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.
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 DALA2018091305572Skin · crackedVERTICAL STAB SKIN CRACKED IN 5TH FASTENER HOLE BELOW ZFS52.267. COMPLIED WITH ER/A 536162-14AD REV B SEC IV.SDR DALA2018090405393Skin · crackedWHILE IN C CHECK, ACCOMPLISHING REPETITIVE INSPECTIONS PER AD 2011-15-01 AND SB MD8880-55A067, MTC FOUND A CRACK COMMON TO A HOLE COMMON TO THE DORSAL SKIN, BELOW THE SKIN SPLICE AND IN THE INTERNAL OEM DOUBLER( P/N 9911960-3)ONLY, LOCATED APPROXIMATELY 15 FASSDR DALA2018090105389Skin · crackedRT SIDE OF VERTICAL STABILIZER AT ZFS=52.267 IS CRACKED. REFERENCE AA 5530-01048 AND AD 2018-10-08. REPAIRED VERT STAB UPPER L/E SKIN/CRACK PER ER/A 571285-14 REV ORIG.SDR FDEA2018083102282Skin · crackedLOWER VERTICAL STABILIZER LT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341902 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA2018083102281Skin · crackedLOWER VERTICAL STABILIZER RT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341903 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FOTR20180806005Skin · dentedVERTICAL STABILZER RT SIDE SKIN WAS DENTED APPROXIMATELY 5 INCHES FROM L/E OF AUX SPAR AND VSS 230.SDR FOTR20180802002Skin Panel · dentedDENT FOUND ON VERTICAL STABILIZER RIGHT SURFACE 12"AFT OF AUX SPAR FSS 231.0.SDR DALA201808145058Skin · crackedMAINTENANCE FOUND A CRACK INDICATION COMMON TO THE 1ST FASTENER HOLE ON THE LT AND 2ND FASTENER HOLE ON THE RT BELOW THE ZFS 52.26 IN THE SKIN LAYER ONLY. REPAIRED IAW ER/A 520320-14AD, REV B.SDR SWAA2022021704915None · delaminatedDORSAL FIN IS DELAMINATED AT RIGHT HAND SIDE LOWER AFT CORNER. / REPAIRED DELAM AT RIGHT HAND SIDE LOWER AFT CORNER OF DORSAL FIN IAW SRM 55-30-01-2R-12 TABLE 202 + SRM 51-70-05-2R-6 80733U 08AUG18SDR NACA2018071800003Spar · corrodedCORROSION FOUND ON VERTICAL STABILIZER REAR SPAR RAIL LEFT HAND SIDE OF VERTICAL STABILIZER APPROXIMATELY AT BS1016 AND RS141.52. REPAIRED V-STAB SPAR RAIL, LT SIDE OF V-STAB APPROXIMATELY AT B STATION 1016 AND RUDDER STATION 141.52. IAW SR NUMBER 3-4159366135SDR SWAA2022022175314Panel · crackedVERTICAL STAB. L/H SIDE; PANEL #324AL RETAINER IS CRACKED / R&R VERTICAL STAB. L/H SIDE; PANEL #324AL RETAINER PER SRM 51-40-02SDR SWAA2022022175316Retainer · crackedVERTICAL STAB. L/H PANEL #323CL;; RETAINER IS CRACKED / R&R VERTICAL STAB. L/H PANEL #323CL;; RETAINER PER SRM 51-40-02SDR SWAA2022022175318Retainer · crackedVERTICAL STAB. R/H PANEL #323CR; RETAINER IS CRACKED / R&R VERTICAL STAB. R/H PANEL #323CR; RETAINER REF SRM 51-40-02.SDR SWAA2022022175321Retainer · crackedVERTICAL STAB. R/H SIDE; PANEL #324AR RETAINER IS CRACKED / R&R VERTICAL STAB. R/H SIDE; PANEL #324AR RETAINER REF SRM 51-40-02.SDR SWAA2022022175326Channel · crackedVERTICAL STAB. R/H PANEL #323CR; VERTICAL CHANNEL IS CRACKED / R&R VERTICAL STAB. R/H PANEL #323CR; VERTICAL CHANNEL PER SRM 51-40-02SDR SWAA2018071123362Panel · erodedVERTICAL STABILIZER LEADING EDGE FIBERGLASS PANEL ERODED. REPAIRED PANEL PER EA.SDR DALA2018062764227Skin · damagedDAMAGE FOUND ON THE DORSAL FIN SKIN, FWD OF ACCESS PANEL, AT FASTENER HOLES BY BSS 52. REMOVED THE DAMAGE AND REPAIRED IAW SRM 55-30-05, FIG 20, SHEET 3. AND APPLIED PROTECTIVE COATINGS.SDR DALA2018062524219Skin · damagedDAMAGE ON DORSAL FIN SKIN FWD OF ACCESS PANEL AT FASTENER HOLES BY STA 2FS-52. REMOVED NUT PLATE STRIP AND BACKING PLATE. TRIMMED DAMAGE PER MD 90 SRM 55-30-05. FABRICATED REPAIR DOUBLER FROM 7075-0.050, FILLER .040 7075-0 AND SPLICE .050 7075-0. INSTALLED REPSDR JGVR201806132004Access Panel · crackedFOUND VERTICAL STABILIZER ACCESS PANEL 340ER CRACKED, REPLACED THE ACCESS PANEL.SDR JGVR20180612001Access Panel · corrodedCORROSION FOUND UNDERNEATH THE ACCESS PANEL 340CR, LOWER AFT ON THE RT SIDE OF THE VERTICAL STAB. BLENDED THE CORROSION, CLEANED, CHEMICALLY TREATED, AND PRIMED AREAS IAW ENGINEERING MEMO.SDR DALA2018060873893Skin · crackedCRACK FOUND IN THE VERTICAL STABILIZER SKIN NEAR THE RAM AIR INLET AREA, LT SIDE, ZFS 9. THE SKIN WAS REPAIRED IAW ERA 569140-14, REV ORIGINAL, AND ETI-90-18-027, REV 2.SDR SIMA2018062260007Skin · dentedLEFT SIDE OF VERTICAL STABILIZER HAD A DENT, 8 INCHES ABOVE PANEL 325DL. REPAIRED THE SKIN IAW ERS-EM-55MR-682.SDR IPXA201805219798Panel · damagedLOWER VERTICAL STABILIZER RIGHT SIDE REAR PANEL DAMAGED. REPAIRED THE PANLE IAW EO MD11-5530-67901-B.SDR DALA2018051503331Skin · crackedVERTICAL STABILIZER 3EA LE ATTACH FASTENER HOLES INDICATE CRACK . RT SIDE, 6TH & 7TH HOLE BELOW SPLICE AND 8TH HOLE ABOVE SPLICE. COMPLIED WITH ERA 507874-14AD REV C, SECT IV, TIME LIMITED REPAIR INSTRUCTIONS.SDR DALA2018051303248Skin · wornWEAR WAS REPAIRED ON THE VERTICAL STABILIZER SKIN ZFS54.SDR DALA2018051503324Skin · damagedTHE LT AND RT VERTICAL STABILIZER EDGE STRUCTURE SPLICE BAND, HAD DEFORMED HOLES ON THE THIRD ROW OF FASTENERS. REAMED AND INSTALLED BUSHINGS IAW DRAWING SG95550001, REV B. INSTALLED AN EXTERNAL DOUBLER IAW DRAWING SG95550001, REV B.SDR IXXA20180604026Skin · delaminatedVERTICAL STAB DELAMINATED ON THE LT SIDE VSS 205.3. REPAIRED THE VERTICAL STAB IAW REA 47322REA 01, AND SRM 51-57-10. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE.SDR DALA2018051003283Access Panel · crackedCRACKED ACCESS PANEL 370AL ON THE VERTICAL STABILIZER. REPAIRED IAW SRM 55-00-00-2R-2, & SRM 51-41-02-0G.SDR DALA2018050403055Skin · damagedDURING FASTENER REMOVAL, HOLES WERE FOUND ELONGATED ON L/E AT VERTICAL STABILIZER JUST ABOVE RAM AIR INLET STA ZFS 17.66 APPROX VERTICAL STABILIZER LEADING EDGE SKIN AT ZFS=17.66 WAS REPAIRED PER ETI-88-18-046 REV 8 AND ER/A568315-14 REV ORIGINAL.SDR DALA2018051503013Skin · crackedCRACKED SKIN ON THE LEFT SIDE OF VERTICAL FIN, 3 INCHES IN LENGTH. REMOVED DAMAGE IAW SRM 55-30-05. FABRICATED A FILLER AND INSTALLED A DOUBLER IAW SRM 55-30-05.SDR 2018FA0000247Skin · crackedDURING A C CHECK, MAINTENANCE FOUND DAMAGE TO THE LT SIDE OF THE VERTICAL STABILIZER RUDDER 1 HINGE LINE CUTOUT, LOCATED 7 INCHES ABOVE ZV-2287. THE SKIN WAS FOUND TO BE CREASED WITH A DEPTH OF D=.250 AND A LENGTH OF L=1. MAINTENANCE REPAIRED DAMAGE TO THESDR COEA2018042322911Panel · chafedHEAVY CHECK COE/MAJOR REPAIR: PANEL 321AL, UPPER TRAILING EDGE CHAFFED. LEVEL 2, REPAIRED PER SRAS PCE-1693/18...12901 DATED 5/24/2018.SDR DALA2018041302499Skin · dentedVERTICAL STAB LEADING EDGE PANEL 322CL HAS 2 DIME SIZE DENTS AT FSS 200. REPAIRED IAW RE/A 556015-15, REV ORIGINAL, AND SRM.SDR DALA2018033102084Access Panel · damagedELONGATE HOLES ON ACCESS PANEL 370TL ON THE VERTICAL STABILIZER. THE ACCESS PANEL WAS REPAIRED IAW ER/A 567293-14, REV ORIGINAL, AND ETI-90-18-022, REV 1.SDR FDEA201803190731Skin · crackedVERTICAL STAB ACCESS PANEL 363ML CUTOUT FOUND TWO CRACKS, VSS 2154. REMOVED AND REPLACED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR IPXA2018040328140Panel · delaminatedINSPECTION TYPE: SEG3, WHILE PERFORMING TAP TEST IAW S55-610-100-2, FOUND THREE AREAS OF DELAMINATION ON THE RT VERTICAL STAB LOWER FWD TORQUE BOX PANEL. REMOVED AND REPLACED THE PANEL IAW SRM 51-40-02-OG, AND AMM 51-21-10.SDR 7C7A2018031500370Skin Panel · crackedCRACK AND CREASE DAMAGE TO THE VERTICAL STABILIZER LOWER FORWARD LT SKIN BETWEEN STRINGERS 20 - 22L AND BETWEEN THE FRONT SPAR AND FRAME 5. REPAIRED THE VERTICAL STABILIZER LOWER FORWARD LEFT SIDE SKIN IAW RD 8-55-3155, REVISION 1, AND ECO 008.55-18.03.SDR DALA2018031501711Skin · crackedAD 2016-09-05, AA 5530-01048: CRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER. REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.SDR ASOA201803097030Skin · crackedDURING A C CHECK, FOUND A CRACK ON THE LEFT TRAILING EDGE FLANGE OF THE VERTICAL STAB ABOVE THE PCU ACTUATORS. MAINNTENANCE INSTALLED A REPAIR TO THE AREA IAW EC/TC ETD2018-145-019454.SDR DALA2018030801475Skin · crackedCRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.SDR JR2R20180306134Angle · crackedLT UPPER BANANA PANEL IS CRACKED. REPLACED ANGLE IAW MD-80 SRM 51-30-2.SDR DALA2018022301090Skin · crackedCRACK INDICATION BELOW THE LEADING EDGE SKIN SPLICE AT ZFS=51.67, ZFS=50.17, ZFS=49.17 AND ZFS=48.17 OF THE LT VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE. REPAIRED IAW ETI-17-18-010, REV 1, DWG SG95550005 AND ER/A 566080-14AD, REV. ORIG.SDR DALA2018022201088Skin · damagedVERTICAL STAB RIGHT SIDE AT ZFS 52.267, UPPER L/E SEGMENT LOWER ROW OF FASTENER HOLES FROM L/E AFT HAVE DEFORMED HOLES. REPAIRED IAW ER/A 565657-14AD, REV O.SDR DALA2018022201087Skin · damagedVERTICAL STAB L/E LOWER ROW OF FASTENERS, RIGHT SIDE HAVE ELONGATED HOLES AND COUNTERSINKS, AT ZFS 52.267. REPAIRED IAW ERA 565657-14AD, REV O.SDR DALA2018022201086Skin · damagedRIGHT SIDE OF VERTICAL STAB AT XFS 52.267, RIGHT LOWER SEGMENT LOWER ROW OF FASTENERS, ELONGATED COUNTERSINKS. REPAIRED IAW ER/A 565657-14AD, REV O.SDR DALA2018022201085Skin · damagedRIGHT SIDE OF THE VERTICAL STAB, UPPER SEGMENT, UPPER ROW OF FASTENERS, COUNTERSINKS ELONGATED. REPAIRED IAW ERA 565657-14AD, REV O.SDR DALA2018022201084Skin · damagedL/E OF VERTICAL STAB, RIGHT SIDE LOWER SEGMENT, UPPER ROW OF FASTENERS COUNTERSINKS ELONGATED. REPAIR IAW ER/A 565657-14AD, REV O.SDR DALA2018022201065Skin Panel · crackedCRACK INDICATIONS IN L/E SKIN PANEL ATTACH HOLES BELOW SPLICE ZFS 52.267, RIGHT HAND SIDE. HOLE 6 TOP TO BOTTOM, MARKED. 5530-01048-01/010 00252: PRI 565466-14AD REV O-4 MATCHES ER/A 565466-14AD REV O STEPS 1-12. COMPLY WITH STEP 13 OF ER/A 565466-14AD REV O OSDR DALA2018022201064Skin · damagedLEFT HAND VERTICAL STAB L/E AT ZFS 52.267: LOWER 2EA ROWS FASTENERS HAVE ELONGATED HOLES AND COUNTERSINKS. REF: AA5530-01048 AND AD 2016-09-05. NRC 018-0001:5530-01048-01/001 00200: REPAIR COMPLIED WITH ON ER/A 565657-14AD REV O. ATTACHED TO NRC 254.SDR DALA2018022101059Skin · crackedCRACK IN VERTICAL STAB SKIN LT SIDE AFT OF SPAR CAP. NRC 018-0001:5530-01048-01/007 00234: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.
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