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 ABXA070331Skin · corrodedRIGHT HORIZONTAL STABILIZER UPPER SURFACE WAS CORRODED APPROXIMATELY 30 INCHES OUTBOARD OF THE VERTICAL CAP. REPAIRED AREA IAW DC9 SRM 55-01 FIGURE 2, SHEET 2.SDR 2007UALA03940Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN CRACKED 59.5" - 61" OUTBOARD FROM INBOARD END OF STAB, 1.5" FWD OF AFT SPAR. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF STAB SKIN & ACCOMPLISHED NDT FOR CRACK CONTAINMENT. FABRICATED 2EA ACCESS HOLES TO FACILITATESDR EIA2007186Skin · crackedLT HORIZONIAL STAB TOP SKIN CRACKED AT STAB STA 560. TRIMMED OUT DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 55-10-03 FIG 7 AND EA-55-0053.SDR 2007UALA03865Skin Panel · dentedRT HORIZ STABILIZER LOWER SURFACE HAS DENT AT APPROX STA 290. REMOVED DAMAGE FROM RT HORIZ LOWER SURFACE & FABRICATED REPAIR DOUBLERS AND FILLERS. INSTALLED IAW SRM 55-10-01. INSPECTED AND APPROVED FOR RETURN TO SERVICE.SDR 07FDEA03699Skin · corrodedCORROSION PITS ON TOP REAR SKIN OF THS LT. REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFACE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101, PIT AREAS BETWEEN 200 AND 1500 MMXMM) REWORK ARESDR 07FDEA03698Skin · corrodedCORROSION PITS ON TOP FWD SKIN OF THS LT REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFACE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101(PIT AREAS BETWEEN 200 AND 1500 MMXMM) REWORK AREAS DSDR SWAA074520Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 184.7. REPAIRED SKIN IAW SRM.SDR SWAA074519Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 151.1. REPAIRED SKIN IAW SRM.SDR SWAA074518Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.SDR DALA1134469221Skin · crackedCRACKED AND BROKEN ON THE SKIN OF LT AND RT HORIZONTAL STABILIZER FAIRING REPAIRED PER MESSAGE 1-565796525-2SDR SWAA074467Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.SDR SWAA074468Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.SDR SWAA074454Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SWA EA.SDR ASAA0742011Skin · damagedDAMAGE TO LEFT HORIZONTAL STABILIZER TIP DUE TO CONTACT FROM AC PUSHING BACK. REFERENCE SDR ASAA0742008. TEMPORARY REPAIR TO LEFT HAND HORIZONAL STAB TIP REPAIRED IAW CASCADE ERO 7152 AND EA 5510 01304. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 6 MONTHS.SDR SWAA074284Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 101.9 AND STA 129.50. REPAIRED SKIN PER SRM.SDR SWAA074285Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.SDR ASAA0742008Skin · damagedDAMAGE TO LEFT HORIZONAL STABILIZER TIP DUE TO CONTACT FROM AIRCRAFT PUSHING BACK INTO ALLEY. INTERM REPAIR PER EA 5510 01303 AIRCRAFT RELEASED FOR FERRY FLIGHT TO YXX.SDR 2007UALA03391Skin · dentedRIGHT HORIZONTAL STABILIZER HAS DENT IN LEADING EDGE AT APPROX STA 176, 14 FT OUTBOARD OF FUSELAGE. REPAIRED DENT, PERFORMED EDDY CURRENT - NO CRACKS PRESENT.SDR IXXA07SMN214SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER, POINTS OF CORROSION ON UPPER SKIN FROM STA XE 28.843 TO STA XE 30.000.SDR BAQA200700029Skin · crackedDURING 500 HOUR AIRFRAME INSPECTION FOUND A CRACK IN THE SKIN OF THE HORIZONTAL STABILIZER. REMOVED AND REPLACED THE HORIZONTAL STABILIZER.SDR IXXA07SMN208SSkin · dentedDURING ROUTINE C CHECK INSPECTION, HORIZ STABILIZER EMPENNAGE INBD L/E EXT SKIN SHOWS (01EA) DENTS AT STA XFS 97.500 AND STA XFS 103.000.SDR SROM200700015Skin · gougedNR378 - RT STABILIZER LOWER SURFACE FOUND WITH A GOUGE IN THE SKIN ON THE RIB ATTACH LOCATION AT 138.7 DEPT IS 0.037 WHICH IS OVER 50 PERCENT. DAMAGED SECTION OF SKIN ON RT STABILIZER LOWER SURFACE LOCATION 138.7 REMOVED. REPAIR DOUBLER FABRICATED AND INSTALSDR SWAA073973Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA.SDR SWAA073942Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LEFT HORIZONTAL STAB OUTBOARD T/E LOWER SKIN SURFACE DELAMINATED. REPAIRED SKIN PER SRM.SDR 2007UALA02958Skin · crackedRIGHT HORIZ STAB LOWER SKIN IS CRACKED AT AFT SPAR 64 INCHES OUTBOAD. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL SKIN DOUBLER REPAIR & INSTALLED ACCESS HOLE CUTOUT REPAIR.SDR ASAA0741931Skin · dentedRIGHT HORIZONAL STAB DENTED AT STA 212.3 TO STA 221.5. DENT IS 5" L X 2.2" W X .082 DEEP. RECHECKED DIMS. DENT IS NOW A ZONE 3 DENT. INSP INTERNAL VISUAL INSPECTION OF DAMAGE AREA EVERY 400 FLT HRS OR LESS. IF CRACKS ARE FOUND OR DAMAGE BECOMES BIGGER REPASDR ASAA0741926Skin · dentedRIGHT HORIZONAL STAB DENT AT STA 212.3 TO 221.5. DENT IS 5" L X 2.2" W X .082 DEEP. RECHECKED DIMENSIONS. DENT IS NOW A ZONE 3 DENT. INSPECTED INTERNAL VISUAL INSPECTION OF DAMAGE AREA EVERY 400 FLT HRS OR LESS. IF CRACKS ARE FOUND OR DAMAGE BECOMES BIGGERSDR 2007UALA02873Skin · dentedDENT ON RT HORIZONTAL STABILIZER LEADING EDGE CAUSED BY BIRD STRIKE. REMOVED DAMAGE. INSTALLED INTERNAL DOUBLER REPAIR AND REPLACED DAMAGED RIB.SDR DHL2007741519Skin · dentedDENT ON LOWER SURFACE, RT HORIZ STAB, STAB STA 114.97. DENT BEYOND SERV LIMITS PER B727 SRM 55-10-1 FIG 2. CUT OUT DAMAGE, 3" BY 1.5", REMOVED PREVIOUS REPAIR DOUBLER ADJACENT TO DENTED AREA, FABRICATED SINGLE REPAIR DOUBLER FROM 2024-T3, .063" BY 17" BY 17.SDR UIEA200700284Panel · gougedPANEL 341BR RIGHT HORIZ STAB LEADING EDGE TOOLING MARKS AND GOUGES. REPAIRED TOOLING MARKS ON RIGHT LEADING EDGE OF HORIZ STAB IAW SRM 55-10-03.SDR USAA070574Skin · crackedRIGHT STAB L/E, LOWER O/B SURF, 43 INCHES FROM O/B END, ELONGATED & CRACKED HOLES. INSTALLED FREEZE PLUG & REPAIR DOUBLER PER EA 98762, DEFECT SIZE: 5 INCHES.SDR USAA070567Skin · crackedRIGHT HORIZONTAL STAB, LOWER SKIN AT REAR SPAR 86 INCHES FROM INBOARD END OF STAB HAS CRACK. FAB'D & INSTALLED PERMANENT REPAIR DOUBLER PER TR 57-10-07, DEFECT SIZE: 1.5 INCH.SDR USAA070554Rib · crackedRIGHT STAB L/E, NOSE RIB FWD CUTOUT, 167 INCHES FROM I/B END. BLENDED DAMAGE & RE-INSTALLED PART PER SRM 55-10-09, FIG 101, DEFECT SIZE: .063 INCH.SDR 07FDEA02463Panel · crackedDURING INSPECTION OF UPPER INTERIOR SKIN PANELS OF STB HORIZONTAL SECTION FOUND 1 PANEL P/N 7207-1 WITH CRACK. ACCOMPLISHED EA NR 8-5510-96123.SDR SWAA073309Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.SDR SWIA200718473Skin · dentedLEFT HORIZONTAL STABILIZER HAS LEADING EDGE DENT AT SECTION 10.91.DAMAGE FOUND TO BE A MAJOR REPAIR. C/W REO 601R-55-12-349. OK FOR SERVICE.SDR SWAA073249Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RH HORIZONTAL STAB SKIN CRACKED BETWEEN STA 129.50 AND STA 138.70. REPAIRED SKIN PER SRM.SDR SWAA073171Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.SDR ARWA20070608Skin · dentedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND LT HORIZONTAL STABILIZER XH 285.00 L/E LOWER SURFACE WITH DENT. REPAIRED L/E PLATING OF LT HORIZONTAL STABILIZER BETWEEN XFS 263 AND XH 285 IN ACCORDANCE WITH AIPSAC DRAWING NR AIPSAC-N661AVE-03/07, SHEET 1SDR DHL2007740554Skin · dentedLT STAB UPPER SKIN HAS 2 DENTS, LSTAB STA 41.5. REMOVED PANEL 9113 TO GAIN ACCESS IAW B727 SRM 51-30-2, CUT OUT DAMAGED AREA (DIM 33/4" BY 13/4"), FABRICATED REPAIR DOUBLER FROM 2024T3 .050" PO NR 9005049 (DIM 9 1/4" BY 4.5") IAW B727 SRM 55-20-3 FIG 1 AND 55SDR USAA070430Skin · crackedLEFT HORIZONTAL STAB L/E, 6TH SCREW HOLE FROM INBOARD END ON BOTTOM ROW HAS CRACK. REPAIRED BY INSTALLING FREEZE PLUG PER SRM 55-10-01 & EA 98671, DEFECT SIZE: .25 INCH.SDR 07FDEA01998Skin Panel · crackedDURING INSP OF HORIZ STAB CONSTANT SECTION SKIN PANEL, FOUND THREE LOWER INTERIOR SKIN PNLS WITH CRACK, P/N 7205-1, P/N 7204-1, P/N 7206-1. SEE ATTACHED SHEET FOR ALL REF (INSPECTION FINDING FORM). REPAIRED IAW EA NR 8-5510-96121.SDR 2007UALA01666Skin · crackedRIGHT HORIZONTAL STAB REAR SPAR LOWER SKIN APPROX 61 INCHES OUTBOARD OF EMPENNAGE CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL SKIN DOUBLER & 2EA LWR SKIN REINFORCED ACCESS PLATE REPAIRS.SDR SWAA072686Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM.SDR AMTA200700260Skin · crackedLT HORIZONTAL STAB LWR SKIN CRACKED 2 PLACES 1 INCH AND 1.25 INCHES IB SIDE OF RIB STAB 129.50, STA 1131 AND 1138. REPAIRED SKIN CRACKS 55-10-01. (K) 10-26-07 INSTALL L/E SRM 51-40-02. (M)SDR SWAA072659Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 92.70. REPAIRED SKIN PER SRM.SDR 07FDEA01963Skin · crackedLT DETACHABLE UPPER SKIN FOUND 1 CRACK AND 10 RIVETS LOOSE RIVETS. REPAIRED SKIN IAW SRM 55-10-00 VOL 1 FIG 8 AND REPLACED FASTENERS IAW SRM 51-35-02 VOL 2 PAR 12-10.SDR 07FDEA02208Panel · crackedTHS PANEL 331BB WITH CRACK AT RIB NR 3 P/N A55178013-004. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-112411.SDR 07FDEA02207Panel · crackedTHS PNL 331BB WITH CRACK AT RIB NR 4, P/N A55178014-004. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-112411.SDR USAA070400Skin · crackedSTA 110.5 - 113 AT TRAILING EDGE LOWER SKIN HAS CRACK. REPAIRED PER TYPICAL 55-10-07, SRM 55-10-01 FIG 201 REP 4, DEFECT SIZE: 2.5 INCHES.
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