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.
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
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 PCSA2011082528Beam · corrodedLEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER BEAM ELEVATOR STATION 17.20-39.50 CORRODED. REPAIRED WITH DOUBLER.SDR DALA1131530917Structure · corrodedCORROSION ON RT HORIZ STAB FWD UPPER PLATE BARREL NUT HOLE. REPAIRED PER ERA 491695-14 REV ORG AND AMR 0955165.SDR DALA1126249012Plate · damagedDURING HMV WEAR AND CORROSION WAS FOUND ON OUTBD AND INBD LUG PLATES AT (HORIZONTAL STABILIZER PIVOT POINT) VERTICAL STABILIZER STA ZRS=173 LT. LUG PLATES WAS REPAIRED IAW SRM 55-02D PARA 24, A (1).SDR NACA 20110026Fitting · gougedWEAR MARK ON FITTING ON LEFT HORIZONTAL STABILIZER UPPER AFT FITTING. WEAR MARK ON FITTING ON LEFT HORIZONTAL STABILIZER UPPER AFT FITTING REPAIRED IAW FAA FORM 8100-9. REF: ID 201102210081-0003D1, SUBJECT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPERSDR USAA2011031791085Strap · brokenSAL - S5 - MAJOR REPAIR - BROKEN STRAP ASSEMBLY AT TRAILING EDGE OF LEFT HORIZONTAL STABILIZER NR 4 LEVEL HINGE ARM AT STAB STA 342, RIB 9. REPLACED STRAP ASSEMBLY IAW A320 SRM 51-72-11.SDR ASAA1148829Stiffener · crackedRT HORIZONTAL STABILIZER STIFFENER FOUND CRACKED AT THE BOTTOM FASTENER HOLE STAB STA 92.7. REMOVED CRACKED STIFFENER FABRICATED REPLACEMENT AND INSTALLED IAW SRM 51-40-02SDR VGQY2011011500008Retainer · corrodedLEFT LOWER VERTICAL STABILIZER, BELOW AIR INTAKE DUCT FOUND WITH CORROSION AFT OF PANEL 361BL. REMOVED AND DISCARDED CORRODED AJC7331-29 RETAINER. FABRICATED NEW RETAINER PER DWG AJC7331 REQUIREMENTS USING MATERIAL 7075-0-0.125". NEW RETAINER INSTALLED AS PSDR VGQY2011011500005Balance Weight · crackedLT HORZ STAB O/B ELEVATOR BALANCE WEIGHT AFT EDGE FOUND WITH ONE (1) INCH CRACKED. TRIMMED OUT DAMAGED AREA ON LT HORIZONTAL STABILIZER FAIRING AS PER DC-10 SRM 55-00-01 FIGURE 3 VOLUME I REVISION 97. FABRICATED REPAIR DOUBLER AND FILLER AS PER SRM 55-00-01SDR FDEA201101140174Web · buckledWEB BUCKLED AT LIGHTNING HOLE - RT HORIZ STABILIZER INTERIOR BOX RIB, APPROX STAB L/E 100.63. CUT OUT DAMAGED AREA OF WEB DIM 1/4" X 1" IAW SRM 55-10-4 FIG 2 REV 103. FABRICATED WEB LIGHTNING HOLE DOUBLER FROM 2024 T3 .032" DIM 9.75" X 13.25" IAW SRM SDR NSVA2011004Structure · damagedPERFORMED PERMANENT REPAIR OF DAMAGES ON LT HORIZONTAL STAB IAW TD 340-55-11-01.SDR DJFA2011001Bracket · crackedDURING A SCHEDULED MX VISIT, WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT BRACKET WAS FOUND CRACKED. THE BRACKET WAS REPLACED.SDR V0XR201012270020Seal · worn(V0XR) LT HORIZONTAL INBD L/E SEAL PANEL 333DL IS WORN BEYOND LIMITS. R & R SEAL. W/C 3063SDR USAA2010121793149Bolt · corrodedMCN - MAJOR REPAIR - C20 CHECK - LEVEL 2 CORROSION ON THE RIGHT HORIZONTAL STABILIZER FWD LOWER BOLT. REPLACED THE RIGHT HORIZONTAL STABILIZER FWD LOWER BOLT IAW TASK CARD I6C55038.SDR SWAA107065Stiffener · crackedDURING SCHEDULED 16Y CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION STIFFENER CRACKED AT BS 1121. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.SDR LR7A2010103100142Fitting · corrodedDURING SCHEDULED C-10 CHECK IN RELATION TO NR 0026 FOUND HORIZONTAL STABILIZER BEAM FITTINGS WITH EXFOLIATION CORROSION AT FS 1041. REPLACED FITTINGS IAW LOCKHEED SMP583 CHAPTER 51-70.SDR USAA2010090791938Fitting · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON L3 CLEVIS FORWARD FACE CENTER SECTION LEFT HORIZONTAL STABILIZER. REPAIRED L3 CLEVIS FORWARD FACE CENTER SECTION LEFT HORIZONTAL STABILIZER IAW EA 133021.SDR USAA2010090791936Fitting · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION AT UPPER CLEVIS L7 FORWARD FACE OF LEFT HORIZONTAL STABILIZER AFT ATTACH POINT. REPAIRED UPPER CLEVIS L7 FORWARD FACE OF LEFT HORIZONTAL STABILIZER AFT ATTACH POINT IAW EA 133043.SDR USAA2010090791934Fitting · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON FORWARD ATTACHMENT FITTING FORWARD LOWER CLEVIS L4 FORWARD FACE OF LEFT HORIZONTAL STABILIZER AT BS 1093.417, LBL 40. REPAIRED FORWARD ATTACHMENT FITTING FORWARD LOWER CLEVIS L4 FORWARD FACE OF LEFT HORIZONTAL STABILIZERSDR USAA2010091691999Bolt · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON 8 BOLTS ON LEFT STABILIZER NR 2 BALANCE PANEL AT STAB STA 120.3 TO STAB STA 129.5. REPLACED 8 BOLTS ON LEFT STABILIZER NR 2 BALANCE PANEL AT STAB STA 120.3 TO STAB STA 129.5 IAW B737 SRM 51-10-02.SDR CALA2010090200409Clevis · corrodedSUPPORT TASK RT HORZ STAB AFT LOWER CLEVIS HAS CORROSION REMOVED LIGHT CORROSION AND TREATED AS REQUIRED PER SOPM 20-10-03 AND SRM 55-10-10.SDR VNAA2010083000011Structure · dentedCREW REPORTED A DENT IN THE RIGHT HORIZONTAL STABILIZER. MAINTENANCE USING MANUFACTURER MANUALS INSPECTED, REMOVED, AND REPLACED THE RIGHT HORIZONTAL STABILIZER. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.SDR AALA20100827TUL01Angle · crackedTAIL - UPPER EDGE OF ANGLE CRACKED INSIDE RIGHT HORIZONTAL STAB AT SIDE ROLLER AREA. REMOVED AND REPLACED DAMAGED RIGHT HORIZONTAL STAB ANGLE WITH NEW ONE IAW 55-10-00-4. ALSO CHANGED ROLLER BRACKET IAW AARD 55-10-00-5.SDR CA100716005Cap · corrodedTHE LIGHTNING PROTECTION END CAPS (P/N DSC740067-1 AND -2) ON THE LEFT AND RIGHT WERE FOUND DISBONDED FROM THE HORIZONTAL STABILIZER. THE ADHESIVE BETWEEN THE LIGHTNING PROTECTION STRAPS AND HORIZONTAL STABILIZER HAD BECOME BRITTLE OVER TIME AND THE EDGES HAD SDR VGQY2010062300039Web · crackedLEFT HORZ STAB AT STAB BL 421.50, RIB WEB AFT END FOUND CRACK AT FASTENER HOLE (CRACK LENGTH APPROX = 0.575 INCH). NO SRM REPAIR. REMOVED CRACKED WEB PER SRM 51-30-02, REV 116. WEB TRIMMED OFF, WEB AND SPLICE FABRICATED 7075-T6 AL CLAD SHEET AND INSTALLED. SDR USAA2010062591284Support Angle · crackedSAL - S4 - MAJOR REPAIR - CRACK ON LEFT HORIZONTAL STABILIZER SUPPORT ANGLE AT RIB NR 6. REPLACED LEFT HORIZONTAL STABILIZER SUPPORT ANGLE AT RIB NR 6 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D55182732.SDR FDEA201006101940Strap · corrodedLT HORZ STAB LOWER AFT PIVOT FITTING STRAP HAS CORROSION. REMOVED CORROSION FROM FITTING IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 55-10-01 FIG 101 DET II. ACCOMPLISHED EA F-5510-141151, SPLICE PLATE PN 182N1608-5. MAJOR REPAIR.SDR SWAA102913Structure · crackedDURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL L/E T-CHORD UPPER AFT FASTENER HOLE CRACKED. REPAIRED STABILIZER PER ER.SDR A6WA201040318Fitting · corrodedANTI-ROTATION FITTING- 600-21073-7 HORIZ STABILIZER PIVOT PIN CORROSION WITH PITTING IN PIN NOTCHES. REPLACED ANTI AND ROTATION FITTING.SDR FDEA201004141183Strip · crackedHORIZONTAL L/E PANEL 331 DB JOINT STRIP IS CRACKED AT RIB 33A. REMOVED JOINT STRIP IAW SRM 51-40-21, PARA 5. MATERIAL ID 2024-T3, 0.071, PO NR 618569.1. FOR THE DOUBLER AND 2024-T3 0.063, PO NR 652264.1 FOR THE FILLER IAW SRM 55-12-28. FABBED REPAIR IAW SRM SDR VGQY2010041300001Stiffener · corrodedRIGHT HORIZONTAL STABILIZER REAR SPAR AT ELEVATOR STATION 206.8 STIFFENER LOWER END FOUND CORRODED. COMPLIED WITH EN 1048-10, ALTERNATIVE FABRICATION FOR HORIZONTAL STAB REAR SPAR ATTACHED ANGLE 65B03779-12.SDR ASAA1077380Stiffener · crackedRT STAB INNER SPAR AT STAB L/E STA 78.29 HAS CRACKED VERTICAL STIFFENERS IN 4 PLACES.SDR AALA20100116TUL03Plate · damagedHORIZONTAL STABILIZER LUG PLATES NUMBERS 1, 2, 3, 4, 5, 6, 7 AND 8 BORE OUT OF LIMITS. REPLACED THE EIGHT LUG PLATES PER TASK CARD 55-94-05.SDR VGQY2010070200043Doubler · crackedRT HORZ STAB TIP AREA, MOST O/B RIB WEB LWR CHORD FOUND CRACK. REMOVED AND REPLACED EXISTING REPAIR DOUBLER PER SRM 52-30-06 REV 166, FIGURE 1. REPAIR DIMENSION: 12.50 INCH BY 6.00 INCH; INSPECTION THRESHOLD: 20,000 FLIGHT CYCLES FROM DELIVERY OF AIRPLANE; SDR CA091209005Bracket · cracked(CAN) BRACKET CRACKED IN OTBD RADIUS.SDR SWAA097414Structure · crackedDURING SCHEDULED 8Y CHECK, FOUND HORIZONTAL STABILIZER CRACKED AT STA 101.9. REPAIRED STABILIZER PER AAR EA.SDR SWAA097413Structure · crackedDURING SCHEDULED 8Y CHECK, FOUND HORIZONTAL STABILIZER CRACKED AT STA 138.7. REPAIRED STABILIZER PER AAR EA.SDR USAA2009120393300Bolt · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON LEFT HORIZONTAL STABILIZER THREAD BOLT AT FRONT SPAR UPPER CLEVIS. REPLACED LEFT HORIZONTAL STABILIZER THREAD BOLT AT FRONT SPAR UPPER CLEVIS IAW B737 AMM 27-41-11.SDR CALA2013091191210Structure · damagedRT HORIZONTAL STABILIZER AFT UPPER CHORD, STATION 2590, RBL 43.5 A FASTENER HOLE WAS FOUND DAMAGED DURING COA 850111. OVER-SIZED HOLE TO APPROXIMATELY 0.469 INCHES & INSTALLED BOLT WITH NUT IAW UA-EVA-72110 & FAA FORM 8100-9. (DIFFICULTY DATE SUBMITTED AS 11/SDR USAA2009120393301Bolt · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON BOLT AT LEFT HORIZONTAL STABILIZER FRONT SPAR LOWER CLEVIS AT BS 1085. REPLACED BOLT AT LEFT HORIZONTAL STABILIZER FRONT SPAR LOWER CLEVIS AT BS 1085 IAW B737 AMM 27-41-11.SDR EE4Y090354Support Angle · crackedEMPENNAGE LT HORIZ STABILIZER L/E AREA AT STA XI-7 SUPPORT TEE CRACKED.SDR CA091021008Bracket · cracked(CAN) WHILE PERFORMING AN EDDY CURRENT INSPECTION TO COMPLY WITH A PHASE 31 SID INSPECTION, A CRACK WAS DETECTED IN THE OUTBOARD BRACKET THAT ATTACHES THE RT ELEVATOR TO THE H STAB. THE CRACK WAS NOT DETECTABLE VISUAL INSPECTION ALONE. (TC 20091021008)SDR SWAA096122Fitting · corrodedDURING SCHEDULED 18Y CHECK, FOUND LT HORIZONTAL STABILIZER FITTINGS LUG FACE CORRODED. REPAIRED FITTINGS PER SRM.SDR USAA2009102792887Strap · corrodedSAL - Q2 - MAJOR REPAIR - CORROSION ON UPPER CHORD OF RIGHT HORIZONTAL STABILIZER TRAILING EDGE AT STAB STA 83.5. REPAIRED UPPER CHORD OF RIGHT HORIZONTAL STABILIZER TRAILING EDGE AT STAB STA 83.5 IAW B737 SRM 55-10-13 REPAIR 3.SDR USAA2009101592777Plate · corrodedSAL - Q2 - MAJOR REPAIR - CORROSION ON LEFT HORIZONTAL STABILIZER HINGE FITTING PLATE NR 3 AT ELEV STA 66.54. REPLACED LEFT HORIZONTAL STABILIZER HINGE FITTING PLATE NR 3 AT ELEV STA 66.54 IAW B737 SRM 51-10-02 & 51-40-02.SDR CALA2009091400545Fitting · gougedLEFT HORIZONTAL STABILIZER FORWARD LOWER FITTING GOUGED AT AFT INBOARD SIDE. BLENDED OUT THE GOUGE ON LEFT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR CHORD COMPLIED WITH STEPS 1 THRU 6 REF ECRA 5510-02055.SDR SWAA095636Cap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT HORIZONTAL STABILIZER END CAP DELAMINATED. REMOVED AND REPLACED END CAP PER MM.SDR USAA2009090492376Beam · corrodedCLT - Q3 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON LEFT HORIZONTAL STABILIZER BEAM UPPER SURFACE AT AFT HINGE LINE AT STAB STA 193.9. REPAIRED LEFT HORIZONTAL STABILIZER BEAM UPPER SURFACE AT AFT HINGE LINE AT STAB STA 193.9 IAW B737 SRM 55-10-13 RESDR USAA2009090492375Beam · corrodedCLT - Q3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT HORIZONTAL STABILIZER BEAM AT STAB STA 239.9 AT TRAILING EDGE. REPAIRED RIGHT HORIZONTAL STABILIZER BEAM AT STAB STA 239.9 IAW B737 SRM 55-10-13 REPAIR 3.SDR 2009FA0000722Bracket · crackedDURING SCHEDULED A, B, AND C INSP FOUND ROLLER BRACKETS CRACKED ON LT AND RT INBD FWD HORIZ STAB RIBS. REPLACED INBD RIB COMPONENTS WITH IMPROVED PN COMPONENTS IAW MFG COMMUNIQUE 83. RECOMMEND MFG ISSUE A RECOMMENDED SB OR KIT TO REPLACE THE ORIGINAL PN COMPSDR 2009F00063Bracket · crackedDURING SCHEDULED A, B, AND C INSP FOUND ROLLER BRACKETS CRACKED ON LT AND RT INBD FWD HORIZ STAB RIBS. NEW RT INBD RIB ASSY HAD BEEN INSTALLED 1190.3 HRS PREVIOUSLY FOR REPLACEMENT OF CRACKED ROLLER BRACKETS. INSTALLED NEW IMPROVED PN RIBS AND BRACKET ASSY.
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