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 GUUA07120602Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET.SDR GUUA07120601Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET.SDR CALA0600239Brace · corrodedINSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE RT LOWER I/B CHORD CORRODED BETWEEN STA 1104 AND 1112. THE AREA WAS REPAIRED IAW ECRA 5510-01840.SDR 06FDEA2003Panel · damagedFOUND SEVERAL DAMAGED CAMLOCK FASTENER HOLES ON PANEL 9115. REPAIRED PANEL 9115 IAW FED-EX EA 7-5510-100550.SDR CA060516004Reinforcement · crackedEXCESSIVE MOVEMENT FOUND AT AFT LT HINGE ASSY, INSIDE REINFORCEMENT P/N 0732106-1, ALSO FOUND CRACKED.SDR 06FDEA1881Repair · misinstalledPREVIOUS REPAIR FOUND LOCATED ON THE RT NUMBER ONE SPOILER UPPER SURFACE. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 FIG. 203 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR"SDR AMTA200600329Pin · damagedLOWER PIN THAT ATTACHES LT HORIZONTAL STAB HAS PLATING DAMAGE. REPLACED NEW PIN BOLT IN LOWER LT POSITION HORIZONTAL STAB ATTACH IAW 27-41-11-4. (K)SDR AMTA200600328Pin · damagedLOWER RT ATTACH PIN BOLT AT HORIZONTAL STAB HAS PLATING DAMAGE. INSTALLED NEW LOWER RT PIN IAW 27-41-11-4. (K)SDR AMTA200600327Pin · damagedMID PIN THAT ATTACHES RT HORIZONTAL STAB HAS PLATING DAMAGE. REPLACED PIN IAW 27-41-11-4. (K)SDR UPS06446920Hinge Bracket · crackedBS 2598 B/H STABILIZER HINGE SUPPORT FITTING AREA 1EA HOLE CORROSION CRACK AT FRAME SUPPORT (4TH LAYER FROM AFT) CRACK LENGTH 0.030". BOTH HOLE REWORKED TO 0.500" AS PER EO B747-5310-14056 HOLE CONFIRMED CRACK FREE.SDR 06FDEA1678Bracket · crackedCRACK SUPPORT BRACKET FOR TAIL FUEL TRANSFER PIPE IN EMPERAGE.SDR 06FDEA1601Structure · damagedLT INBOARD AILERON INBOARD TRAILING EDGE FOUND AN IMPACT DAMAGED.SDR UIEA200600107Web · crackedCRACKED WEB AND LOWER CHORD AT THE RT HORIZONTAL STABILIZER STA BL 421.50. WEB AND LOWER CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-17410726 AND FAA FORM 8100-9.SDR UIEA200600104Web · crackedLT HORIZONTAL STAB, UPPER CHORD AT STAB BL 421.5 FOUND 1/2" CRACK AT AFT END. CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-176012397 AND FAA FORM 8100-9.SDR CA060422002Hinge Fitting · gouged(CAN) RT HORIZONTAL STAB NR 1 ELEVATOR HINGE FITTING LOWER PORTION HAS A GOUGE REPAIRED IAW CUSTOMER EA. (TC NR 20060422002)SDR USAA060578Stiffener · crackedSTA 92.7 24 INCHES AFT OF REAR SPAR CRACKED. FABRICATED AND INSTALLED PART IAW SRM 51-10-02, DEFECT SIZE: .500 INCH.SDR USAA060557Hinge · damagedSTAB FASTENER HOLE AT NR 6 BEARING HINGE ELONGATED. OVERSIZED HOLES AND TREATED AREA IAW TR 55-50-01A, DEFECT SIZE: .031 INCH.SDR USAA060554Hinge · damagedSTAB FASTENER HOLE AT NR 6 BEARING HINGE ELONGATED. OVERSIZED HOLES AND TREATED AREA IAW TR 55-50-01A, DEFECT SIZE: .0312 INCH.SDR QXEA200601061Structure · corrodedYYC - C4 RIGHT HORIZONTAL STABILIZER ELEVATOR HORN HAS FRETTING DAMAGE ON INTERNAL REBATE ALONG INBOARD EDGE. REPAIRED IAW DHC-8-200 CORROSIOON PREVENTION MANUAL CHAPTER 4, PART 1 AND DHC-8 MM 20-21-03, PAGES 1-7.SDR ASAA0610350Structure · corrodedCARRY OUT CASCADE ERO 5344 RT HORIZ STAB FRONT AND REAR SPAR BUSHING INSPECTION AND REPLACEMENT DUE TO CORROSION. ERO 5334 PARTS 1 TO PART 16 AS APPLICABLE TO RT HORIZ STAB AND AS EA 5510 01235.SDR UPS06M46964Panel · corrodedHORIZ STAB POSITION NR R22 BARREL NUT BORE SIDEWALL AND BOTTOM FACE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 38, BORE REAMED TO 1.067" OD REMAINING BLEND OUT 0.025"DEEP AND EXCEED LIMIT. MAGNIFY DVI C/OUT FOUND NO CORROSION. FAB AND PROTSDR 2006FA0000373Bracket · cracked3 CRACKS WHERE FOUND ON THE TOP RT OB BOLT HOLE AND ONE CRACK IN WELD JUST AFT OF SAME BOLT HOLE, (NUT PLATES HAD BEEN PREVIOUSLY REMOVED). UNKNOWN CAUSE, AD SHOULD BE REVISED TO REFER FURTHER INSPECTION OF COMPLETE BRACKET ASSY. (K)SDR 2006UALA00432Bushing · migratedLT HORIZ STAB FWD SPAR UPPER LUG FWD & AFT BUSHINGS MIGRATED. REMOVED BUSHINGS, FOUIND CORROSION, REMOVED CORROSION, FABRICATED ADN INSTALLED NEW BUSHINGS PER BOEING DRAWINGS 65-72039-29, 30, AND 31. WORK ACCOMPLISHED PER AAR EA I060104 AND SUPPORTED WITH 810SDR 06FDEA0958Rib · crackedWITH REFERENCE TO FEDEX EA 1-5510-94597, LEFT HAND HORIZONTAL STABILIZER FORWARD UPPER RIB CAP AT STA XE = 51.00 FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5510-94611.SDR DHL2006804519Stiffener · crackedRIGHT HORIZONTAL STABILIZER STIFFENER CRACKED 1 INCH XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED STIFFENER (AL7075"0" 0.063") IAW SRM 55-3-0 PG 8. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TSDR DHL2006804518Stiffener · crackedLT HORIZONTAL STABILIZER STIFFENER CRACKED 1 INCH XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (AL7075"0" 0.063") IAW SRM 55-3-0 PG 8. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED TSDR UPS06M46732Bushing · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 8L EXISTING REPAIR BUSHING FOUND CORRODED. CORRODED REPAIR BUSHING REMOVED. CORROSION AT BORE REMOVED. BOTTOM SURFACE CLEANED, REMAINING BLEND OUT AT BORE 0.035"DEEP EXCEEDED LIMIT. DVI CARRIED OUTSDR UPS06M46731Bushing · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 11L EXISTING REPAIR BUSHING FOUND CORRODED. CORRODED REPAIR SLEEVE BUSHING REMOVED. CORROSION AT BORE REMOVED, REMANING BLEND OUT AT BORE 0.050" DEEP, EXCEEDED LIMIT. VISUAL INSPECTION CARRIED OUT, SDR UPS06M46730Bushing · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 5L EXISTING REPAIR BUSHING FOUND CORRODED. CORRODED SLEEVE BUSHING REMOVED. CORROSION AT BORE REMOVED. SURFACE CLEANED, REMAINING BORE BLEND 0.020" EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUNSDR UPS06M46695Bushing · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE NR 23L EXISTING REPAIR BUSHING CORRODED. CORRODED SLEEVE BUSHING (1.067"DIA) REMOVED. CORROSION AT BORE REMOVED, SIDEWALL REMAINING BLEND OUT 0.010" EXCEEDED LIMIT. VISUAL INSP FOUND NO CORROSION. BORSDR UPS06M46693Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE NR 17L EXISTING REPAIR BUSHING CORRODED. CORRODED REPAIR BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT AT SIDEWALL 0.050" DEEP, BOTTOM 0.015" DEEP EXCEEDED LIMIT. VISUAL INSP FOUND NO CORROSION. BORE SSDR UPS06M46673Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE 18R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING (1.089"DIA) REMOVED. CORROSION AT BORE REMOVED REMAINING SIDEWALL BLENDOUT 0.050" EXCEEDED. DVI CARRIED OUT AND NO CORROSION FOUND. BARREL NUT BORE AND BLENSDR UPS06M46672Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE NR 6R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLENDOUT AT SIDEWALL 0.160"DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLENDSDR UPS06M46671Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE NR 12R EXISTING REPAIR BUSHING CORRODED. CORRODED SLEEVE BUSHING REMOVED (1.067"DIA). CORROSION AT BORE REMOVED REMAINING BLEND OUT AT BOTTOM 0.035", SIDEWALL 0.130" DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUSDR UPS06M46669Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE NR 9R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT 0.200" EXCEEDED LIMIT. BARREL NUT BORE CLEANED AND PROTECTED. DVI CARRIED OUT AND NO CORROSION FOUNSDR UPS06M46668Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE NR 2R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT 0.080"DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLEND OUT SMOOTHSDR UPS06M46667Bushing · corrodedHORIZONTAL STABILIZER BARREL NUT HOLE NR 15R EXISTING REPAIR BUSHING CORRODED. CORRODED BUCKET BUSHING REMOVED. CORROSION AT BORE REMOVED REMAINING BLEND OUT AT SIDEWALL 0.040" DEEP EXCEEDED LIMIT. DVI CARRIED OUT NO CORROSION FOUND. BARREL NUT BORE AND BLSDR UPS06M46694Bushing · corrodedINSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT HOLE 36L EXISTING BUSHING FOUND WITH CORROSION. REPAIR SLEEVE BUSING REMOVED. CORROSION AT BORE REMOVED. BOTTOM BLEND OUT 0.075 DEEP, BEARING/SIDEWALL REMAINING 0.065" EXCEEDED LIMITS. DVI CARRIED OUT NO CSDR UPS06M46670Bushing · corrodedHORIZONTAL STABILIZER BOLT HOLE 1R EXISTING REPAIR BUSHING FOUND WITH CORROSION. EXISTING REAPIR BUSHING REMOVED. CORROSION REMOVED, BOTTOM 0.100"DEEP B BEARING/SIDEWALL REMAINING BLENDOUT 0.170"DEEP EXCEEDED LIMIT. VISUAL INSP CARRIED OUT NO CORROSION FOUNSDR 06FDEA0325Repair · misinstalledFOUND REPAIR LOCATED AT LT HS 330-350 REPAIR REQUIRES EVALUATION FOR MAJOR - MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SDR 06FDEA0324Repair · misinstalledFOUND REPAIR LOCATED LT HS683-696. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-SDR QXEA200600378Fitting · tool damageYYC - C3 LEFT HAND HORIZONTAL STABILIZER PIVOT FITTING HAS TOOL MARK. REPARIED IAW HORIZON AIR EA R-55-45 AND REO 670-55-11-031.SDR USAA200601001Rib · crackedA 3 INCH CRACK ON RIB 7 RT HORIZ STAB TIE. INSTALLED DOUBLER PER EA M00729.SDR UPS06M46286Structure · corrodedINSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 19 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 19 LEFT BORE & BOTTOM REWORKED PER EN1033-06. FAB SLEEVE BUSDR UPS06M46282Structure · corrodedINSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 22 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE NR 22 LT BORE REWORKED PER EN1032-06. FAB SLEEVE BUSHING PESDR C2XA06TY002Housing · gougedRT HORIZ STAB SPHERICAL BEARING HOUSING GOUGED. REWORKED HOUSING TO 1ST OVERSIZE W/ ENGINEERING APPROVAL. ALL WORK C/W IAW EC5510-01130, EC551-01080, EMB-145 AMM 55-37-00.SDR UPS06M46281Structure · corrodedINSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE 16 LEFT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL C/OUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. BARREL NUT HOLE 16 LEFT BORE & BOTTOM REWORKED PER EN1022-06. FAB SLEEVE BUSDR QXEA200600041Structure · chafedPDX - RIGHT H-STAB BOTTOM FLANGE SURFACE HAS VARIOUS CHAFE MARKS AT OUTBOARD END WHERE LEADING EDGE 342BR ATTACHES. REPAIRED IAW RD 8-55-626, DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.SDR QXEA200600042Structure · chafedPDX - CHAFE ON LEFT H-STAB UPPER FLANGE SURFACE AT OUTBOARD END WHERE LEADING EDGE 332BL ATTACHES. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16 AND SRM 51-20-36.SDR USAA051646Clevis · corrodedFOUND CLEVIS R1 ON HORIZ STAB CORRODED. REMOVED CORROSION, REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".
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