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 K11A2008120272205Angle · crackedANGLE HAS 2 INCH CRACK FWD OF JACKSCREW, STAB STA 32, RBL 14.Apr 30, 2007 · N722CK · Boeing 7272H3SDR K11A2008120272204Web · crackedVERTICAL WEB HAS 4 INCH CRACK FWD OF JACKSCREW, STAB STA 32, RBL 14.Apr 30, 2007 · N722CK · Boeing 7272H3SDR 07FDEA01671Angle · crackedRT HORIZONTAL L/E CENTER I/B SECTION UPPER I/B ATTACHED FLANGE CRACKED MARKED. REMOVED CRACKED RT HORIZ L/E T-CAP SECTION AT UPPER I/B STA XFS 166 IAW DC/MD 10 SRM 55-00-01 FIG, 6 VOL 1, AND INSTALLED ANGLE REPAIR PER MD/DC10 SRM 55-00-01 FIG, 6 VOL 1.Apr 30, 2007 · N68050 · Doug MD1010FSDR USAA070287Tie · wornLEFT HORIZONTAL STA 0 AT REAR SPAR HAS WEAR. REMOVED AND REPLACED BOW TIE PER SRM 51-01-02, DEFECT SIZE: 1 INCH.Apr 18, 2007 · N421US · Boeing 737401SDR USAA070295Tie · wornRIGHT HORIZONTAL STA 0 AT REAR SPAR HAS WEAR. REMOVED AND REPLACED BOW TIE PER SRM 51-01-02, DEFECT SIZE: 1 INCH.Apr 18, 2007 · N421US · Boeing 737401SDR K11A2008120272201Rub Strip · corrodedRUB PADS HAVE CORROSION AROUND ADJUSTMENT SCREWS, LT HORIZONTAL STABILIZER STAB T/E 2ND AND 3RD FROM O/B ELEVATOR.Apr 12, 2007 · N722CK · Boeing 7272H3SDR DHL2007806550Stiffener · crackedLT HORIZ STAB STIFFENER CRACKED 1" STA XFS 47.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21.Apr 10, 2007 · N806DH · Doug DC873FSDR DJFA2007047Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER, THE RT BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. [SUP 05-04Apr 10, 2007 · N452LX · Beech 400ASDR DJFA2007046Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER, THE RT BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. [SUP 05-04Apr 9, 2007 · N697TA · Beech 400ASDR C2XA07TY019Bushing · migratedTYS - DURING A CURRENT 5C INSPECTION THE LT HORIZONTAL STAB HINGE FITTING WAS FOUND MIGRATED. MAINTENANCE REMOVED THE LT STAB BUSHING, REWORKED HOUSING TO THE 2ND OVERSIZE DIAMETER AND INSTALLED THE 2ND SIZE BUSHING IAW EMB 135/145 SRM 55-10-02. ALL WORK WASApr 9, 2007 · N16951 · Emb EMB145LRSDR CALA0700163Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE WEB L-ANGLE AT STAB STA 83.5. A REPAIR WAS INSTALLED IAW ECRA 5510-01883.Apr 3, 2007 · N14604 · Boeing 737524SDR DJFA2007029Hinge Bracket · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, THE LT IB HORIZONTAL STABILIZER ELEVATOR HINGE BRACKET WAS FOUND CRACKED. MAINTENANCE WILL REPLACE THE BRACKET IAW MFG ENGINEERING. (SUPPLEMENTAL 28 MARCH 07) THE CRACK WAS .2" ON THE INBD HORIZONTAL HINGE HALF. TMar 15, 2007 · N701LX · Cessna 750SDR CA070222003Bracket · cracked(CAN) HORIZONTAL STABILIZERS REMOVED FOR REPAIR. AFT ATTACHMENT POINT REINFORCEMENT BRACKETS PN 0732101-4 REPLACED WITH NEW. ADJACENT RIVETS REPLACED. TAIL RE-ASSEMBLED. DUAL INSPECTED. (TC NR 20070222003)Feb 22, 2007 · Cessna A185ESDR SIMA200701513Spar Cap · bentLEFT HORIZONTAL STABILIZER REAR LOWER SPAR CAP BENT. PERFORMED CUT OUT OF DAMAGE, FABRICATED REPAIR DOUBLERS. INSTALLED REPAIR DOUBLERS AND RESTORED PROTECTIVE FINISH IAW SAAB SDS 011469, DATED 8 JANUARY 2007. RETURNED AIRCRAFT TO SERVICE.Jan 13, 2007 · N904AE · Saab 340BSDR UPS07848926Angle · crackedINSPECTION TYPE:C2 LEFT HORIZ STAB LEADING EDGE VERY INBOARD UPPER T-ANGLE CRACKED. CUT OUT DAMAGED AREA ON INBOARD UPPER T-ANGLE ON LT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, RECEIVED, LOCATED, DRILLED UP AND INSTALLED T-ANGLE FITTING ON THE LEFT HORIZ STABJan 3, 2007 · N744UP · Doug DC871FSDR 2007FA0000160Bracket · crackedDURING INSPECTION OF HORIZONTAL STABILIZER ROLLER BRACKETS AND STRUCTURE IAW COMMUNIQUÉ NR 70, FOUND LT HORIZONTAL STABILIZER FWD ROLLER BRACKET, PN 45A21085-003, AND LT AFT ROLLER BRACKET, PN 45A21086-003, BOTH CRACKED. MFG AC TECH SUPPORT BELIEVES IMPROPER Dec 16, 2006 · N93XP · Beech 400ASDR UPS06848256Angle · crackedINSPECTION TYPE:C2 RT HORIZ STAB 2 CRACKS INBD END ON T-ANGLE, FWD OF FRONT SPAR, 9PNL 64J. REMOVED AND REPLACED T-ANGLE IAW SRM 51-01-21, 51-03-00 AND 51-1-20D.Oct 10, 2006 · N755UP · Doug DC871FSDR COMA0670199Fitting · chafedRT HORIZONTAL STAB PIVOT PIN ANTI-ROTATION FITTING IS DAMAGED/CHAFED. REPAIRED IAW REO 670-55-11-053.Oct 10, 2006 · N655CA · Cndair CL6002C10SDR 06FDEA03407Plate · crackedRT HORIZONTAL STAB COMPARTMENT BETWEEN FS 87 AND 86 WEB AT STR 36R IS DENTED AND CRACKED. REMOVED AND REPLACED PLATE AND L-SECTION AT RT HORIZONTAL STAB COMPARTMENT BETWEEN FS 87 AND 86 AT STR 36R IAW A300-600 SRM 51-72-10.Sep 23, 2006 · N722FD · Airbus A300B4622RSDR 06FDEA2876Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 28 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2875Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 12 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2874Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 22 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2873Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 20 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2872Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 16 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2871Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 36 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2870Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 25 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2869Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 33 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2868Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 31 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2867Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 29 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2866Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 27 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2865Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 15 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2864Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 1 RT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2863Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 21 LT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2862Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 25 LT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2861Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 17 LT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2860Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 1 LT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2859Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 20 LT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2858Structure · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 18 LT OF HORIZONTAL STABILIZER.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02809Fitting · damagedHORIZONTAL STABILIZER NR 26R BARREL NUT BORE FOUND EXCEEDED LIMIT AS PER EO 1-5510-7-5000 D1 PT1. HORIZ STAB RT NR 26 BARREL NUT, SPLICE FITTING REMOVED AND REPLACED PER SRM 51-32-01 VOL II, SRM 51-38-01 VOL II AND SRM 51-33-01 VOL.II (REFERENCE TO S.B.MD11-5Aug 3, 2006 · N521FE · Doug MD11SDR USAA060967Bushing · corrodedRT STAB UPPER ATTACH, FED FLANGE AT BUSHING. INSTALLED NEW BUSHING IAW SRM 55-10-10, DEFECT SIZE: .25 INCH.Jul 26, 2006 · N533AU · Boeing 7373B7SDR 2006UALA01446Bracket · crackedAFT TAIL COMPARTMENT HORIZ STAB CENTER SECTION THRUST BEAM BRACKET CRACKED UPPER SIDE LT AND RT SIDE. REMOVED AND REPLACED CRACKED BRACKETS.Jul 21, 2006 · N350UA · Boeing 737322SDR 06FDEA2637Structure · corrodedHORIZONTAL STABILIZER - INSPECT/REPAIR HORIZONTAL STABILIZER BARREL NUT HOLES. WORK ACCOMPLISHED AS PER EA 1-5510-94622 AIR WORTHINESS DIRECTIVE AD 2003-22-08- STABILIZERS - HORIZONTAL STABILIZER - EMBODIMENT OF HORIZONTAL STABILIZER S/B MD11-55-023 BARREL NUJul 20, 2006 · N526FE · Doug MD11SDR KCSA061227Support · corrodedRT HORIZ STAB UPPER I/B POWER PACK ELEVATOR HINGE SUPPORT HAS CORROSION.Jul 19, 2006 · N706CK · Boeing 747249FSDR IXXA06SMN211SStructure · dentedDURING ROUTINE C CHECK INSPECTION, RT HORIZONTAL STABILIZER WITH 02 DENTS , XFS 103.760 - XFS 141.750.Jun 30, 2006 · N41CX · Doug DC862FSDR DJFA2006266Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE A / B LEVEL INSPECTION, THE RIGHT INBOARD HORIZONTAL STABILIZER ROLLER RIB STRUCTURE AND AN INTERNAL BRACKET WERE FOUND CRACKED. DETAILED INJun 17, 2006 · N746TA · Beech 400ASDR 06FDEA2314Structure · misdrilledMIS-DRILLED HOLE IN PANEL SUPPORT AT FWD, CENTER, LT SIDE OF HORIZONTAL STAB JACKSCREW COMPARTMENT. REPAIRED PANEL SUPPORT PER SRM 51-40-4 FIG 1Jun 15, 2006 · N493FE · Boeing 727227SDR ASAA0690689Structure · damagedREPLACE TEMP REPAIR ON HORIZONTAL STAB, REPAIRED IAW EA 5510 01242.Jun 13, 2006 · N302AS · Boeing 737990SDR CA060615002Guide · bentGUIDE PLATE SEPARATED FROM HORIZONTAL STAB FILLET, WAS FOUND LYING BETWEEN VERTICAL STABILIZER AND HORIZONTAL STABILIZER. UNIT HAD BEEN CRUSHED BETWEEN HORIZONTAL STAB AND VERTICAL STAB AS STAB WAS TRIMMED POTENTIAL THAT GUIDE PLATE COULD HAVE MOVED AFT AND JJun 4, 2006 · Amd FALCON50MYSTSDR CALA0600176Fitting · crackedINSPECTION FOUND A 5 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION -X- BRACE RT FORWARD LOWER CORNER FITTING. THE FITTING WAS REPLACED IAW SRM 51-40-02.May 21, 2006 · N12349 · Boeing 7373T0SDR ASMF200605004Structure · damagedDURING OVERNIGHT CHECK A FOD IN LT HORIZONTAL STABILIZER WAS DETECTED. DAMAGE WAS CHECKED AND PROVISIONAL REPAIR WAS PERFORMED IAW SRM 55-10-01. FINAL REPAIR WAS PERFORMED IAW SRM 55-10-01, ALL CORRECT.May 13, 2006 · N850AM · Boeing 737*
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