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 JGVR20210302002Skin · corrodedONE AREA OF VERIFIED CORROSION ON VERTICAL STAB LH SKIN, NEAR TIP CAP. MECHANICALLY BLENDED ONE AREA OF CORROSION ON VERTICAL STAB LH SKIN, NEAR TIP CAP IAW CESSNA 680 SRM 51-70-02. PERFORMED NDT ON BLENDED AREA TO VERIFY CORROSION REMOVAL AND REMAINING MATERIMar 2, 2021 · N357QS · Cessna 680ASDR DALA2021012700515Panel · delaminatedDURING INSPECTION MAINTENANCE FOUND DELAMINTATION ON VERTICAL STAB RT FWD TORQUE BOX PANEL NR 175T2001. C/W ERA 589568-14.Jan 24, 2021 · N178DZ · Boeing 767332SDR DALA2022101606677Skin · damagedAIRCRAFT 9521, WHILE IN ATL FOR C-CHECK, MAINTENANCE WAS PERFORMING INSPECTIONS PER WORKCARD 5530-01048-02 AND FAA AD 2018-10-08 ON THE VERTICAL STABILIZER LEADING EDGE AT ZFS=52.267. DURING WORKCARD ACCOMPLISHMENT, MTC REPORTED CRACK INDICATIONS AT ONE EXISTIJan 22, 2021 · N988AT · Boeing 717200SDR A6WA202101257565Access Panel · crackedVERTICAL STABILIZER PANEL 326AL AFT END BENT AND 1 EA DENT. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND MEASURED 1 (EA) DENT ON VERTICAL STABILIZER PANEL 326AL, 0.700 L X 0.500 W X 0.007 D, DENT FOUND TO BE WITHIN LIMITS, REF CRJ200 SRM 55-00-31 AND A.W. SUJan 15, 2021 · N437AW · Cndair CL6002B19SDR IPXA2021011564471Skin · delaminatedINSPECTION TYPE: SEG DELAMINATION MARKED IN RED, .600" DIA CUTOUT, 20" FWD OF THE AFT EDGE AND 32" BELOW THE UPR EDGE OF PANEL. REPAIRED IAW B757 SRM 51-70-10-2R, 250 DEGREE, PER SRM 55-30-01-2R-5.Jan 15, 2021 · N414UP · Boeing 75724APFSDR IPXA2021011564470Skin · delaminatedINSPECTION TYPE: SEG DELAMINATION MARKED IN RED, .700" CUTOUT, 32" FWD OF THE AFT EDGE AND 52" ABOVE THE LOWER EDGE OF PANEL. REPAIRED IAW B757 SRM 51-70-10-2R, 250 DEGREE, PER SRM 55-30-01-2R-5.Jan 15, 2021 · N414UP · Boeing 75724APFSDR IPXA2021011564469Skin · delaminatedINSPECTION TYPE: SEG DELAMINATION MARKED IN RED .700" DIA CUTOUT, 7" FWD FROM THE AFT EDGE, AND 15.250" BELOW THE UPPER EDGE OF PANEL. REPAIRED IAW B757 SRM 51-70-10-2R, 250 DEGREE, PER SRM 55-30-01-2R-5.Jan 15, 2021 · N414UP · Boeing 75724APFSDR IXXA20210207301Skin · delaminatedVERTICAL STABILIZER LEFT SIDE SKIN PANEL WAS DELAMINATED BEYOND SRM LIMITS. REMOVED AND REPLACED CORE AND INNER SKIN AND REPAIRED PER AMES ENGINEERING DOCUMENT 47447REA02 REV IR AND APPROVED BY DERT-710167-SW ON 8110-3 DATED 1-19-21.Jan 14, 2021 · N331AZ · Boeing 767338SDR DALA2022052303520None · none(LOG 1697340) DURING SCHEDULED MAINENANCE FOUND TOOLING DAMAGE ON THE SECTION 48 BODY TO HORIZONTAL STAB SKIN FILLER AND UNDERLYING STRUCTURE. MAINTENANCE REPAIRED DAMAGE PER ERA 589149-14.Jan 6, 2021 · N371DA · Boeing 737832SDR SWIA202056352Skin · corrodedVERTICAL STABILIZER UPPER SKIN PLATE HAS FIVE FASTENERS AFT THAT HAVE RUSTED HEADS AND CORRODED TAILS. (C-CHECK) RO 2/17/2021. REMOVED AND REPLACED 5 EA FASTENERS ON THE VERTICAL STAB UPPER SKIN IAW CRJ 200 SRM 51-42-22.Dec 20, 2020 · N506CA · Cndair CL6002B19SDR SWIA202055631Skin · dentedVERTICAL STAB, RT SKIN HAS MULTIPLE DENTS. C-CHECK RO 1/28/2021. DISCREPANCY HAS A TYPOGRAPHICAL ERROR, SHOULD READ LT SIDE SKIN. REPAIRED SKIN MHIRJ REO 601R-55-31-368 REV-, DATED 12/29/2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED ADec 16, 2020 · N957SW · Cndair CL6002B19SDR DALA2020121104051Skin · crackedVERTICAL STAB ZFS 52.267 LT SKIN CRACK INDICATION. MAINTENANCE COMPLIED WITH ALL STEPS OF PRI 588955-14AD REV ORIG, 1, 2, 3, AND 4. COMPLIED WITH TIME LIMITED REPAIR SECTION 1 OR ER/A 588955-14AD REV ORIGINAL.Dec 10, 2020 · N997AT · Boeing 717200SDR FDEA202011243052Panel · dentedRT VERTICAL STABILIZER PANEL 175N2001 IS DAMAGED. DAMAGE IS 13.5" FROM L EDGE OF PANEL AND 15" FROM BOTTOM OF PANEL PLEASE EVA. REPAIRED SMALL PUNCTURE ON THE OUTER SKIN OF RT VERTICAL STAB PANEL P/N=175N2001, IAW SRM 55-30-01-2R REPAIR 5 AND SRM 51-70-10-2RNov 24, 2020 · N916FD · Boeing 75727BSDR DALA2020110603624Skin · crackedTHE FIRST BOLT HOLE ABOVE SKIN SPLICE AT STATION 2FS=52.267, HAS CRACK INDICATION IN VERT STAB LEADING EDGE LT SIDE, MARKED, REF AA 5530-01048 AND AD 2018-10-08. CRACK REPAIRED PER ERA 588486-14AD REV O (REF PRI 599486-14 REV 1) SEC 1. PERMANENT REPAIR.Nov 5, 2020 · N989AT · Boeing 717200SDR DALA2020110603623Skin · crackedWORKING PRI 588486-14. THE FIRST BOLT HOLE ABOVE SKIN SPLICE AT STATION 2FS=52.267, HAS CRACK INDICATION IN VERT STAB LEADING EDGE LT SIDE. MAINTENANCE COMPLETED PRI 588486-14 REV 1. PERMANENT REPAIR PERFORMED, PER ERA 588486-14AD REV "O".Nov 5, 2020 · N989AT · Boeing 717200SDR FDEA202011032760Panel · dentedVERTICAL STAB LEFT SIDE PANEL 322DL HAS DENT REPAIRED VERTICAL STABILIZER LEFT SIDE PANEL 322DL BY BONDING REPAIR PLIES, IAW B757 SRM 55-30-01-0I FIG 1 AND 55-30-01-2R REPAIR 4 FIG 201 AND 51-70-06 PARA 5 A FIGURE 5 AND REPAIR GENERAL. APPLIED FINISH, IAW B7Nov 3, 2020 · N784FD · Boeing 757222SDR DALA2020102603460Skin · crackedLT SIDE OF VERTICAL STAB LEADING EDGE HAS 3 CRACK INDICATIONS IN HOLES NR 2, 3, & 4 BELOW STA 2FS=52.267, REF AMDS CARD 5530-01048-02 STP 8, AA5530-01048 AD 2018-10-08. RE-EVALUATION OF FASTENER HOLES FOUND HOLES NR 3 & 4 WITH NO CRACK INDICATION. HOLE NR 2 Oct 25, 2020 · N997AT · Boeing 717200SDR DALA2020102603459Skin · crackedTHE RT SIDE OF VERTICAL STAB LEADING EDGE HAS A CRACK INDICATION IN HOLE NR 3 BELOW STA 2FS=52.267, REF AMDS CARD 5230-01048-02 STEP 8, AA 5530-01048 AD 2018-10-08. INSPECTED RT HORIZONTAL STAB HOLE NR 3. BHEC IAW CARD 5330-01048-02. CRACK INDICATION IS IN Oct 25, 2020 · N997AT · Boeing 717200SDR FDEA202010242768Doubler · corrodedLEFT HORIZONTAL LEADING EDGE INBOARD SECTION ALC7051-1-401 HAS EXTENSIVE CORROSION. INSIDE AND OUTSIDE SKIN IS SWOLLEN AROUND FASTENERS, MARKED NR 15 AND NR 16. FOUND CORROSION TO BE ON ACCESS PANEL DOUBLER P/N ALC7273-13. REPLACED DOUBLER AND INSTALLED NEOct 24, 2020 · N550FE · Doug MD1010FSDR CALA2020102901215Skin · delaminatedLT EXTERNAL BONDED SKIN BETWEEN AUX SPAR AND FRONT SPAR SKIN IS DELAMINATED AT FSS 270. GENERATED BY CARD 63-5530-1-2500, REF AMES ILN N/R 127305-0000-0449. REMOVED DAMAGE, PREPPED, AND REPAIRED DAMAGE AT MARKED LOCATION ON LT EXTERNAL BONDED SKIN ON VERTICAOct 23, 2020 · N670UA · Boeing 767322SDR CALA2020101901200Skin · dentedUPPER EMPENNAGE SKIN AFT OF RUDDER T/E HAS DENT(A3NB-05-3-6062).Oct 18, 2020 · N456UA · Airbus A320232SDR FDEA202010162532Skin · dentedRT RUDDER SKIN HAS A DENT BETWEEN RUDDER STA 231.852 AND 306.371 AND APPROXIMATELY 33" INCHES FROM THE TRAILING EDGE. MARKED REPAIRED DENT ON RT RUDDER SKIN, IAW B757 SRM 55-40-01-2R AND 51-70-03 PARA 5 L.Oct 16, 2020 · N798FD · Boeing 757222SDR DALA2020100903323Access Panel · damagedELONGATED HOLE ACCESS PANEL 326AT ON VERTICAL STABILIZER. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC ON ACCESS PANEL 326AT ON VERTICAL STABILIZER AS PER SRM.Oct 8, 2020 · N341NW · Airbus A320212SDR SWAA2020111025379Skin · wornWEAR ON EXTERNAL SKIN CLOSURE ANGLE AFT POSITION RT SIDE AT VERTICAL STABILIZER. REPAIRED CLOSURE ANGLE ON EXTERNAL SKIN AFT POSITION RT SIDE AT VERTICAL STABILIZER, IAW B737-700 53-80-71-2R-6 REPAIR 6 SRM SRM 51-40-02.Oct 7, 2020 · N931WN · Boeing 7377H4SDR SWAA2021081218332Skin · debondedWHILE PERFORMING TASK CARAD 712-00-21 POST DOCK INTERMEDIATE CHECK-GENERAL WALK AROUND SAFETY INSPECTION. FOUND AT VERTICAL FIN R/H MOST LOWERD FIN PANEL DEBONDED AND MISSING HARDWARE. (PANEL 324 ER) / FABRICATED NEW PANEL IAW BOEING DWG 175A1601 AND REINSTALLSep 23, 2020 · N720WN · Boeing 7377H4SDR FDEA202009142195Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON LEFT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASTSep 14, 2020 · N588FE · Doug MD11FSDR FDEA202008181922Skin · delaminatedVERTICAL LEADING EDGE DAMAGE REPAIR VERTICAL LEADING EDGE. MULTPLIE SPOTS OF COMPOSITE SEPARATED AND EXPOSED, 10 AREAS OF DAMAGE ON THE RT SIDE OF VERTICAL STAB, REPAIRED THE VERTICAL LEADING EDGE 10EA AREA IAW SRM 55-31-12-20-2, PARA 2.A, SRM 51-77-11, FIGAug 18, 2020 · N744FD · Airbus A300B4622RSDR FDEA2020072391582Access Panel · delaminatedVERTIAL STAB PANEL 325CR DELAMINATED ON THE CENTER OF TOP SURFACE. REPAIRED VERT STAB PANEL 325CR IAW EA 6-5530-T0354979-P1 STABILIZERS-V VERTICAL STABILIZER-TRAILING EDGE ACCESS PANEL 325CR DELAM.Jul 19, 2020 · N744FD · Airbus A300B4622RSDR IPXA2020072097952Panel · delaminatedINSPECTION TYPE:CCK, RT TORQUE BOX PANEL HAD TWO DELAMINATED DENTS ON THE LWR SKIN SURFACE OF PANEL. REPAIRED IAW SRM 51-70-10-2R, REPAIR 5, AND 2 IAW EO B757-5530-77182-A.Jul 19, 2020 · N440UP · Boeing 75724APFSDR 120B2020071300066Panel · delaminatedPANEL 324BL HAS A DELAMINATION SPOT ON THE INSIDE OF THE PANEL.Jul 13, 2020 · N36NE · Boeing 767323SDR UIEA2020070701480Access Panel · delaminatedVERT FIN LWR ACCESS PNL 322CL BACK SIDE HONEY CONE FOUND DELAM. PERFORMED METAL HOT BOND REPAIR AS PER "HX" RI NR RI-55-30-14113 REV A.Jul 4, 2020 · N489MC · Boeing 747412FSDR FDEA2020061091163Skin · crackedEMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL.Jun 9, 2020 · N617FE · Doug MD11FSDR FDEA2020061091162Skin · crackedEMPENNAGE ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID 72.0 CRACK FRAME REMOVED AND REPLACED AS PER EA 1-5500-T0354594 TITLE : STABILIZERS - GENERAL - PYLON CARRY THRU PANEL FRAME AJC 7593-51 ALJun 9, 2020 · N617FE · Doug MD11FSDR IPXA2020060155934Fairing · brokenINSPECTION TYPE SEG COMPOSITE DAMAGE AROUND UPPER FASTENER HOLES. DAMAGE FOUND TO BE OUT OF LIMITS, NOT REPAIRABLE. REPLACED FAIRING PANEL.May 30, 2020 · N171UP · Airbus A300F4622RSDR SWAA2021071579202Skin · corrodedVERTICAL STAB. CUTOUT FOR RUDDER BALANCE WEIGHT HORN HAS EXCESSIVE CORROSION ON LOWER WEB AND ASSOCIATED STRUCTURES. / REMOVED AND REPLACED VERTICAL STAB. CUTOUT FOR RUDDER BALANCE WEIGHT HORN LOWER WEB AND ASSOCIATED STRUCTURES PER SRM 51-40-02.May 11, 2020 · N258WN · Boeing 7377H4SDR UIEA2020050100929Skin · delaminatedRT SIDE VERTICAL STAB SKIN DELAMINATED.(<P>REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS PER 47401REA15.</P>)Apr 28, 2020 · N657GT · Boeing 767281SDR ABXR2020042400022Skin Panel · delaminatedRIGHT SIDE VERTICAL STAB SKIN DELAMINATED. REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS.Apr 24, 2020 · N659GT · Boeing 767281SDR JGVR20200410001Access Panel · crackedFOUND VERTICAL STABILIZER ACCESS PANEL 340FR CRACKED IN MULTIPLE SCREW DIMPLES, REPLACED WITH NEW CESSNA P/N 5531005-3.Apr 10, 2020 · N576QS · Cessna 560XLSDR MK1Y20200407012Skin Panel · delaminatedDURING MAINTENENCE FOUND MULTIPLE DELAMINATION DAMAGES ON INNER SKIN OF THE PANEL P/N 175T2001-4Apr 7, 2020 · N153DL · Boeing 7673P6SDR MK1Y20200407006Skin Panel · delaminatedDURING MAINTENENCE INSPECTION MULTIPLE DELAMINATION DAMAGES FOUND ON INNER SKIN OF LH PANEL P/N 175T2001-3Apr 7, 2020 · N153DL · Boeing 7673P6SDR SWAA2020040636093Skin · wornSUPPLEMENTAL INFORMATION: DORSAL FIN SEAL AT FWD TIP HAS WORN INFO FUSELAGE SKIN ON R/H SIDE. BLENDED DAMAGE REF SRM 53-00-01; PERFORMED NDT AND FOUND THICKNESS REMAINING (.033) OK FOR 10 REVENUE FLIGHT CYCLES REF ROW 44 SRM SUPPLEMENT ARM 90-7023-01 REV B. FRApr 6, 2020 · N209WN · Boeing 7377H4SDR UIEA2020040200595Angle · damagedVERT STAB-TIP FAIRING LWR WEB RH SIDE T ANGLE AND CHANNEL NUT FOUND DAMAGED(<P>VERTICAL FIN TIP RIB RH CHORD DAMAGED AREA REPAIRED IAW RI # RI-55-31-13974 REV A</P>)Apr 2, 2020 · N464MC · Boeing 747446SDR UIEA2020040200642Fairing · crackedVERT STAB FIN FAIRING #321A RH AFT EDGE FOUND CHAFING(<P>VERT STABILIZER L/E DOOR SEAL FIN FAIRING #321A SKIN CRACK AREAS (STA 2280) REPAIRED IAW RI-55-35-13975 REV A</P>)Apr 2, 2020 · N464MC · Boeing 747446SDR IPXA2020033053685Panel · delaminatedINSPECTION TYPE:N/ADELAM AND CUT OUT OF 4.5" X 2" AND 2" DIAMETER.REPAIRED PER EO MD11-5530-72242Mar 29, 2020 · N257UP · Doug MD11FSDR DALA2020040102110Skin · delaminatedLH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 92 TO STA 118 FOUND DELAMINATION. C/W SRM 51-70-10. (LP 1540351)Mar 27, 2020 · N827MH · Boeing 767432ERSDR DALA2020033102100Skin · delaminatedLH SIDE INTERNAL SKIN OF THE VERTICAL STABILIZER FOUND DELAMINATION AT FSS 170 TO FSS 220. 19 NICH AFT OF THE AUX FRONT SPAR. REPAIRED PER ERA 585841-14 (LP 1540344)Mar 27, 2020 · N825MH · Boeing 767432ERSDR DALA2020033102099Skin · delaminatedLH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 245 TO STA FSS 270 FOUND DELAMINATION. C/W ERA585841. (LP 1540341)Mar 27, 2020 · N825MH · Boeing 767432ERSDR DALA2020033102098Skin · delaminatedLH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 220 TO STA FSS 245 FOUND DELAMINATION. REPAIRED PER ERA 585841-14 (LP 1540339)Mar 27, 2020 · N825MH · Boeing 767432ERSDR SIMA202003254003Skin · crackedVERTICAL STAB., SKIN BEHIND SPAR 3, R/H LOWER PROFILE CRACKED. -C/A-VERTICAL STABILIZER, RH LOWER PROFILE BTW ZV1430 - ZV1932 REPAIRED IAW ETD 2020-145-010830.Mar 24, 2020 · N858AE · Emb EMB135KLSDR DALA2020042202290Skin Panel · delaminatedRIGHT SIDE VERTICAL STAB EXTERIOR SKIN PANEL IS DELAMINATED FSS 92.25. REPAIRED SKIN PER SRM 51-70-10. (LP 1549483)Mar 21, 2020 · N190DN · Boeing 767332
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