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 P4YA2009050300001Attach Fitting · corrodedWHILE PERFORMING MX ON THE HORIZONTAL STABILIZER, AN OPPORTUNITY INSP WAS PERFORMED OF THE ADJACENT AREAS. SEVERE EXFOLIATION CORROSION WAS FOUND ON THE LOWER RT HORIZONTAL STABILIZER ATTACH FITTING. THE SRM CLASSIFIES THE PART AS A PRIMARY STRUCTURE ITEM.May 3, 2009 · N961BW · Casa C212CCSDR 2009FA0000344Bracket · crackedDURING SCHEDULED INSP FOUND HORIZ STAB LT FWD ROLLER ATTACH BRACKETS CRACKED. AREA PREVIOUSLY NOTED AS SUBJECT TO CRACKING IAW MFG COMMUNIQUES AND LATER INCORPORATED INTO MM INSP GUIDE. AREA CAN BE DIFFICULT TO INSPECT; TECHS AND INSP CAUTIONED TO INSPECT AREAMay 1, 2009 · N45RK · Beech 400ASDR CA090407010Bracket · cracked(CAN) HORIZ STABILIZER WAS REMOVED FOR UNASSOCIATED MX. LT PICK-UP BRACKET WAS FOUND TO BE CRACKED ON OTBD FACE. DAMAGE IS SIMILAR TO CRACKS DISCUSSED IN TNS SERIES "B" 55, PARAGRAPH 2.1 WITH THE EXCEPTION THAT THIS ACFT IS ALREADY FITTED WITH MOD/627 - MALEApr 3, 2009 · Dhav DHC2MKISDR IXXA09SMN043SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER FITTING CRACKED AT STATION XFS 60.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.Mar 30, 2009 · N605AL · Doug DC873FSDR DLM88090551Attach Fitting · corrodedDURING HMV CORROSION WAS FOUND ON HORIZONTAL STAB ATTACH PLATES ON BOTH SIDES. PLATES WAS REPAIRED IAW SRM 55-02 FIG 28 PARAGRAPH 24.Mar 29, 2009 · N977DL · Doug MD88SDR DLM88090598Attach Fitting · corrodedRUST ON HORIZ STAB ATTACH PLATES BOTH SIDES. RUST REPAIRED IAW SRM'S 51-10-3D AND 55-02.Mar 5, 2009 · N977DL · Doug MD88SDR AALA2009021300100Lug · corrodedNUMBER 8 RIGHT OUTBOARD HORIZONTAL STABILIZER PLATE LUG BORE CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER 8 LUG PLATE PER CARD NR 2988AA.Jan 12, 2009 · N412AA · Doug DC982SDR SWIA200921195Fitting · crackedRIGHT STABILIZER PIVOT FITTING BASE CRACKED ON LOWER AFT SIDE. C-CHECK, REPAIRED PER SRM AND REO.Jan 10, 2009 · N413SW · Cndair CL6002B19SDR SWIA200921193Fitting · crackedHORIZONTAL STABILZER PIVOT FITTING BASE CRACKED. C-CHECK, REPLACED FITTING.Jan 10, 2009 · N413SW · Cndair CL6002B19SDR CA081122007Attach Fitting · loose(CAN) DURING A SCHEDULED INSPECTION OF THE HSTA IN ACCORDANCE WITH THE MAINTENANCE PROGRAM, PSA MAINTENANCE REPORTED LOOSE FASTENERS (ITEM 35, 36, 24, 25) THAT SECURE THE HSTA UPPER ATTACHMENT FITTING (ITEM 33) TO THE HSTAB (SEE ATTACHED ILLUSTRATION) UPON FUNov 9, 2008 · Cndair CL6002C10SDR CA081020001Mount · misinstalled(CAN) METAL FILINGS WERE FOUND UNDER THE RUDDER SERVO DUE TO THE MOUNTING STRUCTURE HAVING BEEN INSTALLED OFFSET FROM THE FACTORY. THIS CAUSED THE RUDDER CABLE TO EXIT THE DRUM ON AN ANGLE AND RUB THE CAPSTAN. THE SERVO WAS REPLACED AND A PERMANENT FIX IS SCHEOct 3, 2008 · Cessna 525SDR CA080916006Attach Bracket · cracked(CAN) CARRIED OUT SEB 03-6 ON VERTICAL TAIL ATTACH BRKT AND STAB SPAR. SPAR WAS NOT CRACKED BUT THE STEEL ATTACH BRKT WAS CRACKED AROUND A RIVET HOLE FOR THE PREVIOUSLY INSTALLED NUT PLATES. AD PREVIOUSLY ALLOWED REMOVAL OF NUT PLATES. THIS OPERATOR HAS SEEN Sep 12, 2008 · Cessna 152SDR 08FDEA03520Fitting · corrodedGENERATED BY EO 7-5510-7-5000, HORIZONTAL STAB RT HINGE FITTING O/B BUSHING BORE HAS CORROSION OVERSIZED LUG BORE TO 2.2244 INCH CORROSION REMOVED. HFEC INSPECTED BORE NO DEFECTS NOTED. FABRICATED OVERSIZE BUSHING, CAD PLATED BUSHING. INSTALLED OVERSIZE BUSAug 20, 2008 · N211FE · Boeing 7272S2FSDR SWAA084212Fitting · corrodedDURING SCHEDULE BRDG CHECK, FOUND RT HORIZONTAL STABILIZER CLEVIS LUG FITTING FACES CORRODED. REPAIRED PER SRM.Jul 28, 2008 · N336SW · Boeing 7373H4SDR SWAA084213Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LT HORIZONTAL STABILIZER CLEVIS LUG FITTING FACES CORRODED. REPAIRED PER SRM.Jul 28, 2008 · N336SW · Boeing 7373H4SDR C2XA08SH090Fitting · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT HORIZONTAL STAB HINGE PIN FITTING HAD MIGRATED PLAIN BUSHINGS. MAINTENANCE PERFORMED A REAMING PROCEDURE TO THE SECOND OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)Jun 20, 2008 · N16147 · Emb EMB145XRSDR C2XA08SH089Fitting · gougedSHV - DURING C-CHECK IT WAS FOUND THAT THE LT HORIZONTAL STAB HINGE PIN FITTING WAS GOUGED. MAINTENANCE PERFORMED A REAMING PROCEDURE TO THE FIRST OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)Jun 20, 2008 · N16147 · Emb EMB145XRSDR CA080611005Attach Bracket · worn(CAN) DURING ANNUAL INSP WITH AN AOG AIR SUPPORT WING ANGLE INSTALLED MODIFICATION, MOVEMENT WAS FOUND IN THE HORIZONTAL STABILIZER FWD ATTACH POINTS. THE HORIZONTAL STABILIZER FWD ATTACH BRACKETS WERE REMOVED AND INSPECTED AND IT APPEARS THAT THE FUSELAGE FITJun 9, 2008 · Dhav DHC2MKISDR M7K2008F00032Fitting · crackedDURING ROUTINE INSPECTION, THE FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO FLANGE EDGE. NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THIS PART. BORE HOLES MUST BE MATCH DRILLED AND ALIGNED PERFECTLY. SUGGEST A MORE DURABLE MATERIMay 23, 2008 · N808MH · Urocop EC130B4SDR M7K2008F00031Fitting · crackedDURING ROUTINE INSP THE FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO THE FLANGE EDGE. A NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THIS PART. PART MAY HAVE BEEN SHIMMED INCORRECTLY OR BORE HOLE NOT ALIGNED PERFECTLY. SUGGEST A MMay 23, 2008 · N808MH · Urocop EC130B4SDR M7K2008F00020Fitting · crackedDURING ROUTINE INSP FITTING WAS FOUND CRACKED IN (2) PIECES. NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THIS PART. PART MAY HAVE BEEN SHIMMED INCORRECTLY OR BORE HOLE NOT ALIGNED PERFECTLY. SUGGEST A MORE DURABLE MATERIAL BE USED IN THIS PARTS MFMay 23, 2008 · N821MH · Urocop EC130B4SDR SWAA082534Fitting · corrodedDURING SCHEDULED SPV CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.May 11, 2008 · N356SW · Boeing 7373H4SDR 2008UALA02211Lug · corrodedLT HORIZONTAL STABILIZER FWD SPAR UPPER LUG HAS EVIDENCE OF CORROSION. MAJOR REPAIR ACCOMPLISHED: HONED LUG BORE TO DIMENSION OF 1.2537". SPOT FACED FWD AND AFT FACES TO FINAL DIMENSION OF 1.042". ACP'D REPAIR AND INSTALLED OVERSIZED SLEEVE AND BUSHINGS.Apr 16, 2008 · N203UA · Boeing 737322SDR 2008UALA02162Clevis · corrodedRT HORIZONTAL STABILIZER CENTER SECTION AFT SPAR UPPER CLEVIS FWD AND AFT LUG HAVE EVIDENCE OF CORROSION. SPOTFACED FWD AND AFT FACES OF THE LUGS TO REMOVE CORROSION TO THE FINAL DIMENSION OF 1.110" ON THE FWD LUG AND 1.126 INCH ON THE AFT LUG. REAMED FWD LUApr 12, 2008 · N203UA · Boeing 737322SDR 2008UALA02161Clevis · corrodedRT HORIZONTAL STABILIZER CENTER SECTION FWD SPAR UPPER CLEVIS FWD AND AFT LUG HAVE EVIDENCE OF CORROSION. SPOTFACE FWD AND AFT FACES ON BOTH LUGS TO REMOVED CORROSION WITH FINAL DIMENSION OF .596 INCH ON THE FWD AND .577 INCH ON THE AFT LUG. REAMED THE BORESApr 11, 2008 · N203UA · Boeing 737322SDR 2008UALA02088Lug · corrodedRT HORIZONTAL STABILIZER AFT SPAR UPPER LUG HAS EVIDENCE OF CORROSION. MAJOR REPAIR: REMOVED CORROSION.Apr 10, 2008 · N203UA · Boeing 737322SDR 2008UALA01795Lug · corrodedLT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CLEVIS FWD AND AFT LUGS HAVE EVIDENCE OF FRETTING CORROSION. MAJOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR.Mar 29, 2008 · N202UA · Boeing 737322SDR 2008UALA01794Lug · corrodedLT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER CLEVIS FWD AND AFT LUGS HAVE EVIDENCE OF FRETTING CORROSION. MAJOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR.Mar 29, 2008 · N202UA · Boeing 737322SDR 2008UALA01793Lug · corrodedLT HORIZONTAL OUTBOARD STABILIZER FWD SPAR UPPER LUG FWD BUSHING HAS FRETTING CORROSION. MAJOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR.Mar 29, 2008 · N202UA · Boeing 737322SDR 2008UALA01792Lug · corrodedLT HORIZONTAL OUTBOARD STABILIZER REAR SPAR UPPER LUG FWD BUSHING HAS FRETTING CORROSION. MAJOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR.Mar 29, 2008 · N202UA · Boeing 737322SDR 2008UALA01635Bushing · corrodedRT HORIZONTAL STABILIZER FWD SPAR UPPER ATTACH LUG AFT BUSHING SHOW SIGNS OF CORROSION. MAJOR REPAIR: REMOVED CORROSION.Mar 21, 2008 · N202UA · Boeing 737322SDR 08FDEA00565Lug · corrodedRT HORIZIONTAL STAB NR 6 ELEVATOR HINGE ARM LUG AT THE ELEVATOR IS CORRODED UPPER INBD. REMOVED AND REPLACED IAW AMM 55-16-45-1. FUNCTIONAL TEST GOOD IAW AMM 27-31-11.Feb 22, 2008 · N803FD · Airbus A310324SDR SWAA080821Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.Feb 12, 2008 · N697SW · Boeing 7373TOSDR SWAA080820Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER SRM.Feb 12, 2008 · N690SW · Boeing 7373G7SDR CALA0800132Fitting · corrodedRT HORIZONTAL STAB FORWARD UPPER LUG HAS CORROSION. REMOVED SLEEVE AND BUSHINGS. REMOVED CORROSION AND PERFORMED REQUIRED INSPECTIONS PER ECRA 5510-01915. FABRICATED AND INSTALLED REPAIR SLEEVE AND FLANGE BUSHINGS PER SRM 55-10-10.Feb 12, 2008 · N19621 · Boeing 737524SDR CALA0800131Fitting · corrodedRT HORIZONTAL STAB FORWARD LOWER LUG HAS CORROSION. REMOVED SLEEVE AND BUSHINGS, REMOVED CORROSION AND PERFORMED REQUIRED INSPECTIONS PER ECRA 5510-01915. FABRICATED AND INSTALLED REPAIR SLEEVE AND FLANGE BUSINGS PER SRM 55-10-10.Feb 12, 2008 · N19621 · Boeing 737524SDR IXXA08SMN050SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FITTING INTERCOSTAL SIDE CRACKED XFS 60.000. REMOVED CRACKED FITTING. PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-14, AND 51-3-1.Feb 7, 2008 · N822BX · Doug DC871FSDR IXXA08SMN049SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER FITTING INTERCOSTAL SIDE CRACKED AT STATION XFS 60.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 51-1-8B, AND Feb 7, 2008 · N822BX · Doug DC871FSDR QXEA200802056Lug · damagedPDX - C4 CHECK - RIGHT HORIZONTAL STAB ANTI-ROTATION LUG APPEARS TO HAVE DAMAGE BEYOND PREVIOUS BLEND REPAIR, DUE TO HINGE HARDWARE ROTATION. BLENDED DAMAGED AREA IAW REO 670-55-11-033, HFEC INSPECTED AND NO CRACKS NOTED. ROTOPEENED AND RESTORED FINISH TO BLDec 15, 2007 · N604QX · Cndair CL6002C10SDR SWAA076194Attach Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER FWD AND AFT LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.Dec 13, 2007 · N697SW · Boeing 7373TOSDR CA071204009Bracket · cracked(CAN) WHILE COMPLETING THE REQUIREMENTS OF CF 91-42R1 IAW SB 2/47 REV (E), THE RT FWD STABILIZER ATTACH BRACKET WAS FOUND TO BE CRACKED. THE CRACK EXTENDED FROM THE TOP OF THE IB EAR OF THE BRACKET, THROUGH THE LOCKWIRE HOLE AND CONTINUED APPROX 75 PERCENT OF Nov 30, 2007 · Dhav DHC2MKISDR 2007FA0000988Pivot · looseWHILE PERFORMING AN A-C INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A2118311 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE.Oct 31, 2007 · N940VA · Beech 400ASDR AMTA200700501Attach Fitting · damagedUPON INNSPECTION OF FORWARD SPAR ATTACHMENT BOLTS FOUND THE RT LOWER AND RT UPPER BOLTS DEFECTIVE, GALLING AND FRETTING WEAR. COMPLIED WITH EO 737-55AD-2935, REPLACED (2) BOLTS WITH PN 180A1611-3. (K)Oct 14, 2007 · N308TZ · Boeing 73783NSDR SWAA074808Fitting · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING PER BOEING SB.Sep 25, 2007 · N655WN · Boeing 7373H4SDR QXEA200701463Mount · damagedC5 PDX - HORIZONTAL STAB FORWARD RIGHT MOUNTING STRUCTURE HAS NICKS AND GOUGES ON OUTBOARD SIDE. REPAIRED IAW RD8-55-847, SRM 51-20-51, 51-20-16.Sep 17, 2007 · N345PH · Dhav DHC8202SDR QXEA200701461Mount · damagedC5 PDX - HORIZONTAL STAB FORWARD MOUNT POSTS ARE SCRATCHED ON OUTBOARD SURFACE. REPAIRED IAW RD8-55-847 AND SRM 51-20-51, 51-20-16.Sep 17, 2007 · N345PH · Dhav DHC8202SDR CA080219003Attach Bracket · cracked(CAN) DURING INSP OF FIN ATTACH BRACKET NUT PLATES IAW AD 80-11-04 CRACKS WERE DISCOVERED RUNNING ALONG THE BEND RADIUS OF THE WELDED BRACKET. THE AD ALLOWS FOR REMOVING REPETATIVE INSP REQUIREMENTS IF THE NUT PLATES ARE DRILLED OFF AND REPLACED WITH FIBERLOCKSep 14, 2007 · Cessna 152SDR 2007UALA03479Lug · corrodedRIGHT HORIZ STAB FWD UPPER LUG CORRODED AND BUSHINGS HAVE MIGRATED. REMOVED FWD & AFT BUSHING & SLEEVE AND REMOVED CORROSION ON FWD FACE OF LUG. FABRICATED & INSTALLED OVERSIZED BUSHING & SLEEVE.Aug 29, 2007 · N379UA · Boeing 737322SDR 2007UALA03478Clevis · corrodedRIGHT HORIZ STAB CORRODED: CENTER SECTION AFT UPPER CLEVIS AFT LUG EMITTING CORROSION. REMOVED BUSHINGS (FWD AND AFT LUGS), REAMED BORES OF LUGS, HFEC INSPECTED WITH NO DAMAGE FOUND, ROTO-PEENED, TREATED AND PRIMED LUGS, FABRICATED OVERSIZED BUSHINGS-INSTAAug 29, 2007 · N379UA · Boeing 737322SDR SWAA074244Clevis · corrodedDURING SCHEDULED 20Y CHECK, FOUND RIGHT AND LEFT HORIZONTAL STABILIZER CLEVIS LUG FACES CORRODED. REPAIRED HORIZONTAL STABILIZER PER SRM.Aug 28, 2007 · N331SW · Boeing 7373H4
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