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 WX0A071570Skin · gougedRIGHT VERTICAL STAB UPPER TIP FAIRING SKIN GOUGED. REMOVED SKIN, FABRICATED NEW SKIN AND INSTALLED.Apr 23, 2013 · N418NV · Doug DC983SDR SWAA2013042615242Skin Panel · crackedDORSAL FIN L/E PANEL CRACKED ON LEFT SIDE OF PANEL. REMOVED AND REPLACED PANEL IAW SRM.Apr 14, 2013 · N950AT · Boeing 717200SDR DALA1309056802Skin · dentedLT SIDE VERTICAL STAB DENTED 18 INCHES. REMOVED DAMAGE AND PREPARED AREA FOR REPAIR IAW SRM 51-70-10. INSTALLED REPAIR IAW SRM 51-70-10 942294 RESTORED FINISH IAW MM 51-21.Apr 11, 2013 · N703TW · Boeing 7572Q8SDR DALA13016340907Skin · corrodedVERTICAL STAB DORSAL FIN FASTENER HOLE HA CORROSION 25.5" FROM L/E 7.5" DOWN FROM STA ZFS 52.267. ON INVESTIGATION FOUND FASTENER HOLE 25.5" FROM L/E 7.5" DOWN FROM STA. ZFS 52.267 TO HAVE DRILL START IN COUNTERSINK AND NOT TO BE CORROSION. REPAIRED DAMAGED Apr 10, 2013 · N907DL · Doug MD88SDR FDEA201303290687Skin · failedTWO MISDRILLED HOLES AT VERTICAL STAB LT PANEL 322DL ATTACHMENT. COMPLIED WITH EA F-5530-TO300208. MAJOR REPAIR.Mar 29, 2013 · N938FD · Boeing 75723ASDR Y2PA20130306006Skin · chafedEVIDENCE OF DAMAGE ON UPPER RT SIDE OF VERTICAL STABILIZER BETWEEN STATION ZV120 NEAR FORWARD END OF UPPER AND LOWER BODY FAIRINGS, DISCOVERED DURING C-CHECK. MX REPAIRED IAW DWG 55301301-1 AND APPROVED 8110-3 DATED 02/19/13.Mar 6, 2013 · N205US · Doug DC932FSDR C77A20130502000Skin · damagedDURING A POST FLIGHT WALK AROUND, ACFT WAS REPORTED TO HAVE A HOLE IN THE VERTICAL STABILIZER. THE DAMAGE CONSISTS OF A CRACK WHICH IS 8.75" LONG AND A HOLE IN THE LOWER THIRD OF THE CRACK WHICH MEASURES APPROXIMATELY 1.75" IN DIAMETER. THIS DAMAGE IS OUT Feb 25, 2013 · N627CZ · Emb ERJ170200LRSDR SWAA2013022112974Skin · crackedLTW MDDR 22313T STABILIZER DORSAL FIN CRACKED AT FASTENER HOLE. REF EA 17-55-0370 41R. CUT OUT DAMAGED SECTION OF VERTICAL STABILIZER DORSAL FIN SKIN, FAB AND INSTALLED REPAIR DOUBLER AND FILLER IAW B-717 SRM 55-30-01 REPAIR 5 51-41-01, 51- 40-08, 51-10-04 5Feb 20, 2013 · N948AT · Boeing 717200SDR DALA13008619015Skin · damagedSKIN DAMAGED VERTICAL STAB, APPROX ZFS=52-62. ACCOMPLISHED REPAIR IAW ER/A 511535-14AD, REV O.Feb 15, 2013 · N915DE · Doug MD88SDR ASOA20130215078VSkin · corrodedDURING C-CHECK LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN CORROSION (LOCAL LEVEL 2) AROUND RIVETS. MX PERFORMED REPAIR AND REMOVED CORROSION (LOCAL LEVEL 2) FROM LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN AROUND RIVETS IAW EC5530-01116 REV F. Feb 15, 2013 · N14991 · Emb EMB145LRSDR ASOA2013021577Skin · corrodedDURING C-CHECK RT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN CORROSION (LOCAL LEVEL 2) AROUND RIVETS. MX PERFORMED REPAIR AND REMOVED CORROSION ON RT HORIZ STABILIZER L/E IAW EC5530-01116, REV F. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 15, 2013 · N14991 · Emb EMB145LRSDR SWAA2013022112978Skin · crackedSTABILIZER DORSAL FIN CRACKED AT AFT FASTENER HOLE. REF EA 17-55-037041R. CUT OUT DAMAGED SECTION OF VERTICAL STABILIZER DORSAL FIN SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B717 SRM 55-30*-01 REPAIR 5, 51-41-01, 51-40-08, 51-10-04, 51-20-Feb 12, 2013 · N948AT · Boeing 717200SDR FDEA201302080302Panel · crackedLOWER VERTICAL STABILIZER, NR 2 ENGINE INTAKE DUCT, REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED IAW SRM 55-30-02 REPAIR 2 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Feb 8, 2013 · N524FE · Doug MD11FSDR DALA13006889204Skin · corrodedVERTICAL TIP FORWARD END, RT SIDE FRAME FOR SKIN PANEL CORRODED. WORK ACCOMPLISHED ON ER/A 510927-14, REV O.Feb 8, 2013 · N904DA · Doug MD9030SDR UIEA2013021900098Skin · damagedVERT FIN L/E FAIRING 321H M/D AREA SKIN FOUND DENT AND DAMAGED. (VERT FIN L/E FAIRING 321H, PN 174U11 MID AREA SKIN DENT AREAS REPAIRED IAW R8. R1-55-33-10148).Feb 4, 2013 · N476MC · Boeing 74747UFSDR DALA13004589206Skin · crackedFUSELAGE SKIN OTBD OF LT VERTICAL STABILIZER SKATE ANGLE CRACKED. TRIMMED OUT AND HFEC FOR CONTAINMENT. REPAIRED SG09530003-7009 AND ER/A 510732-14. RII C/W QC1984.Jan 25, 2013 · N906DA · Doug MD9030SDR DALA13004579206Skin · crackedFUSELAGE SKIN OTBD OF RIGHT VERTICAL STABILIZER SKATE ANGLE CRACKED. CRACKS TRIMMED OUT, HFEC INSPECTED FOR CONTAINMENT. REPAIRED IAW SG09530003-7011 AND ER/A 510725-14.Jan 25, 2013 · N906DA · Doug MD9030SDR AALA20130121005Skin · corrodedCORROSION WAS FOUND ON THE CENTER STABILIZER BOX LOWER OUTER SKIN AT THE AFT SPAR AT APPROXIAMTELY RIGHT BUTTLINE 12. INSTALLED EXTERNAL DOUBLER PER EA B767-55-027803.Jan 21, 2013 · N7375A · Boeing 767323SDR FDEA201301080037Panel · crackedLOWER VERTICAL STABILIZER, NR 2 ENGINE INTAKE DUCT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED.Jan 8, 2013 · N614FE · Doug MD11FSDR UALA2012121207184Panel · delaminatedVERTICAL STAB, LEFT SIDE, ON PANEL 322DL, 2 FT AFT OF LOWER GUST SUPPRESSION STATIC PORT, FOUND 5 INCH CIRCULAR AREA OF DELAMINATION. INSTALLED PANEL 322DL PER MM.Dec 10, 2012 · N796UA · Boeing 777222SDR FDEA201212064255Skin · damagedACFT HAS BEEN INVOLVED IN AN ACFT STRIKE, THE RT SIDE OF THE VERTICAL STABILIZER HAS SUSTAINED DAMAGE. INITIAL INSPECTION SHOWS NUMEROUS RIBS AND STIFFENERS BROKEN INTERNAL TO VERTICAL FIN. ALSO, HAS DAMAGED HYD LINES INTERNAL OF STAB, OUTER DAMAGE INCLUDES Dec 6, 2012 · N257FE · Boeing 727233SDR AALA20121129017Skin · damagedLOWER DORSAL LEADING EDGE REQUIRES DOUBLER AT STATION ZFS 52.267 DUE TO 9 HOLES BEING TO DEEP FOR REPAIR BUSHINGS. INSTALLED REPAIR DOUBLER PER SRM 55-03-00 PARAGRAPH 28.Nov 29, 2012 · N33502 · Doug DC982SDR ERAA2120110Skin Panel · dentedDENT FOUND ON RIGHT STATION FORWARD BOTTOM VERTICAL STAB SKIN PANEL P/N 85530011 BETWEEN THE FRONT SPAR AND MIDDLE SPAR AT STIFFENER 85530107-105 BETWEEN RIBS TWO AND THREE.Nov 29, 2012 · N882EA · Dhav DHC8103SDR CA121127005Skin · corroded(CAN) FOUND CORROSION ON THE VERTICAL STABILIZER LT AND RT EXTERNAL SKINS NEAR MULTIPLE SCREW HOLES OF THE RAM AIR INLET FAIRING. CONDITION REPORTED TO ACFT MFG.Nov 27, 2012 · Bombdr BD7001A11SDR USAA2012121000027Skin Panel · debondedC2 CHECK - AREA OF DISBONDING ON SKIN PANEL ON LOWER RIGHT SIDE OF VERTICAL STABILIZER TORQUE BOX BETWEEN FSS 150 TO FSS 180 & BETWEEN ASS 0 TO FSS 0. REPLACED SKIN PANEL ON LOWER RIGHT SIDE OF VERTICAL STABILIZER IAW B757 SRM 51-40-02.Nov 19, 2012 · N902AW · Boeing 7572S7SDR DALA12012540904Skin · looseVERTICAL STAB L/E SKIN LOOSE FASTENERS IN CENTER OF REPAIR. WHILE ACCOMPLISHING THE REPAIR TO THE SUBJECT VERTICAL STAB UPPER L/E, NINE (9) FASTENER HOLES COMMON TO THE THIRD ROW FROM THE LOWER EDGE WERE FOUND TO BE DAMAGED. COMPLIED WITH ERA 508630-14AD REVNov 9, 2012 · N904DL · Doug MD88SDR SWAA2012111909624Skin · wornDORSAL FIN ACCESS PANEL 9504 WORN. REMOVED AND REPLACED SKIN IAW SRM.Nov 6, 2012 · N608SW · Boeing 7373H4SDR SWAA2012111909623Skin · wornDORSAL FIN ACCESS PANEL 9503 WORN. REMOVED AND REPLACED SKIN IAW SRM.Nov 6, 2012 · N608SW · Boeing 7373H4SDR DALA14012036717Skin · damagedVERTICAL STAB SKIN FIXED PANEL HAS THREE LIGHTNING STRIKES AT UPPER END. VERTICAL STABILIZER FWD FIN TIP REMOVED IAW SRM 51-40-02, PG 10, PARA 9. HFEC HOLE INSPECTION IAW NDTM PT.6, 51-00-16, NO CRACKS NOTED AT OPEN HOLES. FASTENERS INSTALLED IAW SRM 51-40-Nov 2, 2012 · N67171 · Boeing 757232SDR UALA2012092405385Skin · delaminatedON WALK AROUND FOUND POSSIBLE DELAMINATION ON RIGHT SIDE OF VERT STAB. ITEM ROLLED FORWARD. REF IPC55-34-51-008, PANEL HAS 11 BY 8 AREA OF DELAM IN MIDDLE OF PANEL. REF SRM 55-30-01. NEED TO ACP INTERIM REPAIR PER ECRA 5530-01666 AVAILABLE ON EDOCS. ACCOSep 22, 2012 · N798UA · Boeing 777222SDR GLBA2012091700057Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE VERTICAL STAB RT SIDE AFT LWR SPAR SKIN 8.5" UP FROM BOTTOM, 3" IN LENGTH. REPAIRED IAW EO 12-1900-55-038. MAJOR REPAIR.Sep 17, 2012 · N261GL · Beech 1900DSDR IPXA2575047Skin · damagedVERTICAL STAB LT SIDE LOWER PANEL HAS SKIN DAMAGE. REPAIRED REF EO B757-5330-47810-A.Aug 27, 2012 · N440UP · Boeing 75724APFSDR UALA2012082304734Tape · peelingLEADING EDGE OF VERTICAL STAB HAS APPROX 4 INCHES OF MYLAR TAPE PEELING OFF OF UPPER PART OF HF ANTENNA. OK FOR SERVICE FOR MAX OF 5 CYCLES PER ECRA 5535-01009. MUST BE INSPECTED PRIOR TO EACH DEPARTURE FOR FURTHER DETERIORATION. ACCOMPLISH PERMANENT REPAIRAug 22, 2012 · N549UA · Boeing 757222SDR DALA1702920911Skin Panel · wornVERTICAL STABILIZER LEADING EDGE SKIN UPPER REMOVABLE PANEL LOWER EDGE WEAR DAMAGE 484644-14.Aug 10, 2012 · N911DL · Doug MD88SDR AALA20120809013Panel · damagedSEVERAL HOLES LOCATED ON THE LOWER DORSAL. INSTALLED DOUBLER REPAIR ON THE LOWER DORSAL PANEL BELOW STATION ZFS 52.267 PER BOEING MD-80 SRM 55-03-00.Aug 9, 2012 · N471AA · Doug DC982SDR DALA1244310927Skin · corrodedON DRILLING AND LOCATING NEW PANEL TO VERTICAL STABILIZER, SKIN FOUND WITH CORROSION ON MATING SURFACE. FABRICATED AND INSTALLED NEW MATING SURFACE IAW SRM 51-30-2.Jul 21, 2012 · N927DA · Doug MD88SDR IPXA2M74618Access Panel · damagedINSPECTION TYPE: 4C, FASTENER COUNTERSINK DOUBLE-DRILLED AT AFT CORNER OF VERTICAL STAB T/E ACCESS PANEL 374BL LT SIDE. REPAIRED LT UPPER VERTICAL STAB T/E AT ZFR 315 IAW STASA EA 011-5530-01-A4104 REV IR & EO MD11-5530-48022-A, FAA 8100-9.Jul 4, 2012 · N292UP · Doug MD11FSDR DALA1502130983Skin · damagedVERTICAL STAB FRONT SPAR AND SKINS DAMAGED. REPAIRED IAW AA 5530-01045.Jun 17, 2012 · N983DL · Doug MD88SDR DALA1235289204Skin · wornWHILE PERFORMING VERTICAL STABILIZER LEADING EDGE SKIN INSPECTION EA_JIC 02-470871-12AD REV C ME01,9 LEADING EDGE HOLES WERE FOUND WORN AND WRITTEN ON NR CARD 99, PER STEP 3 OF SAME EA JIC, ME05 WAS ISSUED. THE LEADING EDGE WAS REMOVED ON NR 107 AND REPAIRS WJun 1, 2012 · N904DA · Doug MD9030SDR FDEA201205231939Panel · crackedLOWER VERTICAL STAB RT REAR CENTER SPAR LOWER PANEL FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49 AND DWG AJC7582 REV H. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.May 23, 2012 · N575FE · Doug MD11FSDR IPXA12M73546Access Panel · dentedVERTICAL STAB, LEFT SIDE ACCESS PANEL 363CL DENTED AND DISBONDED. REPAIRED IAW EO MD11-5330-46915-B.May 14, 2012 · N250UP · Doug MD11FSDR IPXA12M73545Panel · dentedVERTICAL STAB LEFT SIDE PANEL 363CL DENTED AND DISBONDED. REPAIRED DENTS IAW EO MD11-5330-46915-B.May 14, 2012 · N250UP · Doug MD11FSDR DALA1230470931Skin · damagedDURING HMV, ELONGATED HOLES WERE FOUND ON VERTICAL STABILIZER LEADING EDGE SKIN STA ZFS=55.813. ELONGATED HOLES IN SHIN WERE REAMED AND BUSHINGS INSTALLED REF EA 09-470871-12AD REV G ME08.May 9, 2012 · N931DL · Doug MD88SDR AALA20120507020Skin · damagedLEFT SIDE FORWARD LOWER VERTICAL STAB PLANK HAS 48 HAIL DENTS. INSTALLED BMS 5-92 TYPE V ADHESIVE TO ALL DENTS IN AREA, ALLOWED CURE, SANDED SMOOTH TO AREA CONTOUR AND APPLIED EXTERNAL PRIMER COAT TO AFFECTED AREA PER SRM 51-70-01 AND EA B757-55-023268.May 7, 2012 · N653A · Boeing 757223SDR DALA1228840946Skin · damagedDURING INSPECTION PER EA 09-470871-12AD, A DAMAGED HOLE WAS FOUND ON THE RT LOWER AFT PORTION OF THE REMOVABLE LEADING EDGE SKIN. THE DAMAGED HOLE IS THE 11TH HOLE UP FROM ZFS=52. A TRIM OUT REPAIR FOR THIS HOLE LOCATION IS NOT ALLOWED PER SG09550004 REV. B.May 3, 2012 · N946DL · Doug MD88SDR FDEA201205031718Panel · crackedNR 2 ENGINE AIR INTAKE REAR CENTER SPAR LT LOWER PANEL FOUND WITH CRACK. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2 REVISION 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.May 3, 2012 · N607FE · Doug MD11FSDR FDEA201205031717Panel · crackedLOWER VERTICAL STABILIZER NR 2 ENGINE AIR INTAKE REAR CENTER SPAR RT LOWER PANEL FOUND WITH CRACK. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201 REPAIR 2, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 3, 2012 · N607FE · Doug MD11FSDR DALA1227520912Panel · wornDURING PSV VISIT IN MSP FOUND WORN FASTENER HOLES FOR VERTICAL L/E. BUSHED 16 HOLES AND FABRICATED DOUBLER FROM 7075-T6 .125". WORK ACCOMPLISHED PER DWG SG 09550004.Apr 30, 2012 · N912DL · Doug MD88SDR DALA1225280946Skin · damagedWHILE IN MSP FOR PSV AND DURING INSPECTION PER EA 09-470871-12AD A DAMAGED HOLE WAS FOUND ON THE RT LOWER AFT PORTION OF THE REMOVABLE LEADING EDGE SKIN. THE DAMAGED HOLE IS THE 11TH HOLE UP FROM ZFS=52. A TRIMOUT REPAIR FOR THIS HOLE LOCATION IS NOT ALLOWEDApr 20, 2012 · N946DL · Doug MD88SDR DALA1225119001Skin · damagedDURING PSV IN MSP, 2EA ELONGATED HOLES WERE FOUND ON THE LT SIDE OF THE VERTICAL STABILIZER LOWER FIXED SKIN JUST BELOW ZFS=52, COMMON TO LT SPAR CHORD. THE HOLES WILL BE OPENED IN THE FIXED L/E SKIN TO A MAX SIZE OF 0.327 DIA AND A BUSHING/DOUBLER REPAIR INSApr 19, 2012 · N901DE · Doug MD88
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