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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WVER2012071250701Pivot · seizedLEFT AND RIGHT HORIZONTAL STABILIZER PIVOT FITTING ANTI-ROTATION TAB DAMAGED DUE TO SEIZING OF THE INNER/OUTER PIN IN THE VERTICAL STABILIZER BUSHINGS.SDR 5APR20120327113Attach Fitting · out of alignmentTHE HORIZONTAL STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. EACH SIDE OF THE ATTACHMENT FITTING HAS 2 LUGS. ON THE LT SIDE, THESE 2 LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GUAGE, AND FOUND TO BE .0SDR DXTR20120223002Casting · looseFOUND FOUR BOLTS LOOSE AT HORIZONTAL STAB REAR ATTACH CASTING. TORQUED BOLTS IAW MM 20-10-01.SDR ASOA201200550Bushing · corrodedLEFT SIDE HORIZONTAL TO VERTICAL ATTACHMENT POINT BUSHING CORRODED ON VERTICAL. REMOVED THE HORISONTAL STABLIZER IAW AMM 55-10-00-000-801. REPAIRED BUSHING, INSTALLED ORIGINAL HORIZONTAL STABLIZER IAW AMM 55-10-00-400-801.SDR 5APR2011122877100Fitting · out of alignmentTHE HORIZONTAL STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GUAGE, AND FOUND TO BE .635MM. THERE IS NO EVIDENCE OF DAMAGE TO THE STABILIZER.SDR DXTR20111214401Attach Fitting · wornTHE FWD AND AFT HORIZONTAL STAB ATTACH POINTS ARE WORN, ALLOWING HORIZONTAL STAB MOVEMENT BOTH RADIALLY AND UP AND DOWN. THIS MOVEMENT HAS PLAY IN THE HORIZONTAL, SEEMS TO HAVE STARTED TO LOOSEN UP ANOTHER AREA. THE LT SIDE OF THE AFT VERTICAL SPAR HAS AN ARSDR CA111103012Actuator · contaminated(CAN) FLOAT PLANE OPERATOR, TAILPLANE ACTUATOR ASSY GETS WET, WATER HAS TO BE DRAINED AND BEARINGS REPLACED OCCASIONALLY (ANNUAL).SDR A6WA201141061Lug · gougedHORIZONTAL STAB LT OTBD LUG GOUGED. BLENDED DAMAGED AREA NDT INSPECTED FLAP PEENED, ALODINED, PRIMED IAW REO 601R-55-11-391.SDR CA111003011Block · loose(CAN) DURING A REPETITIVE STAB TRIM JACK INSPECTION, NOTED THAT THE BOTTOM JACKSCREW MOUNT WAS LOOSE AND WORKING IN ITS FUSELAGE MOUNTING BRACKET. MOUNTING POINT AND BRACKET WAS REMOVED AND DISASSEMBLED AND THE 3 MOUNTING RIVETS AND THE ASSOCIATED HOLES WERSDR 2011FA0000592Attach Bracket · crackedCRACKS WERE FOUND ON THE REAR HORIZ STABILIZER ATTACHMENT BRACKET ON THE FUSELAGE. 4 EXAMPLE PARTS WERE TURNED IN THE THE CERTIFICATION OFFICE AND ARE BEING FORWARDED TO THE ACO.SDR 2011FA0000544Bolt · looseWHILE COMPLYING WITH AD 11-07-13 LT AND RT ELEVATOR SPAR, IT WAS NOTED THAT THE HORIZONTAL STAB WAS LOOSE AT BOTH THE FRONT AND REAR MOUNTING POINTS. MOVEMENT WAS MOST NOTED AT THE FWD PORTION OF THE STAB WITH A ROCKING MOVEMENT SIDE TO SIDE. UPON INVESTIGATSDR FDEA201108153282Bearing · corrodedRT HORIZ STABILIZER CONSTANT SECTION HINGE BEARING MAKING POPPING NOISE. REMOVED BEARING HAS PITTING CORROSION. R & R BEARING REF AMM 55-51-01-2.SDR 5APR577Y81Attach Fitting · out of alignmentTHE HORIZ STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. EACH SIDE OF THE ATTACHMENT FITTING HAS 2 LUGS. ON THE LT SIDE, THESE 2 LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GUAGE, AND FOUND TO BE .406MMSDR CA110725015Attach Bracket · crackedDURING THE FWD SPAR INSP CF-1991-42R1 THE STAB FORWARD ATTACH FITTING WAS FOUND CRACKED FROM THE TOP ATTACH HOLE TO TOP EDGE OF FITTING. AFTER NDT INSPECTION COMPLETED, A NEW FITTING WAS INSTALLED.SDR 5APR577Y70Fitting · out of alignmentTHE HORIZONTAL STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. EACH SIDE OF THE ATTACHMENT FITTING HAS TWO LUGS.ON THE LEFTSIDE, THESE TWO LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GUAGE,AND FOUND TO BESDR EE4Y20110325Fitting · brokenHORIZONTAL STABILIZER, LT ELEVATOR INBD ACTUATOR FITTING WITH LOCK BROKEN. MAJOR REPAIR.SDR 5APR577Y68Fitting · separatedTHE HORIZONTAL STABILIZER ATTACHMENT FITTING, WHERE THE PITCH TRIM ACTUATOR IS SECURED TO THE STABILIZER. EACH SIDE OF THE ATTACHMENT FITTING HAS 2 LUGS. ON THE LT SIDE, THESE 2 LUGS ARE SEPARATING. THE GAP WAS MEASURED WITH A FEELER GUAGE,AND FOUND TO BE .4SDR UG8A2011050101Mount Fitting · corrodedHORIZONTAL STABILIZER PIVOT BEARING FITTING BORES ARE CORRODED. MADE REPAIRS TO LT LUG IAW FAA APPROVED REPAIR DWG SE05455902 REV A. FIRST OVERSIZE REPAIR INCORPORATED. INSTALLED HORIZONTAL STABILIZERSDR KGBR20110411357Attach Fitting · corrodedHORIZONTAL STABILIZER LEFT (STAB SIDE) FWD ATTACH FITTING HAS LEVEL 3 CORROSION.SDR KGBR20110411355Attach Fitting · corrodedHORIZONTAL STABILIZER RIGHT ATTACH FITTINGS (HSS SIDE) FWD AND AFT FITTINGS HAVE LEVEL 2 CORROSION.SDR 5APR577Y55Fitting · out of alignmentLT SIDE INNER AND OUTER LUG HAVE DEVELOPED A GAP OF .025" BETWEEN THEM. CHECKED LUGGED FACE OF PN 555.10.12.150 ANGLE FITTING FOR STRAIGHTNESS. ALL STEPS COMPLETED WITH NO CRACKS OR DEFECTS NOTED.SDR CA110214013Bracket · crackedTHE PILOT REPORTED AFTER HIS FLIGHT THAT THERE WAS EXCESSIVE PLAY IN THE HORIZONTAL STAB ATTACH AT THE FUSELAGE LT SIDE. CLOSE INSP UNCOVERED THE STRUCTURAL BRACKET PN: 0712042-1 TO BE CRACKED RIGHT THROUGH. THE PART WAS REPLACED WITH A FACTORY SUPPLIED PARTSDR IXXA11SMN046SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE NR 60 ACCESS RT FITTING CRACKED AT STA 1766.000, LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-21, 51-3-0 AND 51-3-1.SDR IXXA11SMN045SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND EMPENNAGE NR 60 ACCESS LT FITTING CRACKED AT STA 1766.000 LONGERON 19. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-21, 51-3-0 AND 51-3-1.SDR KGBR2010112910002Attach Fitting · corrodedCORROSION ON FUSELAGE TO HORIZONTAL STABILIZER ATTACH FITTINGS.SDR KGBR2010112910001Attach Fitting · corrodedCORROSION ON FUSELAGE TO HORIZONTAL STABILIZER ATTACH FITTINGS.SDR 2010FA0001250Attach Bracket · corrodedBOTH LT AND RT FWD HORIZ STABILIZER ATTACH BRACKETS WERE INSTALLED AS PART OF THE AOG AIR SUPPORT WING ANGLE MOD (STC SA01258NY) DURING ANNUAL INSP FOUND HORIZ STABILIZER FWD ATTACH TO BE LOOSE. PART IS ATTACHED TO THE FWD SPAR OF THE HORIZ STABILIZER WITH 2 SDR 2010FA0001229Attach Bracket · crackedDURING ROUTINE ANNUAL INSP, THE RT FWD HORIZ STABILIZER ATTACH BRACKET WAS FOUND CRACKED. SB87-2 CALLS FOR KIT 210-118 TO BE INSTALLED. THE NEW FITTINGS PN 21320191 ARE BEEFED UP AND THE BULKHEAD IS ALSO. DUE TO THE CRITICAL NATURE OF THIS ATTACH FITTING, ISDR 2010FA0000884Fitting · crackedRUDDER TRIM TAB ACTUATOR FITTING IS CRACKED ON LOWER LUG. CRACK EXTENDS FROM BEARING BORE THROUGH THE ENTIRE LUG THICKNESS. CRACK ORIGINATED AT SPOTS WHERE BEARING WAS STAKED INTO LUG.SDR EHAA20100728Attach Fitting · crackedTHE SIXTH (OF EIGHT) AIRFRAME SIDE HORIZONTAL STABILIZER FITTINGS WERE REMOVED AND FOUND TO BE CRACKED. THIS AIRCRAFT IS GOING THRU A COMBINED 1, 2 AND 4 YEAR CORROSION INSPECTION.SDR 2010FA0000729Attach Fitting · cracked3 EA, FUSELAGE SIDE, HORIZ STABILIZER ATTACH FITTINGS WERE FOUND TO BE CRACKED AND 3 OTHERS WERE FOUND WITH INTERGRANULAR CORROSION. 6 OF THE 8 ARE BEYOND LIMITS. ONE OF THE FITTINGS THAT SHOWED NO SIGNS OF CRACKS OR CORROSION WAS REMOVED AND FOUND TO BE BADLSDR CA100608011Fitting · wornDURING MX IN THE AREA, MOVEMENT WAS FOUND BETWEEN THE HORIZ STABILIZER REAR SPAR CONNECTOR FITTING, PN 77-121021(LWR) AND THE REAR SPAR. FURTHER MOVEMENT WAS ALSO FOUND AT PN 52-31107 (FITTING -FUSELAGE HORIZ STABILIZER REAR ATTACHING LT) WHERE IT MOUNTS TO PSDR 2010FA0000483Attach Bracket · corrodedFOUND RT STABILATOR ATTACH BRACKET EXFOLIATED.SDR 2010FA0000346Hinge Fitting · crackedHORIZ STABILIZER LT 2 PLACES 0.9 INCH AND 0.8 INCH & RT 2 PLACES 1.1 INCH AND 0.85 INCH, HINGE FITTING CRACKED.SDR 5APR577Y34Lug · separated(5APR) THE HORIZONTAL STAB PN 555.10.12.037, SN 815, FWD PITCH TRIM ACTUATOR ATTACHMENT FITTING LT OTBD LUG PN 555.10.12.150, IS SEPARATED FROM THE CTR SECTION OF THE FITTING BY 0.76 MM'S. OTBD ATTACHMENT LUGS ARE NORMALLY ALIGNED WITH THE CTR SECTION OF THE SDR FDEA201002020304Attach Fitting · crackedVISUAL CRACK INDICATION ON THE LT HORIZ STABILIZER L/E INTERIOR AREA AT THE FWD ATTACHED FITTING OF THE LOWER CHORD, VIEWED THRU ACCESS PANEL 331-AZ (INBD SIDE). R & R FITTING AT LT HORIZONTAL STABILIZER L/E REF. SRM 51-00-01 VOLUME 1.SDR ASAA0976776Lug · gougedLT HORIZONTAL STAB STA 92.7 RIB FRONT SPAR UPPER CLEVIS AFT LUG AFT FACE UPPER EDGE GOUGED. REPAIRED PEER EASDR DLM88091500Hinge Fitting · wornDURING HMV WEAR WAS FOUND ON EDGE OF LT INBOARD BUSHING OF LT HORZ STAB ATTACHMENT. HORZ STAB ATTACHMENT WAS REPAIRED IAW SRM 55-02 PARA 24.SDR DLM88091498Hinge Fitting · corrodedDURING HMV FRETTING CORROSION WAS FOUND ON INNER SURFACE OF RIGHT OUTBOARD BUSHING OF RIGHT HORZ STAB ATTACHMENT. RIGHT HORZ STAB ATTACHMENT REPAIRED IAW SRM 55-02 PARA 24.SDR CA090722008Fitting · broken(CAN) 10TH-100 HR INSP REVEALED SLIGHT `GIVE` OR PLAY BETWEEN TAILBOOM AND RT HORIZONTAL MOUNT FITTING. VISUAL INSP SHOWED NOTHING. HORIZONTAL STABILIZER WAS TIGHT IAW PROPER INSTALLATION. FURTHER DISASSEMBLY OF RT STABILIZER FROM TAILBOOM REVEALED MOUNTINGSDR GUUA94355071709CHinge Bracket · corrodedDURING ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.SDR GUUA94355071709BHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OTBD HINGE BRACKET.SDR GUUA94355071709AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CTR HINGE BRACKET.SDR CA090615004Attach Fitting · cracked(CAN) DURING THE COMPLETION OF AD CF-1991-42R1, STAB ATTACH FITTING WAS FOUND CRACKED FROM UPPER MOUNTING HOLE TO EDGE OF FITTING, PART WAS REPLACED.SDR FPI2009F00000Attach Bracket · crackedCRACK FOUND IN LT HORIZONTAL STAB BRACE. FOUND DURING 100 HR PHASE INSP.SDR CA090522003Attach Fitting · cracked(CAN) WHILE PERFROMING A ROUTINE 50 HOUR INSP, IT WAS NOTICED THAT THERE WAS EXCESSIVE VERTICAL MOVEMENT ON THE RT SIDE OF THE HORIZONTAL STABILIZER. UPON FURTHER INVESTIGATION, THE RT FWD ATTACH FITTING WAS FOUND CRACKED COMPLETELY THROUGH, JUST BELOW THE BOLSDR QXEA2009051100324Lug · gougedPDX - C5 - FOUND SMALL GOUGE IN THE AFT SIDE ANTI ROTATION LUG DURING REINSTALLATION OF PINS AND BOLTS. REMOVED LT OUTER PIN IAW RIL 0146 STEP 3 AND 4 ALL OTHER STEPS PREVIOUSLY COMPLIED WITH. ELIMINATED GOUGE ON LT AFT SIDE ANTI ROTATION LUG PER REO 670-55-SDR QXEA2009051100323Lug · crackedPDX - C5 - RT OTBD HORIZONTAL STAB LUG HAS A SMALL CRACK (APPROX .125 INCH) ON UNDER SIDE OF ANTI ROTATION TAB ON AFT SIDE. FPI INSPECTED AT THE AREA IAW CRJ700 NDTM PART 1, 51-20-008 CRACK INDICATION CONFIRMED IAW CRJ 700 NDTM PART 1 51-20-006. MAPPED DAMASDR QXEA2009051100322Lug · damagedPDX - C5 - RT OTBD HORIZONTAL STAB LUG P/N AV670-23000 APPEARS TO HAVE BEEN BLENDED BELOW ANTI-ROTATION TAB ON AFT SIDE. BLENDED OUT DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00-001-001-A01 STEPS 1-3, 5.B(1)-(2). MAPPED FOR ENGINEERING. REMOVED DAMAGE IAW TCSDR ASAA0945508Bracket · crackedLT HORIZONTAL STAB NR 5 GAP PANEL BRACKET ASSY CRACKED AT LOWER INBD SPT. REMOVED AND REPLACED.
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