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 DALA2017052404161Panel · crackedVERTICAL STABILIZER LOWER AFT CORNER IS CRACKED AT PANEL 370BL. REPAIRED IAW ERA 555250-14, REV O.May 22, 2017 · N935DN · Doug MD9030SDR SWAA2022012498303Retainer · crackedVERTICAL FIN PANEL 324AL SEAL RETAINER CRACKED AND WORN THRU ON AFT END / REMOVED AND REPLACED VERTICAL FIN PANEL 324AL SEAL RETAINER PER SRM 51-40-02May 13, 2017 · N7747C · Boeing 7377BDSDR DALA2017051403866Repair · damagedELONGATED SEVERAL HOLES ON PREVIOUS REPAIR DOUBLER AT VERTICAL STABILIZER LE SPLICE AT STA ZFS=52.267. REPAIR WAS ACCOMPLISHED PER ETI-17-17-060 REV 3 AND ER/A 535894-14AD REV A.May 13, 2017 · N939AT · Boeing 717200SDR FDEA201705091561Skin · corrodedVERTICAL STAB RT, HAD CORROSION BELOW UPPER RUDDER ACTUATOR. REMOVED CORROSION AND BLEND OUT IAW EA 8-5530-T0333328 P1, SRM 51-21-01, VOL II, SRM 51-21-02, VOL II, PGS 2-9, SOPM 20:10.10, PG 25, AND DPS 2.50.May 9, 2017 · N311FE · Doug MD1030FSDR FDEA201705091560Skin · corrodedVERTICAL STAB HAD SURFACE CORROSION JUST BELOW ACCESS PANEL NR 373GL. BLENDED OUT AND REMOVED CORROSION IAW EA 8-5530-T0333328 P1, SRM 51-21-01, VOL II, SRM 51-21-02, VOL II, PGS 2-9, SOPM 20:10.10, PG 25, AND DPS 2.50May 9, 2017 · N311FE · Doug MD1030FSDR AALA201705199025Skin Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX 82 INCHES FROM BOTTOM AND 24 INCHES FROM LEADING EDGE PANEL. REMOVED AND REPLACED PANEL IAW SRM 51-40-02-OG.May 6, 2017 · N202UW · Boeing 7572B7SDR 7C7A2017050500324Skin · dentedVERTICAL STABILIZER, LT SKIN DENTEDMay 5, 2017 · N891EA · Dhav DHC8106SDR DALA2017042103275Skin · damagedLOOSE ON TWO ROWS FASTENERS ABOVE THE SPLICE (9E/A) AND TWO ROWS FASTENERS BELOW THE SPLICE (28E/A) STA ZFS= 52.26 AT LE VERTICAL STABILIZER. WORK WITH CARD 5530-01045-08. COUNTERSINKS AND HOLES WERE EVALUATED AND WAS FOND 34 WITHIN LIMITS AND 3 OUT OF LIMITS.Apr 20, 2017 · N967DL · Doug MD88SDR SWAA2022012026720None · elongatedVERTICAL STAB L/E RH SIDE STA.136 HAS ELONGATED HOLE. / REPAIRED PER E.A 1-755-3500Apr 19, 2017 · BoeingSDR SWAA2022012026721None · elongatedVERTICAL STAB L/E RH SIDE STA.160 HAS ELONGATED HOLE. / REPAIRED PER E.A 1-755-3500Apr 19, 2017 · BoeingSDR EE4Y2017042003251Skin Panel · dentedEMPENNAGE, VERTICAL STABILIZER AT 250MM ABOVE RIB 8 BETWEEN STR 3 AND STR 4 RIGHT SIDE SKIN WITH DENT CREASED. THE CORRECTIVE ACTION WAS HANDLE UNDER THE OEM DISPOSITION ETD217-190-013503.Apr 19, 2017 · N983TA · Emb ERJ190100IGWSDR DALA2017041903197Skin · crackedVERTICAL STABILIZER, LT AND RT SIDE LEADING EDGE SKINS AND SPARS CRACKED. REPAIRED IAW AMOC 17-080, & 17-081. COMPLIED WITH PRI 557746-14 REV 0, 1, & 2, AND ERA 557746-14 AD, REV 0.Apr 18, 2017 · N994DL · Doug MD88SDR DALA2017041903190Skin · crackedVERTICAL STAB L/E HAS FOUR ATTACH HOLES INDICATING CRACKS ON LEFT SIDE OF L/E SKIN. STEPPED HOLES TO .265 IAW PRI 557746-14 REV . VERIFIED CRACK FREE IAW NDT SPM 06-10-001.003. REPAIRED IAW PRI 557746-14 REV 0, 1, & 2. COMPLIED WITH ERA 557746-14AD, REV ORIApr 17, 2017 · N994DL · Doug MD88SDR DALA2017040702810Skin · damagedSEVERAL ELONGATED HOLES ON VERTICAL STABILIZER LEADING EDGE AT ZFS=52.267. REPAIRED IAW SRM 55-30-01-2R-7, 51-41-01, AND 51-41-05.Apr 6, 2017 · N983AT · Boeing 717200SDR FDEA201704031267Panel · delaminatedDELAMINATION INSIDE THE VERTICAL STAB, LT SIDE PANEL AT VSS 200, 2 LOCATIONS. REPAIRED IAW EA F-5530-T0335605.Apr 3, 2017 · N913FD · Boeing 75728ASDR DALA2017040302755Skin · delaminatedDELAMINATED EXTERNAL SKIN RIGHT SIDE FRONT SPAR AT VERTICAL STABILIZER BETWEEN RIBS 3 & 4. REPAIRED THE SKIN IAW PRI 556232-14, REVISONS O, 1, 2, 3, 4, 5, 6, 7, AND ER/A 556232-14, REV ORIGINAL.Apr 2, 2017 · N660DL · Boeing 757232SDR EBVR20170327002Skin · crackedCRACK IN THE VERTICAL STAB CAP, REPAIRED CRACK IN VERTICAL STAB CAP IAW REPORT S-750-ATA51/01RD (STRUCTURAL REPAIR OF COMPOSITE LAMINATE STRUCTURES). REPAIRED.Mar 27, 2017 · N647QS · Cessna 560XLSDR IPXA2017032015321Skin · damagedLOWER VERTICAL STAB, LEFT SKIN DAMAGED. REPAIRED IAW EO MD11-5530063416-C.Mar 20, 2017 · N288UP · Doug MD11FSDR DALA2017030701845Skin · damagedVERTICAL STAB LEADING EDGE, 5TH FASTENER HOLE FROM LOWER EDGE IS OUT OF ROUND. REPAIRED IAW ER/A 556179-14.Mar 7, 2017 · N914DL · Doug MD88SDR DALA2017030301724Skin · damagedSEVERAL LOOSE FASTENERS WITH ELONGATED HOLES IN L/E VERTICAL WRAP AROUND SKIN PANEL ZFS 148.858. LT AND RT SIDES. REPAIRED THE SKIN PANEL IAW ER/A 553690-14 REV 0.Mar 2, 2017 · N974AT · Boeing 717200SDR DALA2017030201737Skin · damagedVERTICAL STABILIZER LEADING EDGE HAD AN ELONGATED HOLE ON LEFT LOWER EDGE. REPAIRED IAW SRM 55-30-05.Mar 1, 2017 · N924DN · Doug MD9030SDR ASOA201702251293Angle · bentLEFT AND RIGHT LOWER VISOR PANELS DAMAGED. REMOVED, FABRICATED NEW AND INSTALLED IAW ECTC SNIEO AV670-21200 S01, ECTC AV670-21405 S01 AND DRAWING AV670-21405.Feb 25, 2017 · N612QX · Cndair CL6002C10SDR DALA2017031602163Access Panel · corrodedDURING INSPECTION FOUND UPPER FUSELAGE VERTICAL STABILIZER ACCESS PANEL TO FUSELAGE SKATE ANGLE CORRODED O/B OF VERTICAL STAB FWD ATTACH BOLT BS 1016. MAINTENANCE REMOVED AND REPLACED UPPER FUSELAGE VERTICAL STABILIZER ACCESS PANEL TO FUSELAGE SKATE ANGLE O/B Feb 24, 2017 · N377DA · Boeing 737832SDR DALA2017030301722Skin · corrodedVERTICAL STAB L/E SKIN RIGHT SIDE AT ZFS=52.267 FWD 2 ROWS OF FASTENERS BELOW SPLICE ARE PULLING THROUGH SKIN AND HAVE EVIDENCE OF FRETTING CORROSION AROUND FASTENERS. J.C. 5530-01048-01, STEP 4. REPAIRED THE VERTICAL STAB L/E SKIN IAW JC 5530-01048-01 AND SFeb 22, 2017 · N974AT · Boeing 717200SDR DALA2017021901354Skin · crackedVERTICAL STABILIZER CRACKED ON THE RAM AIR ACCESS CUTOUT 6301A. REPAIRED IAW SRM 55-05, PAR. 6, FIG. 3.Feb 18, 2017 · N923DL · Doug MD88SDR DALA2017021901355Skin · crackedVERTICAL STAB AIR SCOOP LEFT LIP HAS A TWO INCH LONG CRACK, REPAIRED IAW ERA 382101-14MA, REV F.Feb 17, 2017 · N918DE · Doug MD88SDR DALA2017021201162Skin · crackedVERTICAL STABILIZER, CRACKS (3EA'S) ON VERTICAL STABILIZER DORSAL FIN LEADING EDGE ACCESS PANEL CUTOUT 6301A. DAMAGE AREA WAS REPAIRED PER SRM 55-05 FIGURE 3 SHEET 1. PERFORM DECAL CONDITION VISUAL INSPECTION EVERY "C" CHECK PER TOPP 30-10-70 PAR I PG 14.Feb 11, 2017 · N911DE · Doug MD88SDR DALA2017020400958Skin · damagedLEFT VERTICAL STAB L/E SPLICE VSS 52.267. FIRST ROW BELOW SPLICE HAD 21 LOOSE FASTENERS AND HAS 18 OVERSIZED/ELONGATED HOLES. REPAIRED ALL LOOSE FASTENERS, OVERSIZED, AND ELONGATED HOLES IAW DWG SG9555001.Feb 3, 2017 · N923AT · Boeing 717200SDR DALA2017020100922Skin · damagedLEFT VERTICAL STABILIZER FOUND SECOND HOLE FROM BOTTOM DAMAGED. REPAIRED IAW ERA 554885-14D.Jan 31, 2017 · N911DA · Doug MD9030SDR DALA2017012300578Skin · wornVERTICAL STABILIZER, WEAR ON LT AND RT OUTER SKIN BTW YV=256 AND YV=221 AT VERTICAL STABILIZER REMOVABLE TIP FAIRING. AREAS WERE BLEND OUT PER SRM 55-01 FIG 1 AND MEASURED WITH ULTRASONIC TEST PER NDT SPM 04-00-07 FIG3 SHEET 2, AS FOLLOW: UPPER RT SKIN, ORIGINJan 22, 2017 · N913DL · Doug MD88SDR DALA2017011500332Skin · damagedLEFT VERTICAL STAB L/E AT SPLICE VSS 52.267, UPPER TWO ROWS HAVE 26 LOOSE SCREWS & 22 OVERSIZED HOLES. INSTALLED A REPAIR IAW BSG 95550001 AND W/C 5530-01048-03.Jan 14, 2017 · N935AT · Boeing 717200SDR SWAA2017012611479Skin · erodedVERTICAL STABILIZER LEADING EDGE ERODED AT COMPOSITE PANEL. R&R VERTICAL STABILIZER PER WO.Jan 6, 2017 · N563WN · Boeing 737752SDR DALA2017010400047Fastener · looseLT VERTICAL STAB L/E SKIN BELOW ZFS 52.267 HAS 10 LOOSE SCREWS IN UPPER ROW BELOW SPLICE AND 2 LOOSE FASTENERS IN LWR ROW BELOW SPLICE REF AA WORK CARD 5530-01048-01 STEP 3. REPAIRED DAMAGED AREA IAW ER/A 551841-14AD REV O.Jan 3, 2017 · N933AT · Boeing 717200SDR SCNA20161231411Fastener · damagedVERTICAL STABILIZER LEADING EDGE NEEDS ATTACHING HARDWARE REPLACED. REPLACED DAMAGE OR MISSING HARDWARE ON VERTICAL STABILIZER LEADING EDGE.Dec 31, 2016 · N816SY · Boeing 7378Q8SDR DALA2016122810100Skin · crackedCRACK CUTOUT ACCESS PANEL 6301A OF VERTICAL STAB PREVIOUS DOUBLER REPAIR WAS REMOVED, NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 55-05 FIG 3.Dec 28, 2016 · N920DL · Doug MD88SDR SWAA2017012311357Skin · crackedLEFT HORIZONTAL STABILIZER RIB FLANGE CRACKED AT BS 92.70. REPAIRED THE SKIN IAW ER AND EA.Dec 24, 2016 · N401WN · Boeing 7377H4SDR SCNA20161222376Skin · erodedVERTICAL STABILIZER LEADING EDGE COMPOSITE ERODED ON LOWER LEADING EDGE. EVALUATED, SEALED EXPOSED COMPOSITES AND RESTORED DECORATIVE FINISH ON VERTICAL STAB L/E COMPOSITE LOWER L/E.Dec 22, 2016 · N809SY · Boeing 7378Q8SDR DALA2016122810105Skin · delaminatedDURING WALK AROUND INSPECTION, FOUND AREA OF DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL LOCATED AT FSS 220 AND BL 1750. DELAMINATION IS OUT OF SRM LIMITS. REPAIRED IAW SRM 51-70-10, REP 4Dec 16, 2016 · N144DA · Boeing 767332SDR JR2R20161208318Skin · crackedDORSAL FIN CRACKED ON LH SIDE OF AIR INLET SCOOP ON PREVIOUS WELD REPAIR. REPAIRED DORSAL FIN AIR INLET SCOOP IAW MD80 SRM 55-05 FIG 3.Dec 8, 2016 · N869GA · Doug MD83SDR DALA2016120809683Skin · damagedVERTICAL STABILIZER LEADING EDGE HAD LOOSE FASTENERS ABOVE THE SPLICE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 55-03 PAR 27 FIG 29 (SHEET 1 AND 2).Dec 7, 2016 · N910DE · Doug MD88SDR FDEA201612024305Skin · dentedSIX INCH HORIZONTAL DENT ON THE RIGHT SIDE FOR THE VERTICAL STAB VSS 125. REPAIRED THE VERTICAL STAB IAW SRM 51-70-10-2R. PRIMED AND TOP COATED IAW SRM 51-70-10-2R AND AMM 51-21-10-7.Dec 2, 2016 · N783FD · Boeing 757222SDR DALA2016110908364Skin · damagedSEVERAL FASTENER HOLES OF THE VERTICAL STABILIZER LEADING EDGE STRUCTURE EXHIBIT EVIDENCE OF DISTRESS AT SPLICE STATION ZFS-52.267 IAW JC 5530-01048-01. REPAIRED IAW DRAWING SG95550001 AND WORK CARD 5530-01048-03.Nov 8, 2016 · N922AT · Boeing 717200SDR DALA2016110808341Skin · damagedELONGATED SCREW HOLE ABOVE SPLICE ZFS= 52 AT VERTICAL STABILIZER LE.Nov 7, 2016 · N902DE · Doug MD88SDR IPXA2016110710312Access Panel · damagedLOWER VERTICAL STAB RT SIDE ACCESS PANEL DAMAGED. REPAIRED IAW EO MD11 -5530-62238-C.Nov 6, 2016 · N287UP · Doug MD11FSDR DALA2016103008078Skin · looseFOUND 15 FASTENERS LOOSE AND COUNTERSINKS WORN OUT OF LIMITS, VERTICAL STABILIZER LEADING EDGE. COMPLIED WITH PRI/ERA 552194-14AD.Oct 26, 2016 · N950DN · Doug MD9030SDR DALA2016102307458Skin · damagedDISTRESS AT VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE. BHEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW DWG SG 95550001 REV.B, BUSHINGS WERE FABRICATED AND INSTALLED IAW DPS 4.710-3 AND DWG SG95550001 REV. B.Oct 22, 2016 · N967AT · Boeing 717200SDR DALA2016102307457Skin · damagedVERTICAL STAB LEADING EDGE AT VSS ZFS 52.267 SPLICE HAS NUMEROUS LOOSE SCREWS & SCREWS PULLING INTO SKIN & ELONGATED HOLES. REPAIRED THE VERTICAL STAB LEADING EDGE SKIN IAW DWG SR95550001 AND JC 5530-01048-03. FABRICATED NEW SPLICE BAN IAW ER/A 549632-14 ROct 22, 2016 · N987AT · Boeing 717200SDR FDEA201610193660Panel · delaminatedVERTICAL STAB RT SIDE PANEL HAS AREA OF DELAMINATION AT APPROX. BS 1786, FSS 170, 10 INCH AREA, EVALUATED DELAMINATION AND FOUND TO BE OUT OF LIMITS IAW SRM 55-30-01-1A FIG. 101 NOTE K. REMOVED AND REPLACED THE PANEL IAW-SRM-51-40- 02-0G AND DWG 175N2001 SHOct 19, 2016 · N799FD · Boeing 757222SDR DXTR2016100301Skin · gougedTHE VERTICAL STABILIZER SKIN HAS A GOUGE ON THE LH & RH SIDE WHERE THE REAR FAIRING ASSY CONTACTS THE VERTICAL STABILIZER. ACCOMPLISHED MINOR REPAIR IAW AQRD ERO-861733 DATED OCT 03/2016.Oct 3, 2016 · N218QS · Amd FALCON2000SDR JR2R20160930393Scoop · crackedVERTICAL STABILIZER RAM AIR SCOOP CRACKED. REPAIRED VERTICAL STABILIZER RAM AIR SCOOP IAW EA 40-2016-308.Sep 30, 2016 · N406NV · Doug MD83
Back to JASC 5532