JASC 5512
Service difficulty reports · 7,887
Reports filed under 5512 · Horizontal Stabilizer, Plate/Skin, 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 = '5512' 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 = '5512' 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 97ZZZX2721Skin · tornA TEAR IN THE HORIZONTAL STABILIZER SKIN WAS FOUND DURING INSPECTION. THE DAMAGE WAS LOCATED ON THE RT INBOARD LEADING EDGE. THE DAMAGE MAY HAVE BEEN CAUSED DURING IMPROPER OR ROUGH INSTALLATION. THE DAMAGE WAS REPAIRED UNDER MANUFACTURER'S INSTRUCTIONS AND SDR UPS97823092Skin · corrodedINSPECTION TYPE:C/CK, LEFT HAND LOWER HORIZONTAL STAB INBOARD SIDE SKIN HAD CORROSION. REMOVED LT LOWER FAIRING AND I/B LOWER SKIN PANEL IAW DC8 SRM D581-3-0. REMOVED CORROSION IN SKIN PANEL AND REPAIRED SKIN PANEL AS PER REO 03183 REV A, ALODINED AND PRIMEDSDR AU970457Skin · corroded(AUS) LH AND RH HORIZONTAL STABILISER LEADING EDGE SKINS PNO 40155-14 AND PNO 40155-15 CONTAINED SEVERE INTERGRANNULAR CORROSION -FOUND FOLLOWING REMOVAL OF DE-ICE BOOTSSDR 97ZZZX2022Skin · damagedANNUAL INSP FOUND RT STAB SKIN WRINKLED AND BENT AT THE END OF TORQUE FITTING P/N 16809-03.SDR SWAA970409Skin · crackedDURING SCHEDULED D-CHECK, FOUND INTERIM REPAIR ON RT HORIZ STAB LOWER SPAR SKIN. INSTALLED PERMANENT REPAIR PER BOEING SRM.SDR CALA9700617Skin · dentedDURING D-INSPECTION, FOUND A DENT LT UPPER SURFACE HORIZ STAB STATION 54 L/E .125 DEEP 1.5 LONG .3125 WIDE. REPAIRED PER SRM 55-00-01 FIGURE 3.SDR MWEA97264Skin · crackedA .75 IN CRACK IN LT STAB UP SKIN FROM HI-LOK HOLE AT STA XHR7. A .125 IN CRACK FROM SAME HLE. REPAIRED IAW SB 55.42 FIG 4 AND DAC TEL MSP.0438/PDG 4/4/97.SDR CKSA97117Doubler · damagedDURING CPCP CHECK INSPECTION, FOUND RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE DAMAGED XFS135. REMOVED DAMAGE AND INSTALLED REPAIR IAW SRM 55-2-1, 51-1-8 AND 51-1-21. CORROSION TASK CARD NUMBER 6000-0551. NON-ROUTINE TASK CARD NUMBER 93240.SDR CKSA97105Plating · corrodedDURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION RIGHT HAND HORIZONTAL PANEL AT XE245 LOWER. REMOVED CORROSION, INSTALLED PLATING REPAIR IAW DC8 SRM 55-2-1. CLEANED AND TREATED AREA IAW 51-1-8. C-1 CHECK INSPECTION WORK CARD NUMBER 4001. NON-ROUTINE TASDR 9706899989Skin · crackedDURING L-CHECK, FOUND CRACK IN LEFT HORIZONTAL STABILIZER SKIN TOP INBOARD AFT AREA. REPAIRED PER EA 99-112305.SDR SWAA970315Skin · dentedDURING WALKAROUND INSPECTION, FOUND HORZ STAB L/E DENTED 4 FEET FROM ROOT AREA, LEFT SIDE. REPAIRED PER SWA RA 1-A55-0209R1.SDR MWEA97152Skin · crackedDURING INSPECTION, RT HORIZ STAB TOP AFT SKIN STA XHS 50, IMPROPERLY REPAIRED. MAINTENANCE REPAIRED IAW DAC TELEX SVC-MSP-0132/DLP 02-04-97.SDR HALA9759Skin · corrodedLEFT HORIZONTAL STAB INBOARD LEADING EDGE ASSEMBLY XRS 9.0 TO XFS 40 LEVEL 2 CORROSION AT OUTBOARD END AND AT FIELD FASTENERS. CUT OUT SKIN WHERE CORROSION CLEANUP WAS BEYOND MATERIAL LOSS LIMITS, FABRICATED REPAIR FILLER AND DOUBLER, TREATED, PRIMED AND INSTSDR HALA97034Skin · corrosionLEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE ASSY XFS 9.0 TO XFS 40.0 LEVEL 2 CORROSION AT OUTBOARD END AND AT FIELD FASTENERS. CUT OUT SKIN WHERE CORROSION CLEANUP WAS BEYOND MATERIAL LOSS LIMITS, FABRICATED REPAIR FILLER AND DOUBLER, TREATED, PRIMED AND SDR HAL9759Skin · corrodedLEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE ASSY XFS 9.0 TO XFS 40.0, LEVEL 2 CORROSION AT OUTBOARD END AND AT FIELD FASTENERS. CUT OUT SKIN WHERE CORROSION CLEAN-UP WAS BEYOND MATERIAL LOSS LIMITS. FABRICATED REPAIR FILLER AND DOUBLER, TREATED, PRIMED, SDR AU970908Skin · separated(AUS) STABILISER LEADING EDGE SEPARATED FROM THREE RIBSSDR AALA970577Skin · corrodedTUL - FOUND CORROSION ON UPPER SURFACE OF LEFT HORIZ STABILIZER INBOARD MOST TRAILING EDGE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 55-10-3 FIG 3. (M)SDR P5CA9700412Panel · crackedLEFT HORIZONTAL, TRAILING EDGED CRACKED AND NUMEROUS LOOSE FASTENERS BY POSITION LIGHT. REPAIRED PER BOEING SRM 51-40-09 AND 12-09-06.SDR HALA9780Skin · corrodedCOMPLY WITH HAI DPM P151859, RIGHT HORIZONTAL STABILIZER L/E HAS 2 CORROSION BLENDS. CUT OUT CORROSION IAW SRM 55-03 FIG 3. FABRICATED DOUBLER AND FILLER, LOCATED DRILLED, COUNTER SUNK PER DC9-SRM 55-03 FIG AND DC-9 SRM 51-30-2. TREATED AND PRIMED DOUBLER ASDR UPS97822359Skin · corrodedINSPECTION TYPE-C, THE LT HORIZ STAB L/E SKIN SURFACE AT STA XFS178.75 HAS EXFOLIATED CORROSION AROUND SCREW HEAD. REMOVED DAMAGED SKIN SECTION IAW SRM 55-21-1 FIG 4. FABRICATED FILLER, DOUBLER AND INSTALLED IAW SRM 55-2-1 FIG 4.SDR 97FDEA00124Skin · crackedNR 0488 48, FOUND 2 CRACKS IN THE CONSTANT SECTION OF THE HORIZONAL STABILIZER. CRACK NR 1 IN RT UPPER PLANK NR 7 (P/N 7228-1), CRACK IS .250 INCH LONG NR 7 BOLT HOLE FWD OF AFT END. CRACK NR 2 IS IN THE UPPER LT AFT CORNER 3 HOLE FWD OF AFT END, CRACK LENGTSDR MASA97014Panel · looseDURING INSPECTION THE LEFT OTBD CLOSING PANEL COMMON TO THE HORIZONTAL STABILIZER WAS FOUND WITH LOOSE ATTACH BOLTS. THE BOLTS WERE TIGHTENED AND THE AIRCRAFT WAS RELEASED AIRWORTHY FOR SERVICE. (X)SDR DL72S970326Panel · brokenON WALK AROUND ON GROUND GEG, FOUND PANEL 9216 PARTIALLY MISSING FROM BOTTOM OF HORIZONTAL STABILIZER. ONE QUARTER OF PANEL WAS MISSING. REPLACED PANEL MFG P/N 65-20657-26.SDR P5CA9700268Panel · dentedDENT AND ABRASION, TOP RT STABILIZER L/E PANEL. REPAIRED PER SRM 55-10-03.SDR RRXA97036Skin · damagedDURING A MAINTENANCE VISIT, FOUND SKIN DAMAGE TO LEFT SIDE HORIZONAL STABILZER AT, XFS=185 AND XE=149. FABRICATED REPAIR AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R17.SDR DHL9780428CAccess Panel · crackedAT C-CHECK, HORIZONTAL STAB REAR SPAR ACCESS PANEL INBD OF NR 4 A-FRAME HAS SMALL CRACK. FABRICATED AND INSTALLED PANEL PER SRM 51-3-0.SDR 97ZZZX1533Skin · crackedLEFT HORIZONTAL STABILIZER LEADING SKIN CRACKED.SDR P5CA9700052Skin · dentedDENT ON RIGHT HORIZONAL STABILIZER LEADING EDGE. REPAIRED DENT PER BAC SRM 51-10-01 AND PERFORMED NDT INSPECTION PER BAC NDTM 51-00-00, PART 6 FIG 4.SDR 97ZZZX524Skin · dentedTEMPORARY REPAIR INSTALLED ON LT HORIZ STAB UPPER SIDE STA XE 103 YA189. REMOVED REPAIR FOUND DENTS. OUT OF LIMITS. CUT OUT DENTED AREAS IAW DOUGLAS DWG 312891/96-10-16-18. FABRICATED DOUBLERS PER SAME DWG. ALODINED AND PRIMED IAW DC 10 SRM 51-21-01. INSSDR CALA9700115Skin · creasedINSPECTION FOUND A CREASE IN LOWER OUTBOARD SKIN OF LT HORIZONTAL STABILIZER. THE CREASED AREA WAS CUT OUT. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 55-10-3, FIGURE 4.SDR RRXA96176Panels · crackedFERRY FLIGHT, DUE TO HORIZONAL STABILIZER DAMAGE. FOUND 2 EACH HORIZONAL STABILIZER LOWER PANELS DAMAGED AT STA XE160 AND XE171. CUT OUT DAMAGED PANEL AND STRINGER, FABRICATED NEW PANEL SECTIONS AND SPLICED IN IAW DOUGLAS DWG SRO8550001-7041.SDR 97ZZZX711Skin · corrodedFOUND HEAVY TO SEVERE CORROSION THROUGHOUT THE HORIZ STAB. CESSNA DID NOT PROVIDE ANY CORROSION PROTECTION AT TIME OF MANUFACTURE. REPLACED PART, CLEANED, TREATED, AND PRIMED WITH EPOXY PRIMER. RECOMMEND CESSNA DO LIKEWISE.SDR ABXA9700194Panel · delaminatedDURING C-CHECK, HORIZONTAL STABILIZER PANEL NR 3806 WAS FOUND DELAMINATED, NR CF-808. REPLACED THE PANEL IAW DC-9 SRM 51-10-4.SDR SCNA96406Skin · gougedDURING HEAVY MAINTENANCE, FOUND GOUGE ON LEADING EDGE OF LEFT HAND HORIZONTAL STABILIZER, APPROXIMATELY 13 FEET OUTBOARD OF FUSELAGE. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 55-10-1 FIGURE 13.SDR ZIAA961120Skin · bulgingMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED HORIZ STAB UPPER SKIN LT AT 2ND ELEV HINGE CORRODED. REPAIRED IAW DWG A74-R32. (X)SDR ZIAA961119Skin · bulgingMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED HORIZ STAB LOWER SKIN LT AT 2ND ELEV HINGE CORRODED. REPAIRED IAW DWG A74-R32. (X)SDR 96ZZZX5979Skin · corrodedFOUND CORROSION ON LEADING EDGE SKIN WHEN STAB BOOTS WERE BEING REPLACED. COULD HAVE BEEN CAUSED BY METAL NOT BEING PROPERLY TREATED WHEN MANUFACTURED OR BOOTS GOT HOLES IN THEM LETTING MOISTURE IN. SUBMITTER STATES PROPER TREATMENT OF METAL AND/OR GOOD BOOTSDR ABXA9700712Skin · erodedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKINS ERODED. REPAIRED LEFT HORIZONTAL STAB LEADING EDGE SKINS IAW ABX REA D955-16859-MR.SDR ZIAA96055Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT HOR O/B EXT. XE 290. XE 222. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR ZIAA96054Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. LT HOR O/B EXT. XE 271-273. XE 310-312.5. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR CALA9601871Hinged Panel · crackedINSPECTION FOUND A .50 INCH CRACK AROUND FASTENER OF LT HORIZONTAL STABILIZER LOWER TRAILING EDGE HINGED PANEL AT STA XE 158. THE AREA WAS REPAIRED IAW SRM 51-70-00.SDR MWEA96541Skin · gougedDURING D-CK, FOUND 2 GOUGES IN LT HORIZONTAL STAB SKIN, LOWER, AT STA XHS32 AND 45. INSTALLED DOUBLER REPAIR IAW SRM 55-03, FIG 19.SDR P5CA9600782Skin · corrodedLEVEL 1 CORROSION TOP OF RIGHT HORIZONTAL STABILIZER STA 335 RBL 260, STA 340 RBL 270, STA 310 RBL 260 TO 270, STA 260 TO 310 RBL 255.2, STA 310 RBL 260 TO 300, STA 0 TO 260 RBL 255, STA 0 TO 26 RBL 231, STA 0 TO 26 RBL 170. CORROSION REMOVED AND REPROTECTED SDR SCNA96294Skin · dentedDURING HEAVY MAINTENANCE, FOUND A DENT APPROXIMATELY 12 INCHES FROM THE INBOARD END OF THE RIGHT HAND HORIZONTAL STABILIZER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH SRM 55-10-00 AND 53-30-10.SDR AALA961434Skin · damagedAFW - LEFT AND RIGHT NR 3 STABILIZER UPPER SKIN PANELS HAVE SEVERAL DENTS, HAIL DAMAGE. PER MRG 757-957. REINSPECT EVER C-CHECK. (M)SDR MALA965145Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND ON RIGHT HORIZONTAL STABILIZER LOWER SKIN JUST OUTBOARD OF BL 72.43 AT LOCATION OF PREVIOUS REPAIR, A 3.5 INCH HORIZONTAL CRACK. REMOVED PREVIOUS REPAIR AND EXAMINED PREVIOUS DAMAGE AND FOUND A 1.5 INCH SDR P5CA9600710Skin · buckledBUCKLED SKIN ON LEFT HORIZONAL STABLIZER UPPER TRAILING EDGE. REPAIRED SKIN PER BAC SRM 51-40-09.SDR CALA9601390Skin · crackedINSPECTION FOUND INBOARD LEADING EDGE OF RT HORIZONTAL STABILIZER DENTED. A HFEC INSPECTION FOUND A .5 INCH CRACK. THE CRACKED AND DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-10-3.SDR 96ZZZX4964Skin · crackedCRACK FOUND IN LT FRONT SPAR OF HORIZONTAL STABILIZER JUST INBOARD OF LT ATTACH RIB. CRACK APPEARED TO STOP UNDER SIDE AT FUSELAGE CONTACT POINT 2 INCHES FROM FRONT SPAR. SUSPECT CAUSE WAS WEAR INTO STABILIZER SKIN FROM FUSELAGE SKIN EDGE CONTACT. FUSELAGE SDR RRXA96083Skin · damagedDURING C-CHECK, FOUND TEMPORARY REPAIR ON LT HORIZ STAB LEADING EDGE, O/B SECTION. REMOVED TEMPORARY REPAIR, FABRICATED INTERNAL AND EXTERNAL DOUBLERS AND STRAPS IAW DER APPROVED ENGINEERING SKETCH A98-R14, INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21.
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