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.

SDR GUUA07120602Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET.Jul 12, 2006 · N81556 · Beech 1900DSDR GUUA07120601Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET.Jul 12, 2006 · N81556 · Beech 1900DSDR 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.Jul 3, 2006 · N69348 · Boeing 7373T0SDR 06FDEA2003Panel · damagedFOUND SEVERAL DAMAGED CAMLOCK FASTENER HOLES ON PANEL 9115. REPAIRED PANEL 9115 IAW FED-EX EA 7-5510-100550.May 24, 2006 · N493FE · Boeing 727227SDR CA060516004Reinforcement · crackedEXCESSIVE MOVEMENT FOUND AT AFT LT HINGE ASSY, INSIDE REINFORCEMENT P/N 0732106-1, ALSO FOUND CRACKED.May 13, 2006 · Cessna A185FSDR 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"May 12, 2006 · N450FE · Airbus A310222SDR 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)May 11, 2006 · N314TZ · Boeing 73783NSDR AMTA200600328Pin · damagedLOWER RT ATTACH PIN BOLT AT HORIZONTAL STAB HAS PLATING DAMAGE. INSTALLED NEW LOWER RT PIN IAW 27-41-11-4. (K)May 11, 2006 · N314TZ · Boeing 73783NSDR AMTA200600327Pin · damagedMID PIN THAT ATTACHES RT HORIZONTAL STAB HAS PLATING DAMAGE. REPLACED PIN IAW 27-41-11-4. (K)May 11, 2006 · N314TZ · Boeing 73783NSDR 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.May 10, 2006 · N521UP · Boeing 747211BSDR 06FDEA1678Bracket · crackedCRACK SUPPORT BRACKET FOR TAIL FUEL TRANSFER PIPE IN EMPERAGE.May 2, 2006 · N526FE · Doug MD11SDR 06FDEA1601Structure · damagedLT INBOARD AILERON INBOARD TRAILING EDGE FOUND AN IMPACT DAMAGED.Apr 26, 2006 · N526FE · Doug MD11SDR 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.Apr 25, 2006 · N809MC · Boeing 747228FSDR 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.Apr 25, 2006 · N809MC · Boeing 747228FSDR CA060422002Hinge Fitting · gouged(CAN) RT HORIZONTAL STAB NR 1 ELEVATOR HINGE FITTING LOWER PORTION HAS A GOUGE REPAIRED IAW CUSTOMER EA. (TC NR 20060422002)Apr 21, 2006 · Boeing 737290CSDR USAA060578Stiffener · crackedSTA 92.7 24 INCHES AFT OF REAR SPAR CRACKED. FABRICATED AND INSTALLED PART IAW SRM 51-10-02, DEFECT SIZE: .500 INCH.Apr 10, 2006 · N778AU · Boeing 7374B7SDR USAA060557Hinge · damagedSTAB FASTENER HOLE AT NR 6 BEARING HINGE ELONGATED. OVERSIZED HOLES AND TREATED AREA IAW TR 55-50-01A, DEFECT SIZE: .031 INCH.Apr 3, 2006 · N777AU · Boeing 7374B7SDR USAA060554Hinge · damagedSTAB FASTENER HOLE AT NR 6 BEARING HINGE ELONGATED. OVERSIZED HOLES AND TREATED AREA IAW TR 55-50-01A, DEFECT SIZE: .0312 INCH.Apr 3, 2006 · N777AU · Boeing 7374B7SDR 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.Apr 1, 2006 · N353PH · Dhav DHC8202SDR 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.Mar 31, 2006 · N742AS · Boeing 737290CSDR 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 PROTMar 26, 2006 · N284UP · Doug MD11FSDR 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)Mar 22, 2006 · N49053 · Cessna 152SDR 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 810Mar 8, 2006 · N326UA · Boeing 737322SDR 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.Mar 6, 2006 · N585FE · Doug MD11SDR 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, TJan 29, 2006 · N804DH · Doug DC873FSDR 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 TJan 29, 2006 · N804DH · Doug DC873FSDR 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 OUTJan 25, 2006 · N283UP · Doug MD11FSDR 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, Jan 25, 2006 · N283UP · Doug MD11FSDR 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 FOUNJan 25, 2006 · N283UP · Doug MD11FSDR 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. BORJan 25, 2006 · N283UP · Doug MD11FSDR 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 SJan 25, 2006 · N283UP · Doug MD11FSDR 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 BLENJan 25, 2006 · N283UP · Doug MD11FSDR 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 BLENDJan 25, 2006 · N283UP · Doug MD11FSDR 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 FOUJan 25, 2006 · N283UP · Doug MD11FSDR 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 FOUNJan 25, 2006 · N283UP · Doug MD11FSDR 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 SMOOTHJan 25, 2006 · N283UP · Doug MD11FSDR 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 BLJan 25, 2006 · N283UP · Doug MD11FSDR 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 CJan 23, 2006 · N283UP · Doug MD11FSDR 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 FOUNJan 23, 2006 · N283UP · Doug MD11FSDR 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 Jan 23, 2006 · N442FE · Airbus A310SDR 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-Jan 23, 2006 · N442FE · Airbus A310SDR 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.Jan 20, 2006 · N606QX · Cndair CL6002C10SDR USAA200601001Rib · crackedA 3 INCH CRACK ON RIB 7 RT HORIZ STAB TIE. INSTALLED DOUBLER PER EA M00729.Jan 16, 2006 · N808MD · Emb ERJ170100LRSDR 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 BUJan 5, 2006 · N282UP · Doug MD11FSDR 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 PEJan 5, 2006 · N282UP · Doug MD11FSDR 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.Jan 5, 2006 · N15948 · Emb EMB145EPSDR 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 BUJan 3, 2006 · N282UP · Doug MD11FSDR 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.Jan 3, 2006 · N379PH · Dhav DHC8202SDR 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.Jan 3, 2006 · N379PH · Dhav DHC8202SDR USAA051646Clevis · corrodedFOUND CLEVIS R1 ON HORIZ STAB CORRODED. REMOVED CORROSION, REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".Dec 29, 2005 · N781AU · Boeing 7374B7
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