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"

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SDR DLM88090803Panel · crackedCRACK OF 1.000 INCH ON VERTICAL STAB OVER LT PANEL LOWER SECTION OF REMOVABLE L/E. CRACK WAS REPAIRED IAW ERA 473514-14 REV ORIG.Mar 20, 2009 · N905DL · Doug MD88SDR SWAA091626Skin · wornDURING SCHEDULED 8Y CHECK, FOUND L/E DORSAL FIN SKIN WORN BETWEEN BS 850 TO BS 853. REPAIRED DOUBLER PER SRM.Mar 11, 2009 · N401WN · Boeing 7377H4SDR IPXA09654908Skin · misrepairedINSPECTION TYPE:6C LT VERTICAL STABILIZER L/E FIXED PANEL THE EXISTING REPAIR PATCH NON - STANDARD REPAIR. METAL NOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.Mar 1, 2009 · N316UP · Boeing 767300SDR DLM88090591Skin · crackedCRACK ON UPPER SKIN DOUBLER AT VERTICAL STABILIZER. REPAIR WAS ACCOMPLISHED IAW ERA 473511-14 REV ORIG.Feb 27, 2009 · N977DL · Doug MD88SDR UHLA2009022300157Skin · crackedMAJOR REPAIR - RIGHT SIDE OF VERTICAL STAB BETWEEN RIBS 12-13 AND STRINGERS 8-9 EXTERIOR SKIN IS CRACKED APPROX 6 INCHES. REPAIRED CRACK AS REQUIRED IAW IC 2009-170/01478.Feb 23, 2009 · N644RW · Emb ERJ170100SESDR UPS09554575Skin · damagedINSPECTION TYPE:C3 WHILE PERFORMING EO B757-5100-30760 FOUND REPAIR ON UPPER SURFACE AT STAB STA 107-109, DOES NOT CONFORM TO 51-70-10. PROPERLY REPAIRED UPPER SURFACE OF STAB STA 107-109 SRM 51-70-10-22.Jan 22, 2009 · N417UP · Boeing 75724APFSDR IPXA09855338Doubler · dentedINSPECTION TYPE:SVC LEADING EDGE OF EXTERNAL DOUBLER REPAIR DENTED APPROX 2.75"H X 1.75"W STA ZFS 205.250. SURVEY SEQ 752-S4-02 (VERTICAL LEADING EDGE). REPLACED DAMAGED DOUBLER; FABRICATED NEW DOUBLER AND INSTALLED IAW DC8 SRM 55-2-1 FIG 4.Jan 15, 2009 · N752UP · Doug DC871FSDR UPS09654321Skin Panel · delaminatedINSPECTION TYPE:C EMP - VERTICAL STABILIZER PANEL 322CR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9.Dec 31, 2008 · N305UP · Boeing 76734AFSDR UPS09654318Panel · debondedINSPECTION TYPE:C EMP VERTICAL STABILIZER RT LOWER SURFACE PREVIOUS REPAIR AREA DEBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 4.Dec 30, 2008 · N305UP · Boeing 76734AFSDR UPS08554253Skin Panel · dentedINSPECTION TYPE:C D385560 LOWER VERTICAL STAB PANEL SKIN 175N2001-4 RT HAS SKIN DENT. REMOVED VERTICAL L/E PANEL 321BL TO FOM IAW MM 55-25-01-4. REMOVED DOUBLERS IAW SRM 51-70-10 PG 202 REPAIR 4 VERTICAL STA 172. SANDED AREA IAW SRM 51-70-10 PG 202 REPAIR 4Dec 28, 2008 · N410UP · Boeing 75724APFSDR DLM88081807Skin · damagedDAMAGED METALIZED COAT ON RUDDER. SURFACE SANDED IAW SRM 51-70-1AD PARA 23 A. (1). PLY OF GLASS FABRIC AND LAMINATE ASTROSTRIKE WERE INSTALLED IAW SRM 51-70-1AD PARA 23 A. (2)(3). RUDDER PAINTED IAW SRM 51-10-3B.Dec 10, 2008 · N974DL · Doug MD88SDR CALA2008121001136Skin · wornFUSELAGE UPPER SURFACE WHERE DORSAL FIN SEAL BLADE TOUCHES THE SKIN IS WORN. REPAIRED THE UPPER SKIN OF THE DORSAL PER ECRA 5331-01433.Dec 10, 2008 · N14652 · Boeing 737524SDR UPS08553995Skin Panel · delaminatedINSPECTION TYPE:C VERTICAL STAB LEADING EDGE PANEL 321BL DELAMINATED AT UPPER/INNER SURFACE. REMOVED DAMAGE, BONDED DOUBLERS, SEALED EDGES, PRIMED IAW SRM 51-70-10 F FIG 201 REPAIRS.Nov 18, 2008 · N414UP · Boeing 75724APFSDR AALA200810320Frame · crackedVERTICAL STABILIZER, LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER RIGHT SIDE ZFS 49.625. REPAIRED PER AARD 55-30-00-2.Nov 13, 2008 · N948TW · Doug DC983SDR 2008UALA06031Panel · crackedLEFT VERTICAL STAB PANEL 322AL HAS CRACK 13.5 INCHES LONG, 4.25 INCHES BELOW TOP OF PANEL AND 9 INCHES AFT OF CENTER LINE. REMOVED AND REPAIRED PANEL.Oct 7, 2008 · N814UA · Airbus A319131SDR DLM8K081240Skin · crackedVERTICAL STABILIZER LT IN SPAR SKIN, SKIN STRAP, FWD SPAR CHORD, AND FWD SPAR WEB FOUND CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIRS.Sep 26, 2008 · N912DE · Doug MD88SDR USAA920081319Skin · delaminatedBFM - MAJOR REPAIR - C3 CHECK - VERTICAL STABILIZER RT SIDE REAR SPAR WEB SKIN HAS DELAMINATION, VERTICAL STABILIZER STATION 150-175. REPAIRED VERTICAL STABILIZER RT SIDE REAR SPAR WEB SKIN, VERTICAL STABILIZER STATION 150-175 IAW B757 SRM 51-70-07. (S)Jun 30, 2008 · N925UW · Boeing 757225SDR USAA920081318Skin · crackedBFM - MAJOR REPAIR - C3 CHECK - VERTICAL STABILIZER RT SIDE REAR SPAR WEB EXTERNAL SKIN CRACKED, VERTICAL STABILIZER STATION 116.20. REPAIRED VERTICAL STABILIZER RT SIDE REAR SPAR WEB SKIN, VERTICAL STABILIZER STATION 116.20 IAW B757 SRM 51-70-06. (S)Jun 28, 2008 · N925UW · Boeing 757225SDR 08FDEA02470Panel · delaminatedTAIL DOCK VERTICAL STAB LT TOP PNL 9706 HAS DELAM ON PNL RADIUS IN CTR OF PNL. REPAIRED PANEL NR 9706 REF SRM 51-40-9 PAR 3, 4. "THIS IS CLASSIFIED AS A MINOR REPAIR."Jun 25, 2008 · N467FE · Boeing 727225SDR 08FDEA02414Skin · damagedDRILL START NEXT TO RIVET, UNDER PANEL 9702, VERTICAL STABILIZER UPPER SKIN, DEPTH OUT OF LIMITS. FOUND WHILE ACCOMPLISHING N/R N00752, FOUND DAMAGE TO BE OUT OF LIMITS. VERIFIED REPAIR MATERIAL TO 2024-T-3 .080". FABRICATED REPAIR DOUBLER AND INSTALLED DOUJun 24, 2008 · N467FE · Boeing 727225SDR ZZDA2008124Skin · crackedVERTICAL STAB RT SKIN CRACKED JUST BELOW HORIZONTAL STAB CUTOUT. COMPLIED WITH EA 17-55-01183A. MAJOR REPAIR, FORM 337 SUBMITTED.Jun 18, 2008 · N937AT · Boeing 717200SDR UPS08852635Skin · bulgedINSPECTION TYPE-C1 VERTICAL FIN, RT SIDE AFT OF ISOLATION STRIP HAS SKIN BULGING AND FASTENERS PULLING. REMOVED FASTENERS FOR ACCESS IAW SRM 51-01-21. NO CORROSION NOTED ON A REA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00, AND 51-01-21.Jun 15, 2008 · N700UP · Doug DC871FSDR NWAA082605514Skin · damagedDURING INSPECTION FOUND DAMAGE CAUSED TO VERTICAL STABILIZER RT LOWER LOWER SIDE SKIN PANEL. DAMAGE WAS CAUSED BY THE DEPARTURE OF RT WING TRAILING EDGE PANEL. REPAIRED PER EA 55-213280 SECT1 SECTION 2 REQUIRES REPETITIVE INSPECTIONS NOT TO EXCEED 24 MONTH IJun 2, 2008 · N514US · Boeing 757251SDR NWAA082615514Skin Panel · damagedDURING INSPECTION FOUND DAMAGE TO VERTICAL STABILIZER LT SIDE SKIN PANEL. REPAIRED PER EA 55-213388. (A)May 18, 2008 · N514US · Boeing 757251SDR 08FDEA01659Panel · unsecureVERTICAL STAB L/E PANEL 322 CL HOIST POINT IS NOT SECURED ON THE INTERIOR SIDE. REPAIRED CRACKED POTTING WITH NEW POTTING EC 3500 MB / A IAW DWG 33-A53373311 AMM 55-32-11 AND SRM 51-35-10 PG 17.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01658Panel · damagedVERTICAL STAB L/E PANEL 322 CL IS DAMAGED ON THE L/E 6 INCHES FROM THE LOWER END. REPAIRED ERROSION STRIP LOWER END ON VERTICAL LE PANEL 300 CL IAW AMM 55-32-11-8 & SRM 55-32-00.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01657Panel · debondedVERTICAL STAB L/E PANEL 322 CL IS DISBONDED AROUND THE HOIST POINT. REPAIRED VERTICAL SATBILIZER L / E PANEL 322 CL HOIST POINT AREA BY TRIMMING BURRS & RESEALING IAW AMM 55-32-11-8.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01656Panel · erodedVERTICAL STAB L/E PANEL 322 CL LEFT SIDE IS ERODED JUST AFT OF THE L/E. REMOVED ERRODED PAINT FOUND NO SIGNS OF DELAMINATION IAW SRM 55-32-00.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01655Panel · debondedVERTICAL STAB L/E PANEL 322 CL LEADING EDGE IS DISBONDED. REPAIRED ERROSION STRIP LOWER END OF THE VERTICAL L / E PANEL 322 CL IAW AMM 55-32-11-8.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01654Panel · damagedVERTICAL STAB L/E 322 AL HAD GOUGES ABOVE THE HOIST POINT ON THE LEFT AND RIGHT SIDES. REMOVED GOUGED PAINT AND REFINISHED AREA IAW SRM 55-32-00 & 51-75-10.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01653Panel · damagedVERTICAL STAB L/E 322 AL HAS DAMAGE. REPAIRED VERTICAL STABILIZER L/E PANEL 322 AL BY REMOVING & BONDING A NEW SECTION OF ERROSION STRIP IAW AMM 55-32-11-8.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01652Panel · erodedVERTICAL STAB L/E PANEL 322 AL HAS AREAS OF EROSION. REMOVED ERRODED PAINT AND REFINISHED AREA IAW SRM 55-32-00 & 51-75-10.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01651Panel · debondedVERTICAL STAB L/E PANEL 322 BL IS DISBONDING AROUND THE HOIST POINT AND THE UPPER LEFT CORNER. REMOVED AND REPLACED THE ERROSION STRIP IAW AMM 55-32-11-8 AND EA 6-5530-118505.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01650Panel · damagedVERTICAL STAB L/E PANEL 322 BL IS DAMAGED ON THE LEADING EDGE. REMOVED AND REPLACED THE ERROSION STRIP IAW AMM 55-32-11-8 AND E.A. 6-5530-118505.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR 08FDEA01649Panel · damagedVERTICAL STAB L/E PANEL 322 BL IS DAMAGED ON THE LEADING EDGE. REMOVED AND REPLACED THE ERROSION STRIP IAW AMM 55-32-11-8 AND E.A. 6-5530-118505.Apr 29, 2008 · N661FE · Airbus A300F4605RSDR HALA0800391Access Panel · damagedVERTICAL FIN ACCESS PANEL 324 CLX HAS BUBBLE ON PANEL. PERMANENT REPAIR CARRIED OUT IAW HAL B767-300 SRM 55-30-01/201 AND 51-70-17, 200F WET LAY UP HOT BOND REPAIR.Mar 10, 2008 · N594HA · Boeing 767332SDR 08FDEA00785Panel · brokenVERTICAL STABILIZER PANEL NR 325 CR IS BROKEN. REMOVED DAMAGE, VERIFIED MAT I.D. APPLIED REPAIR PLYS, CURED. RESTORED FINISH IAW SRM 55-33-13 & 51-77-00.Mar 7, 2008 · N425FE · Airbus A310203SDR 08FDEA00781Panel · puncturedVERTICAL STABILIZER PANEL NR 325 FL IS PUNCTURED. REPAIRED DAMAGED AREA BY APPLYING FIBERGLASS OVERLAYS IAW SRM 53-33-13 FIG 201 SECTION C-C. PAINTED REPAIR AREA ON THE PANEL IAW 51-75-10-08.Mar 7, 2008 · N425FE · Airbus A310203SDR 08FDEA00718Panel · delaminatedVERTICAL STABILIZER PANEL 325DL (ACTUATOR ACCESS PNL), FWD SECTION IS DELAMINATED. RESTORED FINISH PER SRM 51-75-10. REPAIRED BY REMOVING DAMAGE AND APPLYING A 250 DEGREE PREPREG LAYUP IAW SRM55-33-13.Mar 5, 2008 · N425FE · Airbus A310203SDR 08FDEA00707Panel · delaminatedVERTICAL STABILIZER PANEL 325CR IS DELAMINATED. REMOVED DAMAGE, VERIFIED MAT. I D APPLIED PLYS, CURED, RESTORED FINISH IAW 55-33-13 & 51-77-00.Mar 5, 2008 · N425FE · Airbus A310203SDR C2XA08ON094Skin · crackedFLT 7754 - LAX - WHILE PERFORMING ROUTING CHECK INSPECTION MX PERSONNEL FOUND A TEAR ON VERTICAL STAB SKIN 35MM FROM END OF SKIN AT ZV935.00MM TO RIVET ON LOWER PROFILE CHANNEL. ENGINEERING INFORMS A FLY BY FOR NEXT 500FC IS ACCEPTABLE PROVIDED: - THERE IS NOFeb 20, 2008 · N22909 · Emb EMB145XRSDR USAA920080294Panel · delaminatedBFM - MAJOR REPAIR - C4 CHECK - DELAMINATION ON VERTICAL STABILIZER RIGHT HAND SIDE FIXED PANEL, FSS 118-75 - FSS 192.25. REPLACED VERTICAL STABILIZER RIGHT HAND SIDE FIXED PANEL, FSS 118-75 - FSS 192.25 IAW B767 SRM 51-40-02.Jan 27, 2008 · N252AU · Boeing 7672B7ERSDR 2007UALA05389Skin · damagedVERTICAL FIN DAMAGED ON CONTACT WITH HANGAR DOOR. PERFORMED A MAJOR REPAIR.Dec 28, 2007 · N525UA · Boeing 757222SDR DXTA200702666Erosion Shield · looseEROSION TAPE CAME LOOSE FROM VERTICAL STAB AND WEDGED IN RUDDER. RUDDER ONLY MOVES ONE DIRECTION. REMOVED LOOSE EROSION TAPE FOUND IN VERTICAL STAB. AND PERFORMED RUDDER SYSTEM OPS CHECK, OPS CHECK NORMAL. WORK DONE IAW CESSNA 560 M/M CH 27-30-00.Dec 9, 2007 · N399QS · Cessna 560CESSNASDR 2007UALA05005Skin · delaminatedRIGHT SIDE OF THE VERTICAL STABILIZER IS DELAMINATED. BLISTER ON VERTICAL FIN BETWEEN STATIC PORTS RT PANEL REMOVED FOR REPAIR. SENT TO SHOP 273. R&R R30639. REINSTALLED PANEL. AC OK FOR SERVICE.Dec 5, 2007 · N791UA · Boeing 777222SDR C2XA07TY073Rivet · crackedTYS - DURING A CURRENT 3C INSPECTION THE RIGHT AFT FUSELAGE AT FR 76 WAS FOUND WITH SOME CRACKED RIVETS ON THE CONTOUR FLANGE OF THE VERTICAL STAB. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT FUSELAGE CONTOUR FLANGE DRAG ANGLE AT FR 76. ALL WORK WAS ACCOMDec 1, 2007 · N11121 · Emb EMB145XRSDR CA071115011Plate · cracked(CAN) CRACK INDICATION FOUND IN A CORROSION PIT IN THE AFT ATTACH PLATE WHEN INSPECTING IT IAW SB 454. (TC NR 20071115011)Nov 14, 2007 · Dhav DHC6300SDR USAA920071228Panel · delaminatedMCN - MAJOR REPAIR - C4 CHECK - DELAMINATION ON VERTICAL STABILIZER LEFT HAND SIDE, FSS 131.25. REPAIRED VERTICAL STABILIZER LEFT HAND SIDE, FSS 131.25 IAW B737 SRM 51-70-10.Nov 8, 2007 · N200UU · Boeing 7572B7SDR DHL2007785030Skin · bulgedVERTICAL STABILIZER RIGHT SIDE ABOVE UPPER RUDDER HAS BULGING SKIN (FIN WL 168 AT FIN STA 305). CUT OUT DAMAGE AREA AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW B-727 SRM 55-30-3 FIGURE 6 AND 55-30-2 FIGURE 1. TREATED AND PRIMED PARTS IAW B-727 SRM 51Oct 12, 2007 · N785AT · Boeing 727214SDR MWEA070239Access Panel · corrodedVERTICAL STABILIZER DORSAL FIN ACCESS PANEL LEADING EGDE OPENING HAS FRETTING CORROSION AT STATION 1437, STRINGER 1. REMOVED CORROSION. REMOVED AND REPLACED AFT FLANGE AT VERTICAL STABILIZER.Oct 5, 2007 · N814ME · Doug DC981
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