIZER LUG PLATES SRM 53-02. (M)Oct 13, 2000 · N44503 · Doug DC982SDR P2EA00241Fitting · corrodedDURING C-CHECK INSPECTION, (SB 737-55-1028) OF THE FIN ATTACHMENT FITTINGS, CORROSION WAS FOUNDON FIVE OF EIGHT ATTACHMENT LUGS. THE CORROSION WAS FOUND ON THE RT OUTBOARD AFT LUG, AFT FACE, RT OUTBOARD FORWARD LUG, FORWARD FACE, RT INBOARD AFT LUG, AFT FACE Aug 22, 2000 · N122NJ · Boeing 737230SDR DL73K001564Attach Fitting · wornVERTICAL STAB MOVES UP AND DOWN WHEN PUSHING ON UPPER TRAILING EDGE AREA. FOUND ATTACH FITTINGS WORN. REPAIRED SAME.Aug 15, 2000 · N309DL · Boeing 737232SDR DL73K001577Attach Fitting · corrodedTHE RT AND LT ATTACH FITTINGS OF THE HORIZONTAL STABILIZER WERE FOUND CORRODED. THE BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED PER ERA 334715-14 AT HMV.Aug 14, 2000 · N308DL · Boeing 737232SDR DL73K001576Attach Fitting · corrodedTHE NUMBER 2 LUG ON THE VERTICAL STABILIZER ATTACH FITTING WAS FOUND CORRODED. THE BORE WAS OVERSIZED AND NEW BUSHINGS WERE MANUFACTURED PER ERA 334730-14 AT HMV.Aug 14, 2000 · N308DL · Boeing 737232SDR TWAA0014902Angle · crackedDURING OP 15 MAINT CHECK, FOUND TRANSITION ANGLE FROM FUSELAGE TO VERTICAL STABILIZER, APPROXIMATELY STA 1096, WITH A CRACK AT A SCREW HOLE TO EDGE OF ANGLE, RT SIDE. REPAIRED CRACKED ANGLE PER SRM 53-05, FIG 2.Jul 24, 2000 · N977Z · Doug DC931SDR AU000606Nut · split(AUS) ANCHOR NUT FOR RIGHT FORWARD FIN ATTACH BOLT SPLIT.Jul 19, 2000 · Piper PA32RT300SDR 00FDEA00504Fitting · damagedEMPENNAGE, WITH REF TO E1-5510-7-3304 1 PT 2, STEP 9 AND 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 NR 1-5530-52023.Jul 12, 2000 · N584FE · Doug MD11SDR P2EA00229Attach Fitting · corrodedYYC - DURING C-CHECK, WHILE COMPLYING WITH VANGUARD EO NR 0055A024 VERTICAL STAB ATTACH LUG MOD, FOUND THE AFT FACE OF THE RIGHT AFT LUG AND THE FORWARD FACE OF THE RIGHT SECOND FROM AFT LUGS WTH CORROSION. THE RIGHT SECOND FROM AFT LUG DEFECT SIZE FORWARD FAJul 7, 2000 · N123NJ · Boeing 737230SDR DL73K001279Attach Fitting · corrodedCORROSION WAS FOUND ON THE FUSELAGE SIDE OF THE VERTICAL FIN ATTACH LUGS. LUG BORES WERE OVERSIZED THE THE LUG FACES WERE SPOTFACED TO REMOVE THE CORROSION. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334526-14.Jul 7, 2000 · N305DL · Boeing 737232SDR CALA0000958Attach Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT RT AFT END, STA 1275. FASTENERS WERE REMOVED AND THE CRACKED AREA WAS CUT OUT IAW SRM 51-30-5 AND 53-05, FIGURE 23. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23, 51-Jun 23, 2000 · N819NY · Doug DC982SDR 20000712SH011Bolt · damagedDURING ANNUAL INSPECTION, THE CONTROL SURFACES WERE FOUND TO HAVE NEVER BEEN RE-BALANCED AFTER THE AIRCRAFT HAD BEEN RE-PAINTED SOMETIME PRIOR. WHEN REMOVING THE STABILATOR, IT WAS FOUND THAT THE MOUNTING BOLTS COULD NOT BE REMOVED WITHOUT BEING CUT OFF. ON Jun 22, 2000 · N6467R · Piper PA28140SDR CALA0000704Attach Fitting · crackedINSPECTION FOUND A 2.2 INCH CRACK IN VERTICAL FIN ATTACH ANGLE FOR PANEL ASSEMBLY AT FS 1431, ZFS -26.812. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.May 18, 2000 · N14879 · Doug DC981SDR CALA0000688Attach Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER AFT SPAR LOWER CENTER ATTACH ANGLE, FS 1485. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.May 17, 2000 · N72830 · Doug DC982SDR CALA0000479Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER REAR SPAR LOWER ATTACH ANGLE ON LT SIDE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.Apr 15, 2000 · N16804 · Doug DC982SDR DHL200072631CChannel · damagedRET STABILIZER RT SIDE UNDER THE SLIDING PLATE IS DAMAGED ON THE FRONT CHANNEL. REMOVED THE SLIDING PLATE IAW SRM 51-30-2. REMOVED CHANNEL AND MANUFACTURED AND INSTALLED NEW CHANNEL PER SRM 51-10-1. REINSTALLED SLIDING PLATE PER SRM 51-30-2.Apr 5, 2000 · N726DH · Boeing 727228SDR CA000329015Bolt · sheared(CAN) SLIGHT VIBRATIONS NOTICED DURING FLIGHT (3 PER). UPON LANDING, A SHEARED BOLT WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT. BOLT REPLACED AND ROTORCRAFT TEST FLOWN WITH NO VIBRATIONS.Mar 17, 2000 · Snias AS350BASDR ABXA9900758Fitting · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER LEFT ATTACH FITTING CRACKED AT STATION 1094. REPLACED FITTING IAW DC9 SRM 51-30-5.Oct 26, 1999 · N928AX · Doug DC932SDR 99ZZZX3576Fitting · crackedUPON INSPECTION OF AIRFRAME, DISCOVERED THAT LOWER RIGHT AFT VERTICAL STABILIZER ATTACH FITTING WAS CRACKED, AND LEFT HAND SIDE CORRODED. SUBMITTER STATED CAUSE APPEARS TO BE AGE RELATED.Aug 24, 1999 · N67975 · Cessna 152SDR TSAA9953268Bushing · corrodedVERTICAL FIN AFT SIDE OF RIGHT OUTBOARD AFT SPAR ATTACH FITTING CORRODED UNDER BUSHING FLANGE. REPAIR IAW ECO 2973. AIRCRAFT RETURNED TO SERVICE. (M)May 26, 1999 · N807AL · Boeing 7372T4SDR TSAA9953267Bushings · corrodedFUSELAGE LUGS FOR VERTICAL FIN AFT SPAR ATTACH HAVE HEAVY FRETTING ON FACES ON BUSHINGS. REPAIRED PER ECO 2978. AIRCRAFT RETURNED TO SERVICE. (M)May 26, 1999 · N807AL · Boeing 7372T4SDR AU990383Adapter · cracked(AUS) VERTICAL STABILIZER ATTACHMENT ADAPTER CRACKED THROUGH THE RIGHT ATTACHMENT BOLT HOLE.Apr 20, 1999 · Dhav DHC6300SDR CA990323033Fitting · corroded(CAN) THE DEFECT WAS DETECTED DURING AN ANNUAL INSPECTION. CORROSION WAS EXTENSIVE ENOUGH TO REQUIRE REPLACEMENT OF THE ATTACH FITTING. ALL AIRCRAFT IN FLEET WILL BE SUBJECTED TO SPECIAL INSPECTION IN THE AFFECTED AREA.Mar 10, 1999 · Grumav TBM3EAIRTRDSDR CA990323032Fitting · corroded(CAN) THE DEFECT WAS DETECTED DURING AN ANNUAL INSPECTION. CORROSION WAS EXTENSIVE ENOUGH TO REQUIRE REPLACEMENT OF THE ATTACH FITTING. ALL AIRCRAFT IN FLEET WILL BE SUBJECTED TO SPECIAL INSPECTION OF THE AFFECTED AREA.Mar 10, 1999 · Grumav TBM3AIRTRDSDR AU990385Adapter · cracked(AUS) VERTICAL STABILIZER FORWARD ATTACHMENT ADAPTER CRACKED THROUGH RIGHT ATTACHMENT BOLT HOLE.Feb 26, 1999 · Dhav DHC6300SDR RRXA98388Skin · gougedDURING A MAINTENANCE VISIT, FOUND LEFT WING OUTBOARD FLAP WEDGE HAD PREVIOUS BLENDOUT ON TOP INBOARD CORNER AT THE ATTACH SEAM GOUGED, BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBJul 27, 1998 · N8076U · Doug DC871FSDR AU980818Fitting · loose(AUS) VERTICAL STABILIZER REAR ATTACHMENT FITTING RIVETS SHEARED AND FITTING LOOSE.Jul 21, 1998 · Piper PA34200T
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