JASC 5551

Service difficulty reports · 672

Reports filed under 5551 · Horizontal 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 = '5551'
  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 SWAA030601Pin · corrodedDURING SCHEDULED 5Y CHECK, FOUND BOTH LT & RT HORIZ STAB AFT LUG UPPER ATTACH PINS CORRODED. REMOVED AND REPLACED ATTACH PINS PER MM.Mar 17, 2003 · N710SW · Boeing 7377H4SDR F3LA200300114Fitting · corrodedDURING C-4 CHECK, INSPECTION REPORTED RT. HORIZONTAL STAB CENTER SECTION, AFT UPPER ATTACH CLEVIS, AFT LUG, CORRODED. REPAIRED PER EA 55-737-077.Mar 10, 2003 · N921WA · Boeing 7372Y5SDR F3LA200300098Attach Fitting · corrodedDURING EXIT CHECK, INSPECTION REPORTED CORROSION ON OUTER SURFACE OF LT. HORIZONTAL STABILIZER FRONT SPAR LOWER ATTACH LUG. REWORKED FRONTIER SPAR LOWER ATTACH LUG PER CMM 55-10-06. PERFORMED HFEC PER D637239, PART 6, 51-00-00, FIG. 23, NO CRACKS FOUND. FABRFeb 28, 2003 · N318FL · Boeing 7373Q8SDR BJNA030216Fitting · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND IN THE BORES OF THE HORIZONTAL STABILIZER CENTER SECTION FORWARD TERMINAL FITTINGS UPPER AND LOWER AFT LUGS. THE BORES WERE REAMED TO THE MAXIMUM DIAMETER (1.125 INCH) SHOWN IAW SB. AFTER REAMING INSPECTION SFeb 25, 2003 · N789TM · Boeing 737282SDR CA030205001Bracket · cracked(CAN) DURING CHANGEOVER FROM FLOATS TO WHEELS A CRACK WAS FOUND ON THE TAIL WHEEL ATTACHMENT LUG. THE CRACK WAS ON THE LT FORWARD ATTACH POINT OF THE TAIL WHEEL. THIS BRACKET ALSO ATTACHES THE HORIZONTAL STABILIZER ON THE UPPER PICKUPS. BRACKET WAS REPLACED WIFeb 5, 2003 · Dhav DHC2MK3SDR AUS20021309Fitting · damaged(AUS) HORIZONTAL STABILISER ATTACHMENT FITTING HOLES OVERSIZE.Oct 31, 2002 · Cessna 402CSDR AUS20021251Fitting · cracked(AUS) RH HORIZONTAL STABILISER FORWARD ATTACHMENT FITTING CRACKED.Oct 18, 2002 · Piper PA60600ASDR CA021031002Bracket · cracked(CAN) DURING ROUTINE INSPECTION OF STABILIZER BRACKET NUTPLATES AS PER AD 80-11-04, IT WAS NOTED THAT STEEL BRACKET ITSELF WAS CRACKED. AT REMOVAL, BOTH LEFT AND RIGHT TOP SIDES WERE CRACKED. THE FIN BOLTS TO THIS BRACKET, SO THE CRACKING COULD BE A RESULT OF Oct 17, 2002 · Cessna 152SDR DL733021087Fitting · corrodedCORROSION WAS FOUND ON THE RT INBOARD LUG BORE ON THE HORIZONTAL STABILIZER CENTER SECTION UPPER FITTING. THE BORE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED. THE DAMAGE WAS FOUND AT HMV.Sep 16, 2002 · N305WA · Boeing 737347SDR CA021122002Bracket · cracked(CAN) DURING SCHEDULED MAINTENANCE, IT WAS DISCOVERED THE REINFORCEMENT BRACKETS WERE CRACKED. NEW PARTS 0732101-4 WERE INSTALLED.Jul 20, 2002 · Cessna A185FSDR COMA0260403Bushing · damagedI/B HORIZONTAL TO VERTICAL ATTACH LUGS (ON HORIZONTAL) WERE FOUND TO BE OUT OF TOLERANCE (BUSING HOLES).BUSHING HOLES WERE REAMED TO FIRST OVERSIZE, AND FIRST OVERSIZE BUSHINGS WERE INSTALLED. NEW BUSHINGS WERE THEN REAMED TO AN INTERNAL DIAMETER OF 1.50". ALLJul 1, 2002 · N934CA · Cndair CL6002B19SDR COMA0260404Bushing · damagedPIVOT BUSHING R/II VERT STAB REQUIRED REPLACEMENT P/N 600-21061-7REMOVED AND REPLACED BUSHING I/A/W WVAC E.O. 601R-55-3311.Jun 24, 2002 · N934CA · Cndair CL6002B19SDR CALA0200209Fitting · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER FORWARD UPPER LUG CORRODED. THE CORROSION WAS REMOVED FROM LUG IAW SRM 55-10-10.Apr 16, 2002 · N14342 · Boeing 7373T0SDR 200200232Angle · crackedLT HORIZONTAL STAB INBOARD LEADING EDGE FAIRING HAS AN (L) ANGLE CRACKED 3RD RIB FROM INBOARD END. REMOVED (L) ANGLE CRACKED, ORIGINAL MATERIAL 7075 PER CHEMICAL TEST 747 SRM 51-10-01 AND .030 PER CALIPER NR 99-0043 DUE DATE 04-02. FABRICATED (C) ANGLE FROM 70Apr 5, 2002 · N479EV · Boeing 747132SDR H792002F00000Bracket · crackedDURING ANNUAL INSPECTION NOTICED CRACKS IN THE LEFT AFT HORIZONTAL STABILIZER ATTACH BRACKET. IF BRACKET IS CRACKED, REPLACE WITH IMPROVED BRACKET.Mar 23, 2002 · N155RR · Cessna T210NSDR CALA0200134Fitting · corrodedINSPECTION FOUND TWO R/H FORWARD HORIZONTAL STABILIZER ATTACH FITTINGS HAD LOWER AFT AND FORWARD BUSHINGS CORRODED BETWEEN BUSHING AND LUG. AN OVERSIZED BUSHING WAS INSTALLED AT EACH LOCATION IAW CMM 55-10-10.Mar 17, 2002 · N14346 · Boeing 7373T0SDR COMA0260186Bushing · crackedHORIZONTAL STABILIZER ATTACH FITTING R.H. PIVOT PIN BUSHING LOOSE.REPLACED BUSHING I/A/W S.B. 601R-55-007 STEP 4 PAGE 51 THROUGH STEP 15 PAGE 64 AND REO 601R-55-31-036.Mar 13, 2002 · N991CA · Cndair CL6002B19SDR COMA0260183Fitting · crackedRH HORIZ STAB VISOR FITTING CRACKED.INSTALLED NEW SERVICEABLE FITTING.I/A/W REO 601R-55-11-016 AND SRM 51-42-06.Mar 13, 2002 · N991CA · Cndair CL6002B19SDR DL73K020239Hinge Fitting · corrodedHORIZONATAL STABLIZER / LH / CENTER SECTION / HINGE FITTING:CORROSION REPAIR CORROSION WAS DETECTED ON THE HINGE FITTING OF THE LH HORIZ STABILIZER. THE CORROSION WAS REMOVED BY MACHINING THE BORE DIAMETERS OFeb 27, 2002 · N377DL · Boeing 737247SDR CALA0200082Attach Fitting · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FORWARD ATTACH FITTING ON CENTER BOX LUG FACE CORRODED AROUND BUSHING FORWARD LUG FACE. THE BUSHING WAS REMOVED AND AN OVERSIZED BUSHING WAS INSTALLED IAW CMM 55-10-06.Feb 18, 2002 · N19636 · Boeing 737524SDR AALA20020126Attach Angle · crackedTUL - FOUND VERTICAL STAB ATTACH ANGLE CRACKED AT TOP OF 1463 CANT FRAME. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-2. (M)Jan 29, 2002 · N427AA · Doug DC982SDR COMA0260055Bushing · misalignedR/H AND L/H I/B HORIZONTAL STABILIZER BUSHINGS WERE FOUND TO BE MIGRATING.REMOVED AND REPLACED THE R/H AND L/H I/B STABILIZER BUSHINGS P/N 600-23068 I/A/W CRJ AMM 20-26-00-910-803 AND DWG #600-23068.Jan 17, 2002 · N978CA · Cndair CL6002B19SDR TSAA0255024Attach Fitting · gougedFOUND GOUGE MARKS ON LEFT HORIZONTAL STABILIZER CENTER SECTION LUG, UPPER FORWARD FITTING. REMOVED GOUGE / DAMAGED MATERIAL TO A MINIMUM WIDTH OF .10 INCH AND RADIUS OF 1 INCH AND TAPERED. APPLIED A CHEMICAL CONVERSION COATING AND REFINISHED THE REWORKED SURJan 14, 2002 · N805AL · Boeing 7372M6CSDR DL73K011864Attach Fitting · corrodedTHE REAR SPAR UPPER CLEVIS FITTING OF THE HORIZONTAL STAB WAS FOUND CORRODED. THE DAMAGE WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 26, 2001 · N322DL · Boeing 737232SDR DL73K011863Attach Fitting · corrodedTHE HORIZONTAL STABILIZER CLEVIS ATTACH LUGS WERE FOUND CORRODED ON THE FACES AND BORES. THE DAMAGE WAS CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 26, 2001 · N322DL · Boeing 737232SDR DL73K011862Attach Fitting · corrodedSEVERAL OF THE BORES AND FACES OF THE LT AND RT ATTACH LUGS ON THE HORIZONTAL STABILIZER WERE FOUND CORRODED. THE DAMAGE WAS CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.Nov 26, 2001 · N322DL · Boeing 737232SDR CA011031021Attach Fitting · mismanufactured(CAN) AD 98-10-12, HORIZONTAL STAB ATTACHMENT FITTING NO OF NEW CUSTOMERS A/C HAVE BEEN INSPECTED AT COMPANY & ARE NOT IN COMPLIANCE WITH AD, ALTHOUGH ITS BEEN PREVIOUSLY SIGNED OFF. MOST INSPECTIONS REVEAL THAT CLEARANCE I S LESS THAN THE REQUIRED 5/32 INCH. Oct 31, 2001 · Conaer LA4200SDR AALA20012006Fitting · corrodedTUL - FOUND HORIZONTAL STAB PIVOT BEARING LUG PLATES HAVE CORROSION IN BORE AND ARE BELOW MINIMUM THICKNESS. REMOVED AND REPLACED LEFT INBOARD AND OUTBOARD LUG PLATES. REMOVED AND REPLACED RIGHT INBOARD AND OUTBOARD LUG PLATES PER SRM 51 AND 55. (M)Oct 24, 2001 · N59523 · Doug DC982SDR COMA0160826Bushing · wornL/H VERTICAL STABILIZER BUSHING P/N 600-21061-7 IS WORN.REMOVED THE WORN BUSHING I/A/W CRJ AMM CH 20-26-00-910-802, FABRICATED NEW BUSHING P/N 601R55-31-033-1 I/A/W REO 601R-55-31-033 AND INSTALLED THE BUSHING I/A/W REO 601R-55-31-002.Oct 20, 2001 · N933CA · Cndair CL6002B19SDR AUS20011077Bracket · sheared(AUS) RT HORIZONTAL STABILISER ATTACHMENT BRACKET RIVETS SHEARED.Sep 28, 2001 · Gippld GA8SDR AALA20011788Plate · corrodedTUL - FOUND HORIZONTAL STAB LUG PLATES CORRODED IN BORE AND OUTBOARD FACE, 4 LUG PLATES. REMOVED AND REPLACED 4 LUG PLATES WITH NEW PER SRM 51-01-00 AND 1PC 55-50-00. (M)Sep 1, 2001 · N437AA · Doug DC983SDR USAA010905Attach Fitting · corrodedCLT - FOUND UPPER ATTACH LUGS APPROX .5 INCH TOTAL AREA, CORRODED, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT SPAR. REAMED CLEVIS TO REMOVE CORROSION, MACHINED AND INSTALLED NEW BUSHING PER SRM 55-10-10. (M)Jul 20, 2001 · N371US · Boeing 7373B7SDR USAA010904Attach Fitting · corrodedCLT - FOUND LUG ATTACH FITTING CORRODED APPROX 5 INCH AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, REAR SPAR FORWARD LUG, FORWARD FACE. LUG SPOT FACED TO DEPTH OF .070 INCH PER SRM 55-10-10 GRAPH II. (M)Jul 20, 2001 · N371US · Boeing 7373B7SDR USAA010903Attach Fitting · corrodedCLT - FOUND ATTACH LUG FITTING CORRODED .75 INCH TOTAL SURFACE AREA, LEFT HORIZONTAL STABILIZER CENTER SECTION, FRONT LOWER FORWARD LUG. CORROSION REMOVED, FABRICATED AND INSTALLED NEW BUSHING PER SRM 55-10-10. (M)Jul 20, 2001 · N371US · Boeing 7373B7SDR DL73K011193Fitting · corrodedCORROSION WAS FOUND RH AND LH HORIZONTAL STABILIZER ATTACH FITTINGS ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED PER ERA 397745-14. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV.Jul 19, 2001 · N317DL · Boeing 737232SDR AUS20010755Fitting · corroded(AUS) HORIZONTAL STABILISER AFT UPPER FITTING CONTAINED SEVEREINTERGRANNULAR CORROSION. NDI CARRIED OUT ON FITTING FOLLOWINGREMOVAL FOUND THREE CRACKS BETWEEN THE BOLT HOLES.Jul 5, 2001 · Beech 200BEECHSDR COMA0160396Bushing · scoredFOUND 3 EACH VERTICAL TO HORIZONTAL PIVOT POINT BUSHINGS TO BE SCORED.REMOVED HORIZONTAL STAB ASSY. REMOVED THE DAMAGED BUSHINGS. INSTALLED 3 EACH NEW BUSHINGS AND FINAL REAMED. REINSTALLED SAME HORIZONTAL STAB ASSEMBLY. ALL WORK WAS PERFORMED I/A/W CRJ AMJun 20, 2001 · N945CA · Cndair CL6002B19SDR DL73K010964Attach Fitting · corrodedCORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER ATTACH LUGS. CORROSION WAS REMOVED FROM SEVERAL FACES, BORES AND OVERSIZED REPAIR BUSHINGS WERE INSTALLED PER ERA 397635-14 AT HMV.Jun 14, 2001 · N320DL · Boeing 737232SDR QXEA0101020Fitting · gougedYYC - HORIZONTAL STAB DRIVE FITTING LEFT-HAND ARM GOUGED. REPAIRED IAW HORIZON AIR EA 4-55-293.May 31, 2001 · N481US · Fokker F28MK4000SDR QXEA0101021Fitting · corrodedYYC - HORIZONTAL STAB DRIVE FITTING RIGHT-HAND AND LEFT-HAND LOWER LUGS HAVE MINOR CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-292 AND FOKKER SRM 51-10-04, PARAGRAPH 4.May 29, 2001 · N481US · Fokker F28MK4000SDR DL73S010785Attach Fitting · corrodedCORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS. DAMAGE WAS REMOVED FROM THE FACES AND BORES, OVERSIZED BUSHINGS INSTALLED PER ERA 397579-14 AT HMV.May 17, 2001 · N323DL · Boeing 737232SDR AUS20010426Fitting · cracked(AUS) LT AFT TAILPLANE ATTACHMENT REINFORCEMENT CRACKED.May 7, 2001 · Cessna U206FSDR SWAA011332Attach Fitting · wornDURING SCHEDULED C4 CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION FWD SPAR LT LWR ATTACH LUG WORN. REPAIRED PER SWA RA.May 1, 2001 · N710SW · Boeing 7377H4SDR SWAA011240Fitting · corrodedDURING SCHEDULED D CHECK, FOUND RT HORIZ STAB CENTER SECTION FRONT SPAR UPPER CLEVIS AFT LUG CORRODED. REPAIRED FITTING PER BFG ER.Apr 25, 2001 · N103SW · Boeing 7372H4SDR SWAA011239Fitting · corrodedDURING SCHEDULED D CHECK, FOUND LT HORIZ STAB CENTER SECTION AFT SPAR UPPER CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED FITTING PER BFG ER.Apr 25, 2001 · N103SW · Boeing 7372H4SDR SWAA011102Fitting · corrodedDURING SCHEDULED D CHECK, FOUND RT HORIZ STAB CENTER SECTION REAR SPAR LOWER CLEVIS AFT LUG, AFT FACE, CORRODED. REPAIRED FITTING PER BFG ER.Apr 10, 2001 · N103SW · Boeing 7372H4SDR SWAA011112Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR UPPER HINGE HOUSING ATTACH LUGS CORRODED AT RT SIDE, INBOARD AND OUTBOARD FACES. REPAIRED FITTING PER BFG ER.Apr 10, 2001 · N103SW · Boeing 7372H4SDR SWAA011093Fitting · corrodedDURING SCHEDULED D CHECK, FOUND LT HORIZ STAB CENTER SECTION REAR SPAR HINGE HOUSING LOWER INBD ATTACH CLEVIS CORRODED AT OUTBD FACE. REPAIRED FITTING PER BRG ER.Apr 9, 2001 · N103SW · Boeing 7372H4SDR SWAA011092Fitting · corrodedDURING SCHEDULED D CHECK, FOUND HORIZ STAB CENTER SECTION AFT SPAR LOWER HINGE HOUSING ATTACH FITTING CORRODED AT OUTBD LUG, INBD FACE, LT SIDE. REPAIRED FITTING PER BFG ER.Apr 9, 2001 · N103SW · Boeing 7372H4SDR CALA0100287Attach Fitting · corrodedINSPECTION FOUND RT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING FWD AND AFT BUSHINGS HAD CORROSION BETWEEN BUSHINGS AND FITTINGS. NEW OVERSIZED BUSHINGS WERE INSTALLED IAW SRM 55-10-06.Apr 6, 2001 · N17326 · Boeing 7373T0
Back to JASC 5551