JASC 5532

Service difficulty reports · 1,753

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.

SDR DALA2018022101058Skin Panel · crackedCRACK INDICATIONS IN L/E SKIN PANEL ATTACH HOLES BELOW SPLICE ZFS 52.267, LEFT HAND SIDE. HOLE 1, 2, 6, 7, 8, AND 9, TOP TO BOTTOM. NRC 018-0001:5530-01048-01/009 00251: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.Feb 20, 2018 · N945AT · Boeing 717200SDR DALA2018022101050Skin · crackedCRACK ON RAM AIR SCOPE AT VERTICAL STABILIZER LEADING EDGE. CRACKS ON RAM AIR SCOPE AT VERTICAL STABILIZER LEADING EDGE, WERE REPAIRED (WELDED) PER ER/A 382101-14MA REV H.Feb 20, 2018 · N963DN · Doug MD9030SDR FXGA201802141803Skin · dentedDENT ON VERTICAL STABILIZER LEADING EDGE AT VSS 90.Feb 14, 2018 · N151 · Doug DC6BSDR DALA2018021100816Skin · crackedCRACK ON VERT STAB SKIN LT SIDE NEAR FRONT SPAR STA ZFS=17. CRACKS ON VERT STAB SKIN LT SIDE NEAR FRONT SPAR STA ZFS=17.6 WERE REPAIRED PER SRM 51-30-8 SRM 55-01 FIG 2 (SHEET 2) AND SRM 51-60-0 PAR 5(O). PERFORM VISUAL INSPECTION, FREQUENCY NOT EXCEEDING C-CHEFeb 10, 2018 · N933DL · Doug MD88SDR DALA2018020800760Inlet · crackedCRACK RT SIDE OF RAM AIR INLET. HFEC OF CRACK IAW NDT SPM 06-10-01.001. WELDED CRACK IAW ER/A 382101-MA NO FLAWS NOTED. ALODINED DAND PRIMED THE AREA IAW ER/A 382101-14MA.Feb 7, 2018 · N941DN · Doug MD9030SDR DALA2018020700758Inlet · crackedDURING OVERSPEED INSPECTION, FOUND THE VERTICAL STAB RAM AIR INLET CRACKED. ACCOMPLISHED A REPAIR IAW PS 900-5-1, NR 4. IAW ERA 382101-14MA. OK FOR SERVICE.Feb 6, 2018 · N946DN · Doug MD9030SDR 7C7A2018020100362Skin · damagedDAMAGE ON THE RIGHT VERTICAL STABILIZER, UPPER SKIN PANEL P/N 85530012 BETWEEN RIBS 8 AND 9, AFT OF THE ACCESS PANEL CUTOUT. REMOVED DAMAGE , INSPECTED THE AREA FOR CRACKS AND DEBONDING INDICATIONS.Feb 1, 2018 · N887EA · Dhav DHC8106SDR DALA2018013000520Skin Panel · wornNON REMOVABLE VERTICAL STAB L/E PANEL IS WORN/FRETTED ON SKIN LOWER SURFACE AT ZFS 52.267, CENTER UPPER END OF PANEL. RESTORED FINISH PER SRM 55-30-01-1A.Jan 30, 2018 · N945AT · Boeing 717200SDR DALA2018013000499Skin · crackedCRACKS ( 2 EA ) ON DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER. DORSAL FIN L/E ACCESS PANEL 6301A CUTOUT AT VERTICAL STABILIZER WAS REPAIRED (AS PERMANENT) PER ER/A 516509-14MA (SECTION I) REV 4 AND SRM 51-30-2 AND 51-30-5.Jan 28, 2018 · N962DL · Doug MD88SDR IPXA2018011525475Skin · puncturedLOWER VERTICAL STAB REAR PANEL ASSY , INNER SKIN HAS PUNCTURE DAMAGE. REPAIRED IAW EO MD11-5430-66477-A.Jan 15, 2018 · N250UP · Doug MD11FSDR IPXA2018011525476Skin · damagedLOWER VERTICAL STABILIZER REAR PANEL ASSEMBLY. PANEL 364MR DAMAGE. REPAIR IAW MD11-5430-66477-B.Jan 15, 2018 · N250UP · Doug MD11FSDR IPXA2018011525477Skin · puncturedLOWER VERTICAL STABILIZER REAR PANEL ASSY RT SIDE. NO 364MR HAS PUNCTURE ON INNER SKIN LOCATED 5.4 INCHES FROM PANEL T/E AND 17.5 INCHES FROM UPPER EDGE, PUNCTURE MEASURES .200 X .250. CLASSIFIED AS A MAJOR REPAIR.Jan 15, 2018 · N250UP · Doug MD11FSDR 2018FA0000024Skin · corrodedVERTICAL STABILIZER LT SKIN CORRODED. REPAIRED IAW REPORT S-680-0081/11RDJan 11, 2018 · N369QS · Cessna 680CESDR JGVR20171221001Skin · corrodedREMOVED FIRST LOCK FASTENER COLLAR, JUST ABOVE APU STINGER, ON LT SIDE OF VERTICAL STAB AFT SPAR FACE. MECHANICALLY BLENDED CORROSION APX 3 INCHES ABOVE APU STINGER PANEL 342AB. SUBMITTED FINDINGS TO CESSNA ENGINEERING AND PERFORMED BLEND TREAT REPAIR PER TEXTDec 21, 2017 · N359QS · Cessna 680CESDR DALA2017112408325Skin · crackedCRACK ON VERTICAL STABILIZER SKIN. THE SKIN WAS REPLACED IAW SRM 51-41-02 0G, 51-40-05 0G, AND DWG 5936143, REV AS.Nov 23, 2017 · N995AT · Boeing 717200SDR C77A20171122001Skin · crackedDURING BASIC CHECK, AN APPROXIMATELY 1.25 INCH LONG CRACK WAS DISCOVERED ON THE VERTICAL STABILIZER RT SKIN JUST AFT OF THE HOISTING POINT. REPAIRED IAW ETD2017-170-099340A.Nov 22, 2017 · N617CZ · Emb ERJ170200LRSDR FDEA201711123333Doubler · dentedVERTICAL STAB LT SIDE DENTED JUST AFT OF ACCESS PANEL NR 373GL. REPAIRED VERTICAL STAB LT SIDE REF SRM 55-00-01 FIG 3 SHT 2 VOL I.Nov 12, 2017 · N559FE · Doug MD1010FSDR DALA2019091389998Skin · damagedVERT STAB / RT FWD TORQUE BOX LOWER PANEL. REPAIR OF OUTER SKIN DAMAGE.Nov 10, 2017 · N727TW · Boeing 757231SDR DALA2017110407938Skin · damagedVERTICAL STAB LOWER LE SKIN AT ZFS 52 WORN AND CHAFED. SKIN SPLICE ON INNER SURFACE 15 INCHES ALONG LEADING EDGE. REPAIRED IAW PRI 562910-14AD REV. 0, REV 1, AND REV. 2 AND ER/A 562910-14AD REV. ORIGINAL.Nov 3, 2017 · N946AT · Boeing 717200SDR DALA2017110407937Skin · damagedVERTICAL STABILIZER LEADING EDGE HAD SIGNS OF DISTRESS TO COUNTERSINKS, ALL FASTENERS ARE LOOSE. REPAIRED IAW PRI 562910-14AD REV 0, REV 1. AND REV 2, ER/A 562910-14AD, REV ORIGINAL.Nov 3, 2017 · N946AT · Boeing 717200SDR DALA2017100207189Skin · damagedVERTICAL STAB VSS 52, UPPER ROWS EIGHT FASTENERS COUNTERSINK HOLE OVERSIZED. REPAIRED THE VERTICAL STAB SKIN IAW SRM 55-30-01-2R-6, REPAIR 6, AND DWG SG95550001, REV ORIG.Oct 1, 2017 · N932AT · Boeing 717200SDR DALA2017100207176Skin · damagedVERTICAL STAB HAS 4 FASTENER HOLES WORN OUT OF LIMITS AT LEADING EDGE. REPAIRED IAW SRM 55-30-01-2R-6, REPAIR 6, AND DWG SG95550001, REV ORIG.Oct 1, 2017 · N932AT · Boeing 717200SDR SWAA2017102317293Panel · delaminatedUPPER FUSELAGE VERTICAL STABILIZER FIN PANEL 322B BOTTOM DELAMINATED. REPAIRED PANEL IAW EA.Sep 21, 2017 · N742SW · Boeing 7377H4SDR DALA2017091806918Fastener · damagedLOOSE AND SUNKEN FASTENERS ON SPLICE ZFS=52.267 UPPER & LOWER FASTENER ROWS AT VERTICAL STABILIZER L/E. HOLES AND COUNTERSINK OF REMOVABLE LEADING EDGE AND FIXED LEADING EDGE WERE EVALUATED AND WAS FOUND 80 OF 1/4 AND 99 OF 3/16 WITHIN LIMITS 5 OF 3/16 AND 1 Sep 17, 2017 · N916DE · Doug MD88SDR DALA2017082006316Skin · crackedTHREE CRACK INDICATIONS WERE CONFIRMED AT ZFS 49.267, 48.267, AND 44.267. REPAIRED IAW ER/A 560869-14AD, REV ORIGINAL, AND ETI 17-17-128, REV 3.Aug 19, 2017 · N977AT · Boeing 717200SDR EE4Y2017082104125Skin · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND THE EMPENNAGE, VERTICAL STABILIZER BETWEEN RIBS 11 AND 12 NEAR REAR SPAR RT SIDE SKIN WITH TWO DENTS CREASED.Aug 18, 2017 · N758B · Emb ERJ190100IGWSDR JR2R20170816192Skin · crackedLEFT DORSAL SKIN CRACKED ON LT SIDE AT ACCESS PANEL 6301A. REPAIRED THE SKIN IAW EA 38-2017-124.Aug 16, 2017 · N964GA · Doug MD83SDR DALA2017081506244Doubler · damagedDISTRESS LT HOLES (7 EA) ON REPAIR DOUBLER LE STA ZFS=52.267 VERTICAL STABILIZER. REPAIR DOUBLER ON LE STA ZFS=52.267 VERTICAL STABILIZER WAS REPLACED PER SRM 55-30-01 2R REP 7 AND SERVICE GENERAL REPAIR DRAWING SG95550001 REV B.Aug 14, 2017 · N977AT · Boeing 717200SDR AALA20170727006Panel · delaminatedDELAMINATION ON RIGHT VERTICAL STABILIZER BETWEEN THE AUXILIARY SPAR AND FRONT SPAR, VSS 195 TO 270. REMOVED AND REPLACED THE PANEL IAW SRM 51-70-10-2R, AND SRM 51-40-02.Jul 27, 2017 · N374AA · Boeing 767323SDR UIEA2017071301210Skin · dentedVERTICAL STAB L/E SECTION 321E DENTED. REPAIRED THE VERTICAL STAB L/E SECTION IAW EA 747-5530-28-A6824, REV IR.Jul 13, 2017 · N429MC · Boeing 747481SDR UIEA2017071301211Skin · dentedVERTICAL STAB L/E SECTION 321B HAS SEVERAL DENTS. REPAIRED VERTICAL STAB L/E SECTION 321B IAW EA 747-5530-28-A6835, REV IR.Jul 13, 2017 · N429MC · Boeing 747481SDR UIEA2017071301213Skin · dentedVERTICAL STAB L/E PANEL 321E FOUND A FOUR INCH DENT OVER RIB. REPAIRED THE VERTICAL STAB L/E PANEL VSS 529.801 IAW EA 747-5530-28-A6853, REV IR.Jul 13, 2017 · N429MC · Boeing 747481SDR 2017F00156Skin · corrodedVERTICAL STABILIZER LEFT AND RIGHT SKIN DAMAGE.Jul 12, 2017 · N313QS · Cessna 680CESDR DALA2017071205362Fastener · looseFOUND NUMEROUS LOOSE FASTENERS ON VERTICAL STABILIZER REMOVABLE LEADING EDGE AT STA ZFS 52. REPAIRED REF PRI 560042-14 REV 0 AND ER/A 560042-14 REV A.Jul 11, 2017 · N943AT · Boeing 717200SDR DALA2017071205360Fastener · looseVERTICAL STAB LEADING EDGE LOWER FASTENERS ARE LOOSE AT STA ZFS 52. COMPLIED WITH PRI 560026-14 REV 0 AND REV 1. REPAIRED REF ER/A 560026-14 REV ORIG.Jul 11, 2017 · N943AT · Boeing 717200SDR DALA2017070705275Panel · out of limitsSEVERAL COUNTERSINK OUT OF LIMITS ON REMOVABLE LEADING EDGE AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE AT VERTICAL STABILIZER (EHV) WAS REPAIRED IAW DRAWING SG95550001, REV ORIGINAL, AND JIC CARD 5530-01048-03.Jul 6, 2017 · N980AT · Boeing 717200SDR 2017F00145Access Panel · delaminatedVERTICAL STAB LEADING EDGE UPPER LEFT EDGE DELAMINATED.Jul 6, 2017 · N313QS · Cessna 680CESDR DALA2017070405178Panel · corrodedSEVERAL COUNTERSINKS OUT OF LIMITS ON REMOVABLE LEADING EDGE AT VERTICAL STABILIZER. REPAIRED IAW SERVICE GENERAL REPAIR DRAWING SG 95550001 REV ORIGINAL.Jul 3, 2017 · N980AT · Boeing 717200SDR DALA2017070205114Skin · damagedLOOSE FASTENERS ON LT/RT SIDE AT VERTICAL STABILIZER LEADING EDGE STRUCTURE (REPAIR DOUBLER) AND REMOVABLE LEADING EDGE, STA ZFS=52.267. SEVERAL COUNTERSINK ON REMOVABLE LEADING EDGE STRUCTURE WERE MEASURED ABOVE 0.540" WERE LIMIT IS 0.517" AND ABOVE 0.420" WEJul 1, 2017 · N980AT · Boeing 717200SDR DALA2017070105208Skin · dentedDENT 1 X 0.5 X 0.250 ON LT SIDE OF VERTICAL STAB, AUX BOX SKIN JUST ABOVE RIB 2, 6 INCHES FWD OF FRONT MAIN SPAR. ACCOMPLISHED A PERMANENT REPAIR IAW SRM.Jun 30, 2017 · N690DL · Boeing 757232SDR DALA2017062805139Skin · wornWEAR ON VERTICAL STABILIZER SKIN LEFT HAND SIDE. REPLACED IAW DWG 5936143 AND SRM 51-30-02 AND 51-30-05.Jun 27, 2017 · N928DN · Doug MD9030SDR DALA2017062705000Skin · damagedVERTICAL STAB LE, ZFS 52 SEAM HAS MANY LOOSE FASTENERS AND MANY AREAS OF FASTENER & LARGE AREA WASHER WEAR. COMPLIED WITH PRI 559680-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559680-14, REV ORIG.Jun 27, 2017 · N948AT · Boeing 717200SDR JGVR20170627001Skin · erodedVERTICAL STAB CAP LEADING EDGE IS ERODED THROUGH THE SURFACE SKIN. REPAIRED.Jun 26, 2017 · N846QS · Cessna 560CESSNASDR DALA2017062604952Skin · crackedVERTICAL STABILIZER RT SIDE, HAS CRACK INDICATION AT SEVENTH HOLE BELOW ZFS=52.267 IN SKIN. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.Jun 25, 2017 · N948AT · Boeing 717200SDR DALA2017062204921Skin · crackedRIGHT SKIN CRACKED VERTICAL STABILIZER. REPAIRED IAW ERA 556419-14.Jun 20, 2017 · N949DN · Doug MD9030SDR IPXA2017070518957Skin · damagedINSPECTION TYPE: 3C, VERTICAL STAB RT SIDE SKIN HAS DAMAGE AT ZFR 453.5 AND YV 247.0. REPAIRED IAW EA 011-5530-01-A6859, REV I/R, AND EO MD11-5530-64788-A. MAJOR.Jun 15, 2017 · N273UP · Doug MD11FSDR SWIA201743526Skin · dentedLEFT VERTICAL STAB HAS ONE DENT 10 INCHES FROM T/E AND JUST ABOVE THE NR 2 RIB. REPAIRED VERTICAL STAB IAW REO.Jun 14, 2017 · N907EV · Cndair CL6002B19SDR DALA2017060604517Screw · looseVERTICAL STAB LEADING EDGE APPROX STA ZFS 52, FOUR ROWS SPLICE 40 SCREWS LOOSE. SEE NR FOR ADDITIONAL INFORMATION 001-0235:5530-2005/003 00123 REPAIR PER SRM55-30-01-2R-6. FPI PER PS 900-6-3 NR 02.Jun 5, 2017 · N949AT · Boeing 717200SDR DALA2017052704314Skin · damagedVERTICAL STAB LE AT ZFS 52 HAS MANY WORN FASTENER HOLES, COUNTER SINKS, AND LOOSE FASTENERS. LT & RT SIDES, ABOVE & BELOW THE SEAM. REPAIRED IAW PRI 558868-14, REV 0.May 26, 2017 · N608AT · Boeing 717200SDR JR2R20170526361Skin · crackedVERTICAL STAB PANEL AT VSS ZFS-6.562, LT SIDE HAS A CRACK FROM EDGE OF PANEL EXTENDING 5/8 INCH PAST FASTNER. FIRST HOLE BELOW UPPER AFT CORNER OF INLET PANEL. VERIFIED BY NDT. REPAIRED THE SKIN IAW SRM 55-01.May 26, 2017 · N883GA · Doug DC983
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