JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer Structure, 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 = '5510' 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 = '5510' 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 AU981617Fitting · cracked(AUS) DURING 4C CHECK, TWO CRACKS WERE FOUND AT LT LOWER SUPPORT ANGLE WHERE HORIZONTAL STABILIZER JACK SCREW PRIMARY SUPPORT BEAM ATTACHES TO STAR TRUSS. IN ADDITION, FOUR ATTACH BOLTS WERE SHOWING SIGNS OF LOOSENESS. CRACKS RAN UPWARD IN RADIUS OF ANGLE, CSDR CA980908021Fitting · worn(CAN) WORN BUSHINGS AND FITTINGS FOUND AT TAILPLANE ATTACHMENT TO FUSELAGE. A CRACKED GUSSET BETWEEN VERTICAL AND HORIZONTAL STABILIZER FOUND. FURTHER INVESTIGATION DETERMINED THAT THE CAUSE OF THE CRACK WAS THAT THE AFT ATTACHMENT OF THE TAIL PLANE WAS LOOSSDR HEEA0015592Stabilizer · corrodedSTABILIZER CORRODED UNDER CENTER DOUBLER.SDR HEEA0015554Stabilizer · unbondedSTABLIZER SEPARATED BEYOND LIMITS.SDR HEEA0015489Stab Assy · corrodedSTABILIZER ASSEMBLY CORRODED BEYOND LIMITS.SDR UPS98227198Beam · corrodedINSPECTION TYPE-C, RT STAB UPPER SURFACE T/E BEAM HAS SEVERAL AREAS OF CORROSION FROM I/B TO O/B. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-1. BEAM REPLACED IAW DRAWING NR 65-22987.SDR UPS98227197Beam · corrosionINSPECTION TYPE-C, SURFACE CORROSION ON LT STAB UPPER T/E BEAM FROM I/B TO O/B END. T/E BEAM REPLACED IAW DRAWING NR 65-22987.SDR 98ZZZX2665Channel · crackedUPON INPSECTION, THE HORIZONTAL STABILIZER LEFT SUPPORT AFT CHANNEL WAS FOUND CRACKED IN THE UPPER AND LOWER BEND RADII. THE CHANNEL HAD A LARGE BOW FROM TOP TO BOTTOM AND WAS NOT RESTING AGAINST THE SPAR. POORLY FIT. (FROM MFG).SDR SWAA981286Angle · crackedDURING SCHEDULED TRAN CHECK, FOUND CRACKED AND GOUGED L-ANGLE BEHIND PANEL 9224 ON RT HORIZ STAB. REMOVED AND REPLACED PER BOEING SRM.SDR ABXA9800608Tee Cap · corrodedDURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER AFT UPPER TEE CAP EXFOLIATED AT HINGE POINT, AT STATION 204. REPAIRED TEE CAP IAW ABX REA D955-23948 MR.SDR 99ZZZX5Stringer · crackedDISCOVERED SEVERAL SMALL CRACKS INSIDE HORIZONTAL STABILIZER LOCATED AT LEFT AND RIGHT BL 19.40. CRACKS WERE NOTED DURING SCHEDULED INSPECTION OF THE AREA. A REPAIR WAS PERFORMED BY AN FAA CERTIFIED REPAIR STATION, FOLLOWING N.D.T. CONFIRMATION OF THE CRACKSSDR AALA981193Angle · corrodedTUL - UPPER T/E CHORD ON RT HORIZ STAB HAS CORROSION APPROX 16 INCHES INBOARD OF NR 7 ELEV HINGE. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER ESO DATED 6/10/98. (M)SDR AALA981192Angle · corrodedTUL - FOUND LEFT UPPER T/E CHORD ON LEFT HORIZ STAB HAS CORROSION APPROX 16 INCHES INBOARD OF NR 6 ELEV HINGE. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER ESO 11697, DATED 6/10/98. (M)SDR UPS98227080Beam · corrodedINSPECTION TYPE-C, CORROSION ON HORIZONTAL STAB TRAILING EDGE UPPER SURFACE AT STAB STATION 188.65 LT. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-19-008, UPS ENGINEERING FILE NUMBER 727-55-0372.SDR HEEA0014816Stabilizer · mislocatedHORIZONTAL STABI8LIZER HAS TWO EACH INSERTS LOCATED WRONG PLACE AND THEN FILLED.SDR 98ZZZX3185Fitting · crackedWHILE C/W AD 98-10-12, THE FITTING REQUIRED REPLACEMENT PER PARA (A)(2). INSPECTION OF THIS FITTING PER REVO SB B-78 DISCLOSED A CRACK IN ADDITION TO CORROSION AND FRETTING. IT SHOULD BE NOTED EVEN AFTER REPLACEMENT OF AFFECTED FITTINGS, THE ACFT IN MOST CASSDR 98UAL900296Tube · crackedA 1.2 INCH CRACK WAS FOUND IN 65B02668-3 DIAGONAL SUPPORT TUBE AT STA 2598 HORIZONTAL STABILIZER HINGE SUPPORT BULKHEAD. CRACK WAS AT UPPER END OF TUBE, BEGINNING AT TUBE EDGE AND RUNNING DOWN THROUGH FIRST ROD END ATTACH FASTENER HOLE. TUBE ASSEMBLY REPLACESDR AU980631Hinge · cracked(AUS) LT HORIZONTAL STABILIZER OUTBOARD HINGE ASSEMBLY CRACKED.SDR UPS98827122Fitting · crackedINSPECTION TYPE:D, RT HORIZ STAB L/E ON THE INBD END THE UPPER AND LOWER TEE FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 53-1-0.SDR 98ZZZX2491Beam · corrodedDURING C-CHECK, EXFOLIATION CORROSION ON LEFT HORIZONTAL UPPER TRAILING EDGE BEAM BETWEEN STA 99.8 AND STA 136.5.SDR 98ZZZX3088Support · missingDURING POST-FLIGHT INSPECTION, THE SPOILER TO THE LT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND MISSING AND HAD STRUCK ONE TAIL ROTOR BLADE CAUSING MINOR DAMAGE. THERE WAS NO FEED BACK IN THE CONTROLS DURING FLIGHT THAT WOULD HAVE WARNED OF ANY IMPACT TO THESDR 98ZZZX3087Support · crackedAFTER BEING NOTIFIED THAT ONE OTHER AIRCRAFT IN FLEET HAD LOST ITS SLAT, SUBMITTER C/W VISUAL INSPECTION AND FOUND THE HORIZONTAL STABILIZER SLAT SUPPORT ON THE RT SIDE CRACKED. TWO EACH. TWO OUTBOARD SLAT SUPPORTS CRACKED IN RADIUS AREA OF SUPPORT TO HORIZOSDR 98ZZZX3086Support · crackedAFTER BEING NOTIFIED THAT ONE OTHER AIRCRAFT IN FLEET HAD LOST ITS SLAT, SUBMITTER C/W VISUAL INSPECTION AND FOUND THE HORIZONTAL STABILIZER SLAT SUPPORT AT THE MID-INBOARD SUPPORT CRACKED ON THE LT SLAT, ONE EACH. ONE MID-INBOARD SLAT SUPPORT CRACKED IN RADISDR 98ZZZX2535Support · crackedAFTER BEING NOTIFIED THAT ONE OTHER AIRCRAFT IN FLEET HAD LOST ITS SLAT, C/W A VISUAL INSPECTION AND FOUND THE HORIZONTAL STABILIZER SLAT SUPPORT AT THE MID-INBOARD SUPPORT CRACKED ON THE LT SLAT. ONE EACH. ONE MID-INBOARD SLAT SUPPORTS CRACKED IN RADIUS ARESDR 98ZZZX2530Support · crackedAFTER BEING NOTIFIED THAT ONE OTHER AIRCRAFT IN FLEET HAD LOST ITS SLAT, C/W A VISUAL INSPECTION AND FOUND THE HORIZONTAL STABILIZER SLAT SUPPORT ON THE RT SIDE CRACKED. TWO EACH. TWO OUTBOARD SLAT SUPPORTS CRACKED IN RADIUS ARE OF SUPPORT TO HORIZONTAL STABSDR SWAA980965Angle · crackedDURING SCHEDULED D CHECK, FOUND LT HORIZ STAB WEB AT HSS 175.5 HAS CRACKED L ANGLE STIFFENER APPROX 30 AFT OF FRONT SPAR. REPAIRED PER BOEING SRM.SDR SWAA980962Tip · crackedDURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB TIP HAS 2 CRACK INTERNAL AND EXTERNAL SURFACES 4 FROM L/E AT LOWER EDGE. REMOVED AND REPLACED PER BOEING SRM.SDR AALA981056Beam · corrodedTUL - FOUND CORROSION ON UPPER SURFACE OF RT HORIZ STAB TE BEAM FORWARD OF 4TH FROM OUTBOARD ELEV HINGE. COMPLETED REPAIR BY INSTALLING DOUBLER AS PER ESO 11697 AND SRM 55-10-6. TREATED, PRIMED AND SEALED AREA. (M)SDR UPS98827594Linkage Box · crackedINSPECTION TYPE-C/CK, LEFT HAND HORIZONTAL STABILIZER OUTBOARD GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 216. REMOVED TAB LINKAGE COVER IAW DC8 SRM 51-1-21, WELDED BOX IAW DC8 1 0.301 AND DAC DWG 5652086, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REINSTALLED SDR 98ZZZX2136Brace · failedDURING AN ANNUAL INSPECTION, A RATTLING SOUND WAS DISCOVERED IN THE LEFT HORIZONTAL STABILIZER. FURTHER INVESTIGATION REVEALED THE TRACK WELD SECURING THE DIAGONAL BRACE TO THE BUTT RIB HAD BROKEN LOOSE DUE TO AN INADEQUATE WELD. THE DIAGONAL BRACE IS NOT A SDR 98ZZZX2282Reinforcement · crackedAT ANNUAL INSPECTION, FOUND LEFT AND RIGHT STABILIZER HINGE REINFORCEMENTS CRACKED. LEFT FITTING CRACKED FROM AFT EDGE TO BOLT HOLE AT INBOARD LOWER TAB. RIGHT FITTING HAD SIMILAR CRACKS IN BOTH LOWER TABS. NOT SO OBVIOUS WAS A CRACK ALONG 90 PERCENT OF THESDR HEEA0014196End Plate · crackedHORIZ STAB V FIN VERT END PLATE HAS THREE INCH CRACK AFT OF MOUNTING FLANGE.SDR AALA981505Beam · corrodedTUL - UPPER TE BEAM HAS CORROSION ON TOP SURFACE OF BEAM, ABOVE NR 4 RIB SUPPORT CASTING. REF E58 NR 0123429. REMOVED CORROSION PER SRM 51-10-6. INSTALLED BEAM REPAIR PER SRM 55-10-6 AND ESO 11697 DATED 7/14/98. (M)SDR 98ZZZX2417Bolt · misinstalledPER BOEING TELEX M-7200-98-01560, 5-5-98, PRO AIR ELECTED TO ACCOMPLISH A ONE-TIME INSP OF THE HORIZ STAB/ELEVATOR ATTACH FITTINGS TO IDENTIFY ANY FASTENERS INSTALLED DURING MANUFACTURING THAT HAD INCORRECT GRIP LENGTH. AS A RESULT OF THIS INSP, ALL 20 FASTENSDR CALA9800753Access Panel · delaminatedHORIZ STAB ELEVATOR PCU ACCESS PANEL DELAMINATED 3 X 10. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND BONDED TO PANEL PER SRM 55-20-3 AND 51-40-5.SDR CA980602022Stabilizer · damaged(CAN) DURING POST HMV ENGINE RUNS, A LARGE PIECE OF ASPHALT DISLODGED STRIKING THE TRIMMABLE HORIZONTAL STABILIZER LT SIDE CAUSING UNREPAIRABLE DAMAGE. T.H.S. REPLACED AND REPAIR TO FUSELAGE SKIN CARRIED OUT. INSPECTIONS TO SURROUNDING STRUCTURES AND VERTICASDR MWEA98576Tip · erodedFOUND A HOLE ERODED IN THE LEFT HORIZONTAL STABILIZER LEADING EDGE TIP. MTC FABRICATED AND INSTALLED DOUBLER.SDR UF6A980423Spar · crackedSBN - MX - CRACK FOUND ON FRONT SPAR OF LEFT HAND HORIZONTAL STABILIZER AT STA 42.00 TOP EDGE. MAINTENANCE STOP DRILLED CRACK AND INSTALLED SINGLE FLANGE REPAIR. (X)SDR TWAA9806412Barrel Nut · rustedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT RT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACH TO CENTER SECTION WAS RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. REMOVED BOLT AND BARREL NUT AND CLEANED. REAMED AND BUSHED HOLE PSDR EIAA980201Fitting · misdrilledDURING 'C5' CHECK, HORIZONTAL STABILIZER CENTER SECTION UPPER AFT FITTING HAS CORROSION. DURING REPLACEMENT, FITTING WAS MISDRILLED. REPLACED FITTING AND REPAIRED AREA IAW ECRA 944-55-033-02. (X)SDR TSAA9855214Bushing · corrodedHORIZONTAL STABILIZER RT SIDE UPPER AFT BUSHING CORRODED. REPAIRED BUSHING PER ECO 2895. BLEND OUT DIMENSION 1.2560 INCH BY 1.2640 INCH. AIRCRAFT RETURNED TO SERVICE. (M)SDR TWAA9807306Horiz Stab · gougedMCI - DURING OP16 MAINTENANCE CHECK, FOUND ON LT HORIZ STAB TOP AFT 2 BARREL NUT HOLES GOUGED. REAMED HOLES AND INSTALLED BUSHING AND REDRILLED .562 IN PER ARA 15267. (M)SDR ABXA9800320Bracket · crackedDURING C-CHECK, FOUND THE BRACKET BELOW AND INBOARD OF NR 1 LEFT ELEVATOR HINGED BEARING CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-2.SDR 98ZZZX1489Hinge Fitting · crackedINSPECTION FOUND CRACKS IN HORIZONTAL STABILIZER AFT SPAR SPLICE HINGE FITTING. TAT: 8,363.6 HOURS. LANDINGS: 5,993.SDR DL72S980697Bushing · wornLT HORIZ STAB NR 1 HINGE ATT PT FUS ELEV, FITTING AND BUSHINGS ARE WORN. SPOTFACE I/B FACE OF O/B LUG .012 REMOVED BUSHINGS, CLEANED LUG WITHIN LIMITS PER MM 55-50-0 FIG 801. ROTOPEENED PER PS900-4 TREAT FACES AND BORES. PAINTED FACES AND BORES. TURNED BUSSDR G60A018Fairing · crackedGROUND MAINTENANCE FOUND PART OF THE LEFT AFT HORIZONTAL STABILIZER TRAILING EDGE UPPER SIDE MISSING. GROUND MAINTENANCE PERFORMED AN INTERIM REPAIR IAW BOEING TELEX SEQUENCE 9809446. AIRCRAFT RETURNED TO SERVICE. (M)SDR CALA9800587Pivot Plates · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED. THE PIVOT PLATES WERE REPLACED IAW SRM 51-30-5.SDR DL72S980696Bushing · wornBUSHINGS WORN RT HORZ STAB. NR 1 HINGE ATTACH PT FOR ELEV FITTING BUSHINGS ARE WORN. ALSO, HARDWARE IS WORN AND FITTING LUGS ARE WORN. SPOTFACED .013 ON D/B FACE OF I/B LUG AND .010 ON I/B FACE OF O/B LUG. REMOVED BUSHINGS AND CLEANED LUGS WITHIN LIMITS PESDR SWAA980349Strap · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED STABILIZER STRAP AT BS 331 LBL 46 WL 200. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA980334Beam · crackedDURING SCHEDULED D-CHECK, FOUND UPPER RT HORIZONTAL STAB TRAILING EDGE BEAM CHANNEL CRACKED STUB AT BS 92. REPAIRED PER BOEING SRM.
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