JASC 5514

Service difficulty reports · 2,805

Reports filed under 5514 · Horizontal Stabilizer Miscellaneous 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 = '5514'
  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 QXEA200602226Structure · damagedPDX: LT HORIZONTAL STAB UPPER AND LOWER L/E REBATES HAVE CUTS FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00 TASK 51-14-00-350-801, SRM TASK 51-25-10-370-801 AND SRM 51-23-00 TASK 51-23-00-390-802.May 11, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602227Panel · damagedPDX: RT HORIZONTAL STAB UPPER AND LOWER L/E REBATES HAVE CUTS FROM BOX CUTTERS. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00 TASK 51-14-00-350-802, SRM TASK 51-25-10-370-801 AND SRM 51-23-00 TASK 51-23-00-390-802.May 10, 2006 · N424QX · Bombdr DHC8402SDR OMKR200600003Rib · crackedCRACKED ROLLER RIB SUPPORT.May 10, 2006 · N686TA · Beech 400ASDR USAA060650Stiffener · crackedFOUND CRACK BOTTOM END OF STIFFENER NR 2 AFT OF FRONT SPAR ST 101, RT HORIZ STAB. NEW PART PER BAC DRAWING 65-47504, DEFECT SIZE: .50".May 3, 2006 · N529AU · Boeing 7373B7SDR UIEA200600084Web · crackedCRACKED WEB AND UPPER CHORD AT THE LT HORIZONTAL STABILIZER STA BL421.50. TRIMMED OUT WEB AND UPPER CHORD CRACKS. HFEC INSPECTED AREA, NO ADDITIONAL FINDINGS. FABRICATED REPAIR DOUBLERS, SUPPORT ANGLES AND STRAPS. WET INSTALLED ALL PARTS IAW BOEING MESSAGEApr 25, 2006 · N809MC · Boeing 747228FSDR USAA060577Stiffener · crackedSTA 92 - 7-12 INCHES AFT OF REAR SPAR CRACKED. FABRICATED STIFFENER AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: .250 INCH.Apr 10, 2006 · N778AU · Boeing 7374B7SDR SIMA200610401Tip Cap · flutterDFW - FLT 3538 - ELEVATOR TAIL FLUTTER AT 300KTS AND ABOVE, BETWEEN 10,000 AND 20,000. ALSO IN DESCENT SLOWING THROUGH 250 KTS. REPLACED UPPER AND LOWER RUDDER 1 ATTACHMENT HINGES, RIGHT HORIZONTAL STABILIZER TIP. COMPLETED ALL PARTS OF EO EM-55AD-207R4. ADApr 3, 2006 · N616AE · Emb EMB145LRSDR CA060328002Channel · cracked(CAN) DURING COMPLETION OF A 6C INSP, MAINT FOUND A CRACK IN THE FWD LT HORIZONTAL STABILIZER MACHINED CHANNEL. THIS PARTICULAR INSP WAS COMPLETED DUE TO AD 83-03-03R6 REQUESTING AN INITIAL INSP AND MODIFICATION OF ATTACHMENT AREA. INITIAL REQUIREMENTS WERE PRMar 26, 2006 · Emb EMB110P1SDR UPS06M46949Structure · corrodedHORIZ STAB POSITION NR R15 BARREL NUT BORE SIDEWALL AND BOTTOM FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE PER SRM 51-21-01 VOL 2 REV 38. BORE BOTTOM BLEND OUT 0.065"DEEP, REAMED TO 1.067 OD, REMAINING BLEND OUT 0.015"DEE FOUND EXCEED. MAGNIFY 10X DMar 14, 2006 · N284UP · Doug MD11FSDR CA060313002Bushing · mismanufactured(CAN) THE RAISED BUSHING AREA OF THE ADAPTOR ARE NOT MACHINED AT THE CORRECT ANGLE. BOTH MACHINED SURFACES ARE ANGLED AFT, THIS CAUSES THE HORIZONTAL AND VERTICAL STABILZERS TO SIT OFF SET ON AN ANGLE AND NOT DOWN FLUSH. MARKING ON THE ADAPTOR ALONG WITH THE Mar 8, 2006 · Dhav DHC6SDR UPS06M46950Structure · corrodedINSPECTION TYPE:C HORIZ STAB POSITION NR R17 BARREL NUT BORE SIDEWALL AND BOTTOM FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VOL 2 REV 38. BORE REAMED TO 1.067"OD REMAINING BLEND OUT 0.025" DEEP EXCEED LIMIT. MAGNIFY 10X DVI C/OUT Mar 5, 2006 · N284UP · Doug MD11FSDR SIMA200606001Bushing · migratedDURING HMBV INSPECTION FOUND HORIZONTAL STABILIZER NR 1 BUSHING TO BE MIGRATING. INSTALLED NEW BUSHING IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)Feb 21, 2006 · N618AE · Emb EMB145LRSDR USAA060326Stiffener · crackedFOUND CRACK IN VERTICAL STIFFENER STA 92.7 APPROX 24" AFT OF REAR SPAR. FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: .500".Feb 21, 2006 · N778AU · Boeing 7374B7SDR USAA060320Stiffener · crackedFOUND CRACK STA 92.7 APPROX 12" AFT OF REAR SPAR. FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: .250".Feb 21, 2006 · N778AU · Boeing 7374B7SDR 2006UALA00054Skin · dentedDENT IN RIGHT HORIZONTAL STAB LEADING APPROX TWO TO THREE FEET INBOARD OF TIP. REMOVED DAMAGE & VERIFIED CONTAINMENT USING NDT. FABRICATED & INSTALLED FLUSH REPAIR REF SRM 55-10-01.Jan 10, 2006 · N337UA · Boeing 737322SDR UPS06M46166Structure · corrodedINSPECTION TYPE:C EMPENNAGE-BARREL NUT HOLE NR 34 LT FOUND BEARING WITH SURFACE CORROSION ON THE SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT AFFECTED AREA PER SRM51-21-01.V2.R38, FOUND BLEND OUT EXCEEDED LIMIT PER MD11-5510-19409-K, REPAIR SLEEVE BUSHING FAJan 3, 2006 · N282UP · Doug MD11FSDR UPS06M46161Structure · corrodedEMPENNAGE-BARREL NUT HOLE NR 31 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE AND BOTTOM AREA. CORROSION REMOVAL C/OUT ON B/N HOLE NR 31 LT FOUND EXCEEDED LIMIT PER SRM 51-21-01V2R.38. REPAIR BUSHING FAB PER MD11-5510-19409-K FIG 5. PR 1422 B 1/2 SEALANT AJan 1, 2006 · N282UP · Doug MD11FSDR UPS06M46269Structure · corrodedINSPECTION TYPE:C EMPENNAGE - BARREL NUT HOLE NR 08 LT FOUND BEARING WITH SURFACE CORROSION ON SIDE & BOTTOM AREA. CORROSION REMOVAL CUTOUT & FOUND BLENDED OUT BEYOND ALLOWABLE LIMIT. B/N BORE & BOTTOM REWORKED PER EN 1643-05. FAB SLEEVE BUSHING PER EO MD 1Dec 21, 2005 · N282UP · Doug MD11FSDR AU510001646Hinge Pin · cracked(AUS) LT HORIZONTAL STABILIZER OUTER HINGE PIN CRACKED IN AREA OF THREAD ROOT ADJACENT TO SPLIT PIN HOLES. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW SB727-55A0090R1 PART 4 AND AD/B727/173.(AD/SB DESC: AD/B727/173, SB727-55A0090R1 ) (CASA# 510001646)Dec 12, 2005 · Boeing 727277SDR 05FDEA04153Hinge Fitting · wornRT HORIZONTAL STABILIZER IB NR1 ELEVATOR HINGE FITTING ON HORIZONTAL STABILIZER HAS IB FACE OF FITTING WORN. REMOVED BUSHING, SPOTTED FACE, HFEC INSPECTED LUG BORE FABRICATED AND INSTALLED REPAIR WASHER AND NEW BUSHING ALL IAW EA NR 7-5510-91317. THIDec 6, 2005 · N486FE · Boeing 727227SDR IXXA05RNG100SPanel · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER TRAILING EDGE LOWER AND UPPER PANEL. REPAIR ACCOMPLISHED, REMOVED PANEL AND STIFFENER, FABRICATED AND INSTALLED NEW PANEL AND STIFFENER IN ACCORDANCE WITH DRAWINGS 55-05467-1, 55-05467-2, 55-05Oct 14, 2005 · N721CX · Doug DC872SDR 2005FA0001491Bearing · corrodedTAILPLANE ACTUATOR EXCEEDED SCREW CASING END PLAY LIMIT OF 0.25 MM AS LISTED IN MM. DISASSEMBLED UNIT AND FOUND PRESENCE OF WATER CONTAMINATION AND INTERNAL BALL BEARINGS RUSTED. DATE DISCOVERED 17 AUG 2005. UNIT SHOULD BE CHECKED INTERNALLY FOR CONDITION OSep 1, 2005SDR SWIA200515523Bushing · damagedDURING CLIMB-OUT AT 280KTS AT 25,500 FT, EXPERIENCED AC FLUTTER. REMOVED AND REPLACED HORIZ STABILIZER BUSHINGS IAW SB 601R-55-007.Aug 31, 2005 · N591SW · Cndair CL6002B19SDR AU510001918Bracket · crackedHORIZONTAL STABILIZER UPPER PLATE CRACKED IN AREA ADJACENT TO VERTICAL STABILIZER BRACKET ATTACHMENT. CRACK LENGTH 5MM (0.196IN).Aug 9, 2005 · Cessna A152SDR 2005UALA00598Attach Angle · crackedHORIZONTAL STAB CENTER SECTION CENTER LT SIDE 3 EACH BEAM ATTACHED ANGLES CRACKED, NR 1 UPPER FWD, NR 2 LOWER FWD AND NR3 LOWER AFT. REPLACED 3 EACH CRACKED FITTINGS REF SRM 51-40-02.Jun 25, 2005 · N340UA · Boeing 737322SDR 2005FA0000995Angle · corrodedDURING REPLACEMENT OF AFT TAIL COMPT BULKHEAD CAP-ANGLE, HORIZ AND VERT STABILIZERS REQUIRED REMOVAL. AFTER REMOVAL, TECH FOUND RECENT REPAIR ACCOMPLISHED BY 3RD PARTY REPAIR STATION HAD NUMEROUS ISSUES. REPAIR WAS ACCOMPLISHED, DUE TO FINDING CORROSION DURIJun 24, 2005 · N723MM · Gulstm G1159ASDR 05FDEA01674Fitting · corrodedEMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 26R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Jun 24, 2005 · N619FE · Doug MD11SDR 05FDEA01673Fitting · corrodedEMPENNAGE WITH REFERENCE TO EO 1-5510-7-5000-01 PART 1, FOUND NR 14R FITTING BORE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.Jun 24, 2005 · N619FE · Doug MD11SDR 2005FA0000891Bracket · corrodedWHILE PERFORMING REPAIRS TO RT AND LT HORIZONTAL STABILIZERS, IT WAS DISCOVERED THAT THE OUTBOARD AND CENTER HINGE TEE REINFORCEMENT BRACKETS, P/N 52-21007 AND 52-21008, OF BOTH STABILIZERS WERE SEVERLY CORRODED. THESE BRACKETS REINFORCE THE REAR SPAR WHERE TJun 22, 2005 · N7070C · Namer SNJ4SDR 2005FA0000892Bracket · corrodedWHILE PERFORMING REPAIRS TO RT AND LT HORIZONTAL STABILIZERS, IT WAS DISCOVERED THAT THE OUTBOARD AND CENTER HINGE TEE REINFORCEMENT BRACKETS, P/N'S 52-21007 AND 52-21008, OF BOTH STABILIZERS WERE SEVERLY CORRODED. THESE BRACKETS REINFORCE THE REAR SPAR WHEREJun 22, 2005 · N7070C · Namer SNJ4SDR 05FDEA01362Fitting · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 14 HAS BORE CORROSION EXCEEDING LIMITS. SPLICE FITTING REMOVED AND REPLACED IAW EO-1-5510-7-5000 REV D -PT1. MAJOR REPAIR PER GMM 6-2-100.May 18, 2005 · N576FE · Doug MD11SDR USAA050641Beam · damagedCLT - FOUND BEAM STRUCTURE WITH HOLE .25 INCH, HORIZ STAB LOBE T/E BEAM. DAMAGE TRIMMED AND REPAIR DOUBLER, INSTALLED IAW EA 96571 BOEING 737 SRM 55-10-13. (M)May 10, 2005 · N433US · Boeing 7374B7SDR USAA050640Web · debondedCLT - FOUND WEB DISBOND 1 INCH BY 1 INCH, LEFT HORIZ STAB RIB DISBONDED OUTBOARD OF OUTBOARD BALANCE, PANEL STATION 149.12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW SRM 51-40-02. (M)May 10, 2005 · N439US · Boeing 7374B7SDR CA050509006Fitting · cracked(CAN) FITTING CRACKED 90 PERCENT THROUGH, IN RADIUS BETWEEN OUTER HORIZONTAL AND VERTICAL SECTIONS.May 9, 2005 · Cessna 152SDR GTIA050169Stiffener · crackedFOUND LEFT HORIZONTAL STABILIZER REAR SPAR STIFFENER CRACKED ON UPPER EDGE. REMOVED DAMAGED STAB REAR SPAR STIFFENER. FABRICATE STIFFENER SEAL. LOCATED AND DRILLED FABRICATED STIFFENER. TREATED AND PRIMED FABRICATED STIFFENER. TOP COATED FABRICATED STIFFEMay 5, 2005 · N827NK · Doug MD83SDR CA050428002Bracket · crackedWHILE PERFORMING THE INSPECTION REQUIREMENTS OF SEB 03-06, THE BRACKET WAS FOUND TO BE CRACKED. ALL OTHER PARTS OF INTEREST WHILE PERFORMING THIS SB WERE SERVICEABLE.Apr 27, 2005 · Cessna 152SDR 2005F00076Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M)Apr 11, 2005 · N81535 · Beech 1900DSDR 05FDEA00948Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND BORE NR 22L FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82952.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00947Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 16L, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82952.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00946Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 18L, FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82952.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00945Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 10L, FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00944Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND BORE NR 6L FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82991.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00943Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 1L BARREL NUT BORE FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82998.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00942Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER CENTER SKIN PLANK NR 36R BARREL NUT BORE FOUND EXCEEDED LIMIT. REPAIRED IAW FEDEX EA 1-5510-82996.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00940Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFTHAND BORE NR 8L FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82991.Apr 11, 2005 · N617FE · Doug MD11SDR 05FDEA00911Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER AFT SKIN PLANK NR 34L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82941.Apr 8, 2005 · N616FE · Doug MD11SDR 05FDEA00910Structure · corrodedCORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER AFT SKIN PLANK NR 34R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942.Apr 8, 2005 · N616FE · Doug MD11SDR 05FDEA00901Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 25 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00900Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 19 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 8, 2005 · N576FE · Doug MD11SDR 05FDEA00899Structure · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT NR 17 HAS BORE CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-78133.Apr 8, 2005 · N576FE · Doug MD11
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