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 RRXA96082Skin · corrodedDURING C-CHECK, FOUND LT UPPER HORIZ STAB LEADING EDGE HAD CORROSION IN 2 PLACES AT ATTACHMENT SCREWS, APPROX. XF=143 AND XF=153. REMOVED OLD REPAIR DOUBLER, FABRICATED NEW REPAIR DOUBLER FROM .063 7075T-6. TREATED, PRIMED AND INSTALLED IAW DER APPRVED ENGINSDR AALA961176Skin · corrodedTUL - FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE SKIN CORRODED, AT UPPER SKIN ABOVE OUTBOARD ELEVATOR FITTING. REMOVED CORROSION, TREATED AND INSTALLED EXTERNAL DOUBLER PER ESO1 697 DATED 6-21-96. (M)SDR 96UAL900588Skin · damagedAIRPLANE FERRIED TO OAK FOR ENGINEERING EVALUATION OF RT HORIZONTAL STABILIZER SKIN. DUE TO A SUSPECTED APU HOT START THE LOWER SKIN PANELS OF THE RT HORIZONTAL STABILIZER, DETACHABLE ELEVATOR AND INBOARD ELEVATOR SHOW SIGNS OF EXCESSIVE SKIN WRINKLING AND BUSDR P5CA9600416Wedge · loose fastenersLOOSE TRAILING EDGE WEDGE ON LEFT OUTBOARD HORIZONTAL STABILIZER BOTTOM AND TOP. REPLACED FASTENERS PER BOEING SRM 51-30-02.SDR USAA960525Skin · gougedINT - DURING Q-6 CHECK VISUAL INSPECTION FOUND TWO GOUGES .75INCH AND .625 INCH SKIN STABILIZER STATION 92.7 APPROXIMATELY 17 INCHES FROMAFT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)SDR USAA960524Skin · gougesINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO GOUGES 1 INCHAND .625 INCH SKIN STABILIZER STATION 226 15 INCHES AND 20 INCHES AFT OFFRONT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M)SDR USAA960517Skin · dentedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH INDENTEDAREA STABILIZER SKIN STATION 111.1 APPROX 12 INCHES FORWARD OF AFT SPAR.INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3. (M)SDR ABXA9700424Skin · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT HORIZONTAL STABILIZER UPPER SKIN ABOVE THE REAR SPAR. REPAIRED IAW ABX REA D955-15636-MR.SDR P5CA9600528Skin · corrosionLEVEL 1 MINOR SURFACE CORROSION ON LEFT HORIZ STAB LEADING EDGE STA 200. SURFACE CORROSION REMOVED AND AREA REPROTECTED PER BAC MM 51-21-03 AND BAC SRM 51-10-02.SDR HEEA967442Skin · damagedDURING PAINT PREPARATION FOUND THAT EXISTING PRIMER COAT WAS PEELING OFF STABILIZER AND THAT OUR PRIMER COAT WOULD NOT ADHERE TO EXISTING PRIMER COAT. BLASTED STABILIZER ASSY TO REMOVE EXISTING PRIMER COAT. FOUND THAT STABILIZER SKIN HAD SEVERALSMALL DENTS. SDR IXXA9692Upper Mid Panel · crackedDURNG ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL STABILIZER CENTER SECTION, THE UPPER MID PANEL WAS FOUND CRACKED. THE INSPECTION WAS ACCOMPLISHED IAW DOUGLAS SERVICE BULLETIN 55-15, USING THE NDT METHODS. THE PANEL WAS REPLACED. (M)SDR IXXA9691Panel · crackedDURING ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL CENTER SECTION, THE LOWER FORWARD PANEL WAS FOUND TO BE CRACKED. THE INSPECTION WAS ACCOMPLISHED IAW DOUG SERVICE BULLETING 55-15, USING THE NDT METHODS. THE PANEL WAS REPLACED. (M)SDR IXXA9690Panel · crackedDURING ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL STABILIZER CENTER SECTION, THE FORWARD UPPER PANEL WAS FOUND TO BE CRACKED. THE INSPECTION WAS WITHIN THE SCOPE OF DOUGLAS SERVICE BULLETIN 55-15, USING THE NDT METHODS CALLED OUT. THE PANEL WAS REPLACED. SDR SWAA960517Skin · damagedDURING SCHEDULED 1/4 D-CHECK, FOUND RT HORIZ STAB GOUGED AND DENTED AT 4 PLACES ON LOWER SURFACE, 122 TO 130 O/B FROM FUSELAGE, 10 FWD OF REAR SPAR. REPAIRED PER BOEING SRM.SDR SWAA960523Skin · dentedDURING SCHEDULED SV CHECK, FOUND LT HORIZ STAB L/E DENTED 2 PLACES. REPAIRED PER BOEING SRM.SDR HEEA967367Skin · chafedHOLES IN SKIN; SKIN CHAFED. CORRODED AND HAS DEFECTIVE RIVETS.SDR HEEA967366Skin · chafedHOLES IN SKIN; SKIN CHAFED. CORRODED AND HAS DEFECTIVE RIVETS.SDR UPS96820509Skin · crackedINSPECTION TYPE CS2, RT HORIZONTAL STAB LEADING EDGE SKIN CRACKED AT DOUBLER STA XFS21 6. REPAIRED PER UPS EO.SDR P5CA9600239Panel · delaminatedFOUND PREVIOUS REPAIR ON UPPER SURFACE LEFT HORIZONTAL STABILIZER TRAILING EDGE PANEL DELAMINATED. REPAIRED IAW SRM 51-40-06.SDR 96ZZZX3065Skin · crackedONGOING CRACKS ON TRIM TAB LOWER SKINS AND INBOARD RIBS AT TRIM TAB CONTROL ARM ATTACH POINT. SKIN AND/OR RIB HAS CRACKED FROM 2500-4000 HOURS. FIRST REPAIR WAS TO REPLACE SKIN AND RIBS WITH NEW PIPER PARTS AND THESE LASTED 1000-1500 HOURS BEFORE CRACKING AGSDR 96ZZZX3064Skin · crackedONGOING CRACKS ON TRIM TAB LOWER SKINS AND INBOARD RIBS AT TRIM TAB CONTROL ARM ATTACH POINT. SKIN AND/OR RIB HAS CRACKED FROM 2500-4000 HOURS. FIRST REPAIR WAS TO REPLACE SKIN AND RIBS WITH NEW PIPER PARTS AND THESE LASTED 1000-1500 HOURS BEFORE CRACKING AGSDR 96ZZZX3063Skin · crackedONGOING CRACKS ON TRIM TAB LOWER SKINS AND INBOARD RIBS AT TRIM TAB CONTROL ARM ATTACH POINT, SKIN AND/OR RIB HAS CRACKED FROM 2500-4000 HOURS. FIRST REPAIR WAS TO REPLACE SKIN AND RIBS WITH NEW PIPER PARTS AND THESE LASTED 1000-1500 HOURS BEFORE CRACKING AGSDR 96ZZZX3062Skin · crackedONGOING CRACKS ON TRIM TAB LOWER SKINS AND INBOARD RIBS AT TRIM TAB CONTROL ARM ATTACH POINT, SKIN AND/OR RIB HAS CRACKED FROM 2500-4000 HOURS. FIRST REPAIR WAS TO REPLACE SKIN AND RIBS WITH NEW PIPER PARTS AND THESE LASTED 1000-1500 HOURS BEFORE CRACKING AGSDR CALA9600661Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL UPPER SKIN. THE CRACK WAS LOCATED APPROXIMATELY 15 INCHES OUTBOARD FROM FUSELAGE. THE CRACKED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9 AND 51-20-3.SDR 96ZZZM976Skin · crackedSTL - DURING OP-9, FOUND A .25 INCH CRACK ON ONE SIDE AND A .5 INCH CRACK ON OTHER SIDE OF UPPER AFT SKIN PANEL LEFT HORIZONTAL STABILIZER INBOARD ATTACH HOLE. REPAIRED PER EMLR 66370.SDR UPS96820109Skin · corrosionINSPECTION TYPE: C. LEFT HORIZONTAL STABILILZER, LOWER SURFACE INBOARD T/E SKIN PANEL HAS CORROSION BULGES. REPLACED SKIN PANEL PER SRM 51-1-21.SDR 96ZZZM912Skin · damagedMCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT HORIZONTAL STABILIZER LOWER SKIN AND FRONT SPAR, FS 186 TO FS 255. REPAIRED PER ARA 9957 AND TWA AND STANDARD PRACTICES. (M)SDR W8PA960024Skin · dentedFOUND 2 INCH DENT IN LEFT HORIZONTAL STABILIZER LEADING EDGE. REPAIRED DENT IAW SRM 55-10-01. (M)SDR USAA960387Panel · crackedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND A 1.75 INCH CRACK IN SKIN PANEL JUST OUTBOARD OF REAR SPAR STATION XH=7.234 RIGHT SIDE HORIZONTAL STAB. REMOVED DAMAGE AND INSTALLED FILLER REPAIR PER SR09550010-3 AND USAIR EO NR 5592X156. (M)SDR DL72S960881Skin · damagedAT MID-VISIT, THE HORIZ STAB PANEL NR 9215 WAS FOUND TO HAVE A HOLE IN THE TOP SURFACE. THE HOLE WAS REPAIRED PER SRM 55-10-2.SDR AALA960582Skin · corrodedTUL - FOUND LOWER TRAILING EDGE HORIZ STABILIZER SKIN CORRODED. CUT OUT CORROSION AND REPAIRED PER ESO 11677 DATED 4/9/96. (M)SDR 96ZZZM901Skin · damagedMCI - DURING SPECIAL CHECK, FOUND LEFT STABILIZER LOWER SKIN DAMAGED. REPAIRED PER ARA 9959. (M)SDR SWAA960202Skin · crackedDURING SCHEDULED BC3 CHECK, FOUND CRACK AT RT HORZ STAB AT RIB STA 120.3 AND 129.5 ON AFT SPAR ON RT LOWER IN SPAR. REPAIRED PER BOEING SRM.SDR 96ZZZX3515Skin · buckledWHILE PERFORMING A PHASE 1-4 INSPECTION, NOTICED TOP CENTER SKIN OF THE HORIZONTAL STABILIZER WAS BUCKLED BEYOND LIMITS AS STATED IN THE SRM. WHEN SKIN WAS REMOVED FOR REPLACEMENT, A HIDDEN DAMAGE INSPECTION REVEALED UPPER AFT STRINGER WAS ALSO BENT AND DISTOSDR MWEA96084Skin · corrodedRT HORIZONTAL STAB SKIN INNER SURFACE CORRODED AT STA XHS 132 FWD OF AFT SPAR. INSTALLED DOUBLER REPAIR IAW DAC TELEX SVC-0RD-0033DLP.SDR MWEA96078Skin · corrodedFOUND RT HORIZONTAL UPPER SKIN AT STA XHS60 AND TRAILING EDGE HAS 2 SPOTS OF EXFOLIATION CORRSION. INSTALLED DOUBLER REPAIR IAW DAC TELEX SVC-ORD-0043.SDR USAA960337Skin · crackedPIT - DURING Q-4/C-6 INSPECTION, FOUND 1.5 INCH CRACK UPPER LEADING EDGE SURFACE HORIZONTAL STABILIZER LEFT SIDE APPROXIMATELY 6 FEET OUTBOARD OF VERT STAB. INSTALLED DOUBLER REPAIR .071 2024TS ALU PER SRM 55-03 FIG 3 AND SRM 55-01 FIG 2. (M)SDR ABXA9600469Panel · delaminatedDURING C-CHECK INSPECTION, FOUND PANEL 3703A DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-10-4.SDR ABXA9600467Panel · delaminatedDURING C-CHECK INSPECTION, FOUND PANEL 3806A DELAMINATED. REPLACED PANEL IAW DC-9 SERVICE BULLETIN DC-9-55-1.SDR 96FDEA00659Skin · crackedRT HORIZ STAB FWD UPPER PANEL HAS CRACK IND AT 2 FASTENER HOLES, FWD UPPER SPAR CAP AFT TANG, I/B OF CLOSING RIB PLANE, BEING THE 2ND AND 3RD HOLES. CRACK LENGTHS ARE APPROX .0937 TO .1875 INCH LONG AT THE PERIPHERY. C/W HFEC ON FWD SPAR UPPER REAR TANG NO DSDR AWXA960151Skin · dentedPAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND LT HORIZONTAL STABILIZER FIXED L/E DENTED 1.5 INCHES BY .040 INCH DEEP AT STA 65.73, APPROXIMATELY 8 INCHES OUTBOARD FROM FUSELAGE. REWORKED DENT TO WITHIN LIMITS PER SRM 51-40-1 AND SRM 5SDR CAL960413Skin · looseHOU - INSPECTION FOUND SEVERAL LOOSE RIVETS ON LEFT AND RIGHT SIDES OF RUDDER SKIN. THE RIVETS WERE REMOVED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-2. (X)SDR CAL960412Skin · crackedHOU - INSPECTION FOUND TWO 1.25 INCH CRACKS IN TOP RT SIDE OF RUDDER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2. (X)SDR UPS96805963Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB L/E SKIN AT ATTACHING SCREW HOLES HAD HEAVY CORROSION AT STA XFS 125 AND 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1.SDR UPS96805822Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZ STAB L/E SKIN AT ATTACHING SCREW HOLES HAS HEAVY CORROSION AT STA XFS 125 AND XFS 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1.SDR CAL960404Skin · crackedKUL - INSPECTION FOUND A DENT AND 1.25 INCH CRACK IN THE TOP SKIN OF THE LT HORIZONTAL STABILIZER INBOARD PANEL. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-71-00 AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 57-71-00, PAGE 65. (X)SDR P5CA9600211Panel · crackedFOUND SMALL CRACKS ON THE HORIZONTAL STABILIZER, RT T/E UNDER STATIC DISCHARGE BASE THIRD FROM OUTSIDE. REPAIRED IAW SRM 51-40-15.SDR 96FDEA00375Skin · crackedRT HORIZ STAB UPPER AFT SKIN PANEL HAS .5625 INCH CRACK AT K/B AFT CORNER APPROX 1 INCH FROM PANEL AFT EDGE, ADJACENT TO WORKING BULKHEAD.SDR P5CA9600210Panel · corrodedFOUND LEVEL ONE CORROSION AT RT HORIZONTAL STABILIZER TIP, AROUND STATIC DISCHARGE BASE SECOND FROM THE FRONT SIDE. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01.SDR AWXA960100Skin · dentedPAE - FLT NR 3868 - DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND THREE DENTS IN THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKIN AT RIBS NR 16, NR 10 AND NR 6. REMOVED AND RECONTOURED LEFT HORIZONTAL STABILIZER LEADING EDGE AND REINSTALLED PER SRM 55-10-01
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