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 SWAA095173Beam · corrodedDURING SCHEDULED 24Y CHECK, FOUND LT HORIZONTAL STABILIZER UPPER SURFACE T/E BEAM CORRODED. REPAIRED STABILIZER PER SRM.Aug 11, 2009 · N687SW · Boeing 7373Q8SDR FDEA200906252295Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 1 BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO 1-5510-7-5000 PART 1 LIMITATIONS. REPAIR CARRIED OUT AS PER E.A. 1-5510-131620, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Jun 25, 2009 · N572FE · Doug MD11SDR FDEA200906252294Skin · corrodedHORIZONTAL STABILIZER RT UPPER PLANK NR 15R BARREL NUT BORE CORROSION REWORKED, FOUND EXCEEDED EO 1-5510-7-5000, PART 1 LIMITATIONS. REPAIRED AS PER E.A. 1-5510-131622, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV. 107Jun 25, 2009 · N572FE · Doug MD11SDR FDEA200906232244Structure · corrodedBARREL NUT HOLES INSPECT/REPAIR - LT NR 26 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Jun 23, 2009 · N572FE · Doug MD11SDR DLM88091264Structure · corrodedPITTING CORROSION ON HOR STAB BARREL NUT HOLES BETWEEN RT STRINGER 2-3 FWD, 8-9 FWD AND LT STRINGER 5-6 AFT. REPAIR BUSHINGS WERE FABRICATED IAW DRAWING AMR0955112. BUSHINGS WERE INSTALLED IAW ERA 475561-14 REV ORIG.Jun 22, 2009 · N983DL · Doug MD88SDR ASAA0995834Structure · crackedLT HORIZONTAL STAB CRACKED 9 INCHES AFT OF FRONT SPAR STAB STA 111.10. REPAIRED HORIZONTAL STAB.Jun 3, 2009 · N307AS · Boeing 737990SDR TIMA20090001Fitting · crackedFOUND CRACK IN UPPER CENTER TEE EXTRUSION AFT .75 INCH DURING MAINTENANCE. CRACK WAS REPAIRED IN ACCORDANCE WITH HAWKER BEECHCRAFT FIELD REPAIR FR-CO-01905.Apr 15, 2009 · N99CA · Beech 99ASDR UALA2009040801005Structure · crackedFOUND FASTENER HOLE CRACKED COMMON TO RT SIDE OF HORIZONTAL STAB. CENTER SECTION & LOWER SPLICE PLATE. OVERSIZED FASTENER HOLE & REPLACED RT LOWER SPLICE PLATE.Apr 8, 2009 · N178UA · Boeing 747422SDR IPXA09855353Structure · misrepairedINSPECTION TYPE:SV SURVEY SEQ 752-S1-02 LT HORIZ STAB DOUBLER AT XFS 115.00 MINIMUM REPAIR FASTENER DIAMETER, AS MARKED. REPAIR ACCOMPLISHED PER REO-G12621 AND EO DC8-5320-32359.Apr 6, 2009 · N752UP · Doug DC871FSDR IPXA09855331Structure · misrepairedINSPECTION TYPE:SV SURVEY SEQ 752-52-10 DOES NOT CORRELATE TO ANY SRM REPAIR. ACCOMPLISHED REPAIR PER DC8 SRM 55-2-1 FIG 4.Apr 4, 2009 · N752UP · Doug DC871FSDR HEEA123734Support · corrodedTHE SUPPORT HAS EXFOLIATING CORROSION. REMOVED AND REPLACED.Mar 9, 2009 · N612PH · Bell 407SDR HEEA123733Support · corrodedTHE SUPPORT HAS EXFOLIATING CORROSION. REMOVED AND REPLACED WITH SERVICEABLE.Mar 9, 2009 · N612PH · Bell 407SDR HEEA123732Support · corrodedTHE SUPPORT HAS EXFOLIATING CORROSION. REMOVED AND REPLACED WITH SERVICEABLE SUPPORT.Mar 9, 2009 · N612PH · Bell 407SDR 2009FA0000182Structure · crackedDURING THE SID INSP, THE HORIZONTAL STABILIZER WAS REMOVED. VISUALLY DISCOVERED THE SHELF UNDER THE HORIZ STAB WAS CRACKED AT THE AFT END WHERE IT IS RIVETED TO THE AFT HORIZ STAB MOUNT BULKHEAD.Mar 6, 2009 · N505HC · Cessna 441SDR UALA2009031000701Cap · damagedLIGHTNING STRIKE DAMAGE TO LT HORIZ STAB CAP. STAB T/E WEDGE IN SHOP 321.Feb 28, 2009 · N676UA · Boeing 767322SDR ABXA200903130015Fitting · crackedDURING C-CHECK AT ILN, MAINTENANCE FOUND A CRACK INDICATION DURING AFTER MODIFICATION INSPECTION OF THE RIGHT FORWARD OUTER CHORD AND TENSION FITTING PER A/B 767-53A0078, AS MANDATED BY AD 2005-11-02. THREE DISCREPANT FASTENER HOLE LOCATIONS WERE OVERSIZED TOFeb 9, 2009 · N797AX · Boeing 767281SDR CA090130008Attach Bracket · crackedDURING A ROUTINE 200-HR INSPECTION, CRACKS WERE DETECTED ON THE REAR FIN ATTACH BRACKET THAT IS RIVETED TO THE AFT SPAR OF THE HORIZONTAL STAB. ONE HALF INCH CRACK WAS ALONG THE WELD AT THE TOP FORWARD BOXED AREA AND THE OTHER CRACK WAS PROPAGATING FROM ONE OJan 30, 2009 · Cessna 152SDR ASAA0944293Beam · crackedLT HORIZONTAL STABILIZER LOWER TE BEAM CRACKED AT IB FWD. REMOVED DAMAGE.Jan 21, 2009 · N709AS · Boeing 737490SDR IPXA09855279Structure · misrepairedINSPECTION TYPE:SV VERT STAB L/E REPAIR HAS 2 FASTENERS WITH LESS THAN 4D, STA XFS-70.000 SS 752-S4-05. REPAIRED PER DC8 SRM 55-2-1 FIG 4 SHT 1 REV 78.Jan 15, 2009 · N752UP · Doug DC871FSDR AALA2009020900056Plate · corrodedNUMBER SEVEN LUG PLATE BORE RIGHT OUTBOARD IS CORRODED AND OUT OF LIMITS (HORIZONTAL STABILIZER). INSTALLED NEW SERVICEABLE NUMBER SEVEN LUG PLATE PER CARD K2988AA.Jan 12, 2009 · N412AA · Doug DC982SDR USAA2009012190109Fitting · corrodedSAL - C19 - MAJOR REPAIR - CORROSION ON UPPER, LOWER, & MIDDLE CLEVIS JOINT OF LEFT HORIZONTAL STABILIZER AT ELEVATOR HINGE LINE 113.25. REPAIRED UPPER, LOWER, & MIDDLE CLEVIS JOINT OF LEFT HORIZONTAL STABILIZER AT ELEVATOR HINGE LINE 113.25 IAW B737 55-10-10Jan 6, 2009 · N305AW · Boeing 7373G7SDR ASOA200900037Seal · out of positionAERODYNAMIC SEAL ON HORZ STAB LT SIDE ADJACENT TO VERTICAL STAB IS PUSHED IN OR MISSING.Jan 4, 2009 · N876AS · Cndair CL6002B19SDR C2XA08TY133Hinge Bracket · crackedRT HORIZONTAL STAB HINGE PIN RETENTION EAR IS CRACKED. REMOVED AND REPLACED RT HORZ STAB HINGE PIN BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT STILL IN C CHECK.Nov 20, 2008 · N16911 · Emb EMB145SDR 2008UALA06436Structure · damagedRT HORIZONTAL STABILIZER AFT UPPER CHORD, STA 2590, RBL 43.5 A FASTENER HOLE WAS FOUND DAMAGED DURING COA 850111. OVER-SIZED HOLE TO APPROX 0.469 INCHES & INSTALLED BOLT WITH NUT.Nov 9, 2008 · N174UA · Boeing 747422SDR UPS08854242Doubler · damagedINSPECTION TYPE:SP REPAIR SEQ 803-S2-01 RT HORIZONTAL STAB XE 25.312 - XE 29.812, HAS NO SRM REF. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW EA 008-5500-01-A1585, AND EO DC8-5530-31694-A.Oct 24, 2008 · N803UP · Doug DC873FSDR SWIA200820375Stiffener · crackedC-CHECK, INBOARD HORIZONTAL BULKHEAD ANGLE STIFFENERS CRACKED IN RADIUS WL111.5 ON LEFT SIDE OF FS 280 BULKHEAD. REPAIRED PER REO.Jul 25, 2008 · N776SK · Cndair CL6002C10SDR DJFA2008049Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT AFT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE May 31, 2008 · N452LX · Beech 400ASDR S9BA20080020Adapter · cracked(CLOSE) LT AFT HORIZONTAL WEB ADAPTER CRACKED FOUND DURING SB 454 PART A EMERGENCY MEASURES EXECUTED. AIRCRAFT GROUNDED, REMOVED AND REPLACED LT AFT WEB ADAPTOR.May 23, 2008 · N533SW · Dhav DHC6300SDR SWAA082062Fitting · corrodedDURING SCHEDULED BRDG CHECK, FOUND LEFT HORIZONTAL STABILIZER CENTER SECTION FITTING BEARING HOUSING CORRODED. REPAIRED FITTING PER SWA EA.Apr 17, 2008 · N335SW · Boeing 7373H4SDR ZZDA2008092Structure · dentedMDDR 115768T - RT HORIZONTAL STABILIZER HAS DENT AT STA 184. REPAIRED PER B737 SRM 55-10-01 FIG 202.Apr 15, 2008 · N289AT · Boeing 73776NSDR ZZDA2008091Structure · dentedMDDR 115767T - RT HORIZONTAL STABILIZER HAS DENT AT STA 120. REPAIRED PER B737 SRM 55-10-01 P205 FIG 202.Apr 15, 2008 · N289AT · Boeing 73776NSDR 08FDEA01356Web · damagedTHS - DURING INSTALLATION OF RT THS TIP SOME HOLES FOUND MISDRILLED. REPAIR PERFORMED BY INSTALLAING NEW WEB WITH LOCK FASTENERS DAN7-6 IAW RAS/CASA/6544/2008 ISS B, APPROVED BY EA 6-5514-117183.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01355Web · damagedTHS -DURING INSTALLATION OF LT THS TIP SOME HOLES FOUND MISDRILLED. REPAIR PERFORMED BY INSTALLING NEW WEB WITH LOCK FASTENERS DAN7-6 IAW RAS/CASA/6544/2008 IS B, APPROVED BY EA 6-5514-117183.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR SROM2008016Bushing · looseLOOSE BUSHING ON STABILIZER SCREW JACK LOWER RIGHT HAND MOUNTING STRUCTURE (P/N 6-37464-1). REPLACED BUSHING ON STABILIZER SCREW JACK LOWER RT MOUNTING STRUCTURE IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3, 078-1236-08-473 AND ASI SOLUTIONS DRAWING 534047Apr 6, 2008 · N733PA · Boeing 737205SDR DJFA2008035Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN CMar 29, 2008 · N792TA · Beech 400ASDR 08FDEA01176Rub Strip · chafedLEFT HORIZONTAL STABILIZER PANEL NR 335 BB IS CHAFED. REMOVED GOUGES ON THE PANEL IAW DC/MD-10 SRM 55-00-01; VOL I. FOUND TO BE WITHIN LIMITS IAW DC/MD-10-10 SRM 55-00-01; VOL I AND UT GAUGE T8225P; CAL DATE 12-19-08. REMOVED AND REPLACED WORN THROUGH RUB Mar 28, 2008 · N365FE · Doug MD1010FSDR 08FDEA01141Panel · chafedLEFT HORIZONTAL STABILIZER PANEL NR 335 BB IS CHAFED. BLENDED CHAFED AREA. ORIGINAL MATERIAL 0.071; REMOVED 0.015; REMAINING MATERIAL 0.056 IAW DC/MD-10 SRM 54-00-02; VOL I. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 54- 51-02; VOL III. FABRICATED DOUBLERMar 25, 2008 · N365FE · Doug MD1010FSDR CA080328003Bracket · crackedDURING THE ANNUAL INSPECTION REINFORCEMENT BRACKET (P/N 12 32623-1) WAS FOUND TO HAVE A CRACK RUNNING FROM THE BOTTOM BOLT HOLE TO THE EDGE OF THE BRACKET. THE BRACKET IS ATTACHED TO THE REAR SPAR OF THE LT HORIZ STABILIZER. AFFECTED PART REPLACED. (TC NR 20Mar 19, 2008 · Cessna 210JSDR MASA200800195Fitting · gougedREPAIR TO GOUGE DAMAGE TO H-STAB PIVOT FITTING.Mar 6, 2008 · N917FJ · Cndair CL6002D24SDR DLM90080358Lug · corrodedHORZ STAB PIVOT BEARING LUGS (4 EA) AND BARE SLEEVES (2 EA) CORRODED AND PITTED. INSTALLED REPAIRED HORZ STAB LUGS, IAW DELTA ER/A 466670-14 REV. DATE 19FEB08 I/R.Feb 28, 2008 · N911DA · Doug MD9030SDR AMTA200800102Support · damagedELONGATED HOLES AT E-STA 231.70 AND 225.70 FOR SUPPORT PANEL 333FB ONT EH LT HORIZ STABILIZER. REPAIRED IAW EA737-5510-08-A0010 NOTE ELONGATED HOLES WERE SELF INDUCED, FRE ERA 737-55R-6237. (K)Feb 18, 2008 · N317TZ · Boeing 73783NSDR SWAA080542Stiffener · crackedDURING SCHEDULED 16Y CHECK, FOUND LT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED AT STA 120. REMOVED AND REPLACED STIFFENER PER SRM.Jan 30, 2008 · N697SW · Boeing 7373TOSDR 08FDEA00316Bracket · corrodedTHS LEFT LOWER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED LOWER SURFACE, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED LOWER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 SRM 51-40-21. REMOVJan 28, 2008 · N416FE · Airbus A310221SDR 08FDEA00312Bracket · corrodedTHS LEFT UPPER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED UPPER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 51-40-21. REMOVED UPPER ATTACH PLATE Jan 28, 2008 · N416FE · Airbus A310221SDR 2008FA0000056Attach Bolt · undertorquedDURING A ROUTINE PHASE INSPECTION WE FOUND 50 PERCENT OF THE HORIZONTAL STABILIZER AFT ATTACH BOLTS TO BE UNDERTORQUED, AND CAUSING SOME MOVEMENT AND A POPPING NOISE WHEN THE STABILIZER WAS PUSHED UP AND DOWN AT THE OB TIP. WE RE-TORQUED ALL BOLTS AND THE NOIJan 23, 2008 · N570EJ · Cessna 560CESSNASDR 2008UALA00353Fitting · corrodedRIGHT HORIZ STAB CENTER SECTION, AFT FACE OF THE AFT LUG IS CORRODED ON THE AFT SPAR UPPER ATTACH CLEVIS. MAJOR REPAIR: REMOVED CORROSION. INSTALLED OVERSIZED BUSHING.Jan 21, 2008 · N385UA · Boeing 737322SDR 2008UALA00352Fitting · corrodedRIGHT HORIZ STAB CENTER SECTION FWD LUG FWD FACE CORRODED ON AFT SPAR UPPER ATTACH CLEVIS. MAJOR REPAIR: REMOVED CORROSION.Jan 21, 2008 · N385UA · Boeing 737322SDR CALA0800048Fitting · corrodedRIGHT HORIZONTAL STAB AFT SPAR LOWER LUG HAS CORROSION IN BORE. REMOVED CORROSION IN BORE PER SRM 55-10-10 IAW ECRA 5510-01912.Jan 19, 2008 · N19623 · Boeing 737524SDR CALA0800047Fitting · corrodedLEFT HORIZONTAL STAB ATTACH LUGS INSPECTED FOR CORROSION. INSTALLED NEW SLEEVE PER SOPM 20-50-03. REF BUSHING AND SLEEVE INSTALLATION.Jan 19, 2008 · N19623 · Boeing 737524SDR CALA0800046Fitting · corrodedLEFT HORIZONTAL STAB FORWARD UPPER LUG HAS CORROSION AT BUSHING'S (FORWARD AND AFT). REMOVED BUSHINGS AND SLEEVE, CLEANED CORROSION AND INSTALLED NEW SLEEVE AND BUSHINGS PER SRM 55-10-10 REF ECRA 5510-01911.Jan 19, 2008 · N19623 · Boeing 737524
Back to JASC 5514