JASC 5532
Service difficulty reports · 1,754
Reports filed under 5532 · Vertical 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 = '5532' 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 = '5532' 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 96ZZZM724Vertical Fin · dentedCLT - INSPECTION VISUALLY FOUND A DENT LOCATED AT VERTICAL STABILIZER MEASURING 1 INCH BY 2.5 INCH AT FIN STATION 209.90, RIGHT INSPAR. CUT OUT DAMAGE, INSTALLED DOUBLER AS PER USAIR EA NR 40708. (M)SDR 96ZZZM704Skin · damagedCLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STATION 218 RIGHT TRAILING EDGE PANEL. COMPOSITE REPAIRED AS PER BOEING SRM 51-40-13. (M)SDR USAA960266Skin · chaffedPIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND .25 INCH BY 2 INCH CHAFFED .021 DEEP AT VERTICAL STABILIZER FORWARD LEFT SKIN. INSTALLED DOUBLER REPAIR PER SRM 55-01 FIG 2 SHEET 2. (M)SDR P5CA9600036Skin · delaminatedFOUND DELAMINATED AREA ON RIGHT STABILIZER UPPER SURFACE AHEAD OF OUTBOARD ELEVATOR AND BEHIND REAR SPAR. REPAIRED IAW SRM 51-40-06.SDR P5CA9600035Panel · delaminatedFOUND LEFT SIDE PANEL NR 324AL ON VERTICAL STABILIZER DELAMINATED. REPAIRED IAW SRM 51-40-06.SDR P5CA9600197Le Skin · dentedFOUND LOWER VERTICAL FIN LEADING EDGE SKIN DENTED AT STA 124 AND STA 220. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 55-30-03.SDR P5CA9600198Panel · puncturedFOUND VERTICAL FIN ACCESS PANEL PUNCTURED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 53-30-10.SDR 96ZZZM145Le Cap · corrodedLEVEL 2 CORROSION, LOWER END OF NR 2 VERTICAL STABILIZER LEADING EDGE CAP IS CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. (M)SDR 96ZZZM144Skin · corrodedLEVEL 2 CORROSION, VERTICAL STABILIZER LEADING EDGE SEGMENT NR 1 UPPER END HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. (M)SDR MALA954783Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT VERTICAL STABILIZER SKIN. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 55-90-30. (M)SDR TSAA9555209Skin · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND VERTICAL STABILIZER, LT SKIN EXFOLIATED APPROXIMATELY 2 INCHES BY .50 INCH JUST ABOVE AFT FUSELAGE TO STABILIZER MOUNT BOLT. REPAIRED PER ECO 2649. AIRCRAFT RETURNED TO SERVICE. (X)SDR AALA952082Skin · corrodedTUL - FOUND 1 INCH CRACK IN LEFT SIDE OF VERTICAL STABILIZER SKIN EXTENDING FROM FASTENER HOLE, FS 1212. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO11697 DATED 6-23-95. (M)SDR EISA95433Skin · crackedVERTICAL STABILIZER RIGHT SIDE, JUST BELOW NR 7 VORTEX GENERATOR FROM TOP, SKIN CRACKED AT RIVET HEAD. STOP DRILLED CRACK PER SRM 55-30-3. HFEC CONFIRMED CRACK CONTAINED BY STOP HOLE. EXTERNAL DOUBLER INSTALLED AND SEALED PER SRM 55-30-3. (M)SDR CAL951102Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER, 24 INCHES FROM LEADING EDGE. THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-6. (M)SDR MWEA95353Skin · chafedDURING CORROSION TASK INSPECTION OF VERTICAL STABILIZER, FOUND THE LEFT HAND FORWARD SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. MAINTENANCE REMOVED AND REPLACED SKIN IAW 55-01 PG 1, AIRCRAFT RETURNED TO SERVICE.SDR DL72E954025Skin · crackedAT HMV, FOUND VERT STABILIZER SKIN STOPPED DRILLED 3 TIMES AT RT FS 1333 AT BOTTOM OF VERT FIN. REPAIRED PER MM 55-30-0 PG 801.SDR USAA951095Skin · gougedPIT - C-1 CHECK INSPECTION, FOUND GOUGE 5 INCH LENGTH AND .047 DEEP, MAXIMUM AT THE TOP IN VERTICAL STAB RIGHT SIDE NEAR RIB NR 5, UNDER ICE SCRAPPER. INSTALLED EXTERNAL DOUBLER REPAIR PER USAIR EA NR 31389. (M)SDR P5CA9500782Panel · puncturedHOLE IN AFT WEB OF VERTICAL STABILIZER AT THE OPENING FOR THE UPPER RUDDER ACTUATOR. REMOVED DAMAGED AREA AND REPAIRED PER BOEING SRM 51-40-3.SDR CAL950923Skin · crackedKUL - INSPECTION FOUND A 1.5 INCH CRACK IN SKIN UPPER SURFACE FORWARD OF VERTICAL STABILIZER REAR SPAR ON RIGHT SIDE. THE SKIN WAS REPAIRED IAW ECRA 5530-01159. (M)SDR IXXA199583Skin · corrodedDURING C-CHECK, CORROSION WAS FOUND UNDER THE VERTICAL STABILIZER AFT SPAR CLOSE-OUT PANEL JUST FORWARD OF THE UPPER RUDDER DAMPER. THE CORRODED PARTS WERE REMOVED, AND A NEW SKIN AND FITTING WERE INSTALLED IAW COTNEY ENGINEERING DRAWING SKA95164-1, DATED 8/2SDR MWEA95295Skin · errodedDURING INSPECTION, VERTICAL STABILIZER SKIN WAS FOUND CHAFED BEYOND LIMITS UNDER LEFT AFT HORIZONTAL STAB FAIRING. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN IAW SRM 55-30-0 FIG 7, 55-01 FIG 4 SHT 2. RETURNED A/C TO SERVICE.SDR MWEA95287Skin · errodedDURING INSPECTION, THE VERTICAL STABILIZER SKIN WAS FOUND CHAFED BEYOND LIMITS UNDER THE LEFT FWD HORIZONTAL STAB FAIRING. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN IAW SRM 51-10-2A, 51-30-2, 51-30-5, 55-30-0. RETURNED A/C TO SERVICE.SDR DL72S953379Skin · crackedFOUND DURING E-2 LETTER CHECK, .5 INCH CRACK EXTENDING FROM RIVET AT PNL 9523. REPAIRED PER MM 54-30-0.SDR DL72W953109Skin · crackedFOUND DURING D-2 LETTER CHECK - .75 INCH CRACK IN VERT STAB SKIN RT SIDE JUST AFT OF NR 2 ENG NOSE COWL AT PANEL 9516 . REPAIRED PER M/M 54-30-0, PG 801-802.SDR 95ZZZM530Skin · crackedMCI - DURING OP-17, FOUND A ONE INCH CRACK IN SKIN ON VERTICAL STABILIZER LEFT SIDE AT BASE, FS 1330. STOP DRILLED CRACK PER SRM 51-10-1, AND REPAIRED PER ARA9370A. TOTAL CYCLES 24,723.SDR P5CA9500443Le Panel · dentedFOUR DENTS ON VERTICAL FIN LEADING EDGE PANEL. BLENDED OUT DAMAGE PER BOEING SRM 51-10-01.SDR DL72S952961Skin · crackedSKIN CRACKED, .50 INCH CRACK IN VERT STAB SKIN RT SIDE AT FRONT SPAR AREA BELOW PANEL 9501. REPAIRED PER SRM 55-30-3 FIG 2, AT HMV.SDR DL72S952869Skin · damagedAT HMV, FOUND TIME LIMITED REPAIR RT SIDE VERTICAL STAB SKIN AT TORQUE BOX AREA. INSTALLED PERMANENT REPAIR PER MM 55-30-0 FIG 801.SDR UPS803619Skin · corrodedWHILE IN C-CHECK MAINTENANCE, FOUND CORROSION AND CRACKS AROUND FASTENERS AT VERTICAL STAB LEADING EDGE ON UPPER EDGE LT SIDE. REPAIRED IAW SRM 55-2-0.SDR DL72S952612Skin · crackedFOUND ON A2 LTR CK, 1.125 INCH CRACK VERTICAL STABILIZER SKIN LT SIDE STA 110.400 S-9. REPAIR INSTALLED DOUBLER PER SRM 55-30-3.SDR DL72K952535Skin · crackedFOUND DURING A-2 LETTER CHECK - 3 EACH, .25 INCH CRACKS JUST FORWARD OF LOWER CORNER OF PNL 9501 LT SIDE, 3 EA .25 INCH CRACKS JUST FORWARD OF LOWER CORNER OF PNL 9501 RT SIDE. BOTH ITEMS REPAIRED PER MM 54-30-0, PG 801.SDR 95ZZZX5886Skin · corrodedWHEN AIRCRAFT WAS STRIPPED FOR PAINTING, SEVERE CORROSION WAS NOTED WITH HOLES THROUGH SKIN AND INTO HONEYCOMB. APPEARS TO BE INTERGRANULAR CORROSION, POSSIBLY STARTED AT MANUFACTURING PROCESS.SDR ABXA9500806Skin · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT VERTICAL STABILIZER SKIN GOUGED UNDER THE LOWER HORIZONTAL STABILIZER FAIRING. REPLACED VERTICAL STAB SKIN IAW DC-9 SRM CHAPTER 51-30-2.SDR DL757952168Le Skin · damagedDURING HMV, FOUND A TEMPORARY REPAIR INSTALLED ON THE LEADING EDGE OF THE VERTICAL STAB. THE REPAIR IS LOCATED MID SPAN. THE SHOP INSTALLED A PERMANENT REPAIR PER THE SRM 55-30-01.SDR UPS803163Skin · corrodedWHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON INNER SKIN BETWEEN LONGERONS 30L AND 32L, AT FS 1746. REPLACED SKIN PER DOUGLAS DRAWING NR 5649329.SDR DL73E952016Le Skin · dentedDURING SHOP INSPECTION, VERTICAL STABILIZER L/E WAS FOUND DENTED BEYOND LIMITS. REPAIRS ACCOMPLISHED PER SRM 55-30-6.SDR DL72W951979Skin · crackedFOUND ON B-2 LETTER CHECK, .375 CRACK AT VERTICAL STABILIZER EXTERIOR SKIN RT SIDE STR 910 AT BASE OF VERTICAL. REPAIRED AS PER M/M 55-30-0 PG 801.SDR UPS803130Skin · corrodedDURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON 4 MOUNTING HOLES OF VERTICAL STABILIZER ANTENNA ON STABILIZER SKIN. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0.SDR DL73S951971Le Skin · dentedDURING SHOP INSPECTION, VERTICAL STABILIZER LEADING EDGE PANEL WAS REPAIRED FOR A DENT AT 51 INCHES FROM THE LOWER END OF PANEL. DAMAGE WAS REPAIRED PER SRM 55-30-6.SDR DL72K951354Skin · crackedA .5 INCH CRACK RT SIDE OF VERT STAB BELOW AND AFT OF SADDLE PANEL 9501. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3.SDR DL72K951353Skin · crackedA ONE INCH CRACK LT SIDE OF VERT STAB AT STR-6 APPROX FIN STA 160. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3.SDR DL72K951352Skin · crackedA .5 INCH CRACK RT SIDE OF VERT STAB BELOW PANEL 9501. FOUND DURING B-1 LTR CK. REPAIRED PER SRM 55-30-3.SDR DL72S951334Skin · crackedA 1.25 INCH CRACK IN VERT STAB SKIN RT SIDE AT CUTOUT FOR PANEL 9501 SADDLE PLATE. FOUND DURING E-2 LR CK. REPAIRED PER SRM 55-30-3 PAMM.SDR 95ZZZX2288Chord · corrodedTHE VERTICAL STABILIZER, REAR SPAR, LT CHORD AT STABILIZER, STA 225, WAS FOUND SEVERELY CORRODED DURING A RE-ENGINE MODIFICATION. THE CAUSE IS PROBABLY A LACK OF DRAINAGE AND AGE. THE ONLY WAY TO FIND THIS PROBLEM IS WITH AN X-RAY INSPECTION.SDR 95ZZZX2000Rebate · crackedMSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND VERTICAL STABILIZER ACCESS PANEL REBATE CRACKED, FOR PANEL NR 803, FABRICATED A NEW REBATE USING SAME MATERIAL AS ORIGINAL AND INSTALLED IAW WITH SRM 55-30-00 AND SRM 51-30-00.SDR ARWA031357Panel · corrosionDURING C-CHECK, FOUND VERTICAL STABILIZER TOP LEADING EDGE LEFT SIDE LEVEL 2 CORROSION. REMOVED CORROSION, FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-1 FIG 4. (M)SDR ABXA9500458Skin · chafedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT VERTICAL SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. REPLACED SKIN IAW DC-9 SRM CHAPTER 51-30-2.SDR USAA950333Skin · gougedPIT - DURING Q-2 INSPECTION, FOUND GOUGE RT VERTICAL STAB SKIN PANEL. BURNISHED GOUGES AREA AND INSTALLED INTERNAL DOUBLER PER USAIR EA 29729 AND SRM 55-01 FIG 2 SHEET 2. (W)SDR DL72E951122Skin · stop drilledDURING HMV, FOUND VERTICAL STABILIZER EXTERIOR SKIN HAS A STOP DRILL ON RT SIDE 20 INCHES FWD OF REAR SPAR AT FUSELAGE, REPAIRED PER FABRICATING DOUBLER PER MM 55-30-0 PG 801 CRACK PREVIOUSLY STOP DRILLED, DYE CHECKED CRACK AND NO FURTHER DAMAGE. INSTALLED DOSDR 95ZZZW231Skin · crackedMCI - DURING OP-17, FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER SKIN FUSELAGE, STA 1333. REPAIRED PER ARA 9113. TOTAL CYCLES 22210.
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