JASC 5532

Service difficulty reports · 1,753

Reports filed under 5532 · Vertical Stabilizer, Plate/Skin, newest first.

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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 07FDEA04038Panel · delaminatedVERTICAL STABILIZER LEADING EDGE PANEL 322CL WAS DELAMINATED. THE DIMENSION FOR REPAIR IAW SRM TO GREAT. REPAIR PERFORMED IAW SRM 55-32-00 FIG 203 AND FIG 216, APPROVED BY EA 6-5532-81077 AND RAS/DAHAM/4018735/2004.Sep 19, 2007 · N434FE · Airbus A310203SDR WGEA200700006Skin Panel · damagedVERTICAL STABILIZER LEADING EDGE PANEL HAS NUMEROUS DINGS THROUGH PAINT AND INTO COMPOSITE. REPAIRED VERTICAL STABILIZER LEADING EDGE IAW EA500 AMM 20-09-00 AND SRM 51-70-01. REFERENCE ECLIPSE AVIATION TECHNICAL SERVICE REGUEST FSR CASE 53-090507.Sep 8, 2007 · N109DJ · Eclips ECLIPSEEA500SDR 2007UALA03209Skin · damagedDORSAL FIN SKIN STA 860 PHENOLIC STRIP TORN AND POSSIBLE SKIN WEAR WHERE STRIP WAS TORN. REPAIRED AND INSTALLED DORSAL FIN.Aug 16, 2007 · N371UA · Boeing 737322SDR UPS07850589Skin · looseINSPECTION TYPE:C2 OUTER SKIN LOOSE AROUND COUNTERSINKS AT TOP OF VERTICAL STAB L/E LWR SECTION. REMOVED EXISTING FASTENERS AND FABRICATED AND INSTALLED REPAIR DOUBLER AT TOP OF VERT STAB L/E LWR SECTION IAW SRM 55-2-1 AND SRM 51-1-21.Aug 14, 2007 · N801UP · Doug DC873FSDR TRAX200701088Skin · corrodedCORROSION ON VERT STAB SKIN UNDER LT VOR ANTENNA. FOUND CORROSION TO BE WITHIN REPAIRABLE LIMITS IAW CRJ 200 SRM 55-00-31. REMOVED CORROSION IAW CRJ 200 SRM 51-21-06. SUPPLEMENTAL - SDR CLOSED 08/07/07.Jul 30, 2007 · N854AS · Cndair CL6002B19SDR UPS07550357Skin · gougedINSPECTION TYPE: C VERT STAB. UPPER MOST AFT PANEL SKIN GOUGED AS SEEN THRU PANEL 324EL. ACCOMPLISHED REPAIR AT VERT. STAB IAW EA NR 757-5530-27-A1720 AND UPS EO NR 57-55-20030.Jul 22, 2007 · N401UP · Boeing 75724APFSDR C2XA07TY031Spar · corrodedVERT STAB SPAR 1 INTERNAL SUPPORT BRACKET ON FRM 75 FRETTING. REMOVED FITTING AND BLENDED FITTING AND SKIN. FOUND TO BE WITHIN LIMITS. PERFORMED DYE PEN INSPECTION AND FOUND NO CRACKS. ALODINED, PRIMED, SEALED, INSTALLED FITTING AND APPLIED FILLET SEALANT Jun 22, 2007 · N14991 · Emb EMB145LRSDR UPS07550009Panel · debondedINSPECTION TYPE:C DEF: D352152 AND EO B757-5530-26995- DAMAGE TO VERTICAL STAB LOWER SIDE PANEL DISBONDED INNER & OUTER SKIN AT SAME LOCATION. ACCOMPLISHED LEFT VERTICAL PANEL REPAIR IAW FINAL EA 757-5530-27-A1685 AND UPS ENG FILE NUMBER 757-55-20029 WITH NO Jun 10, 2007 · N407UP · Boeing 75724APFSDR UPS07850119Skin · corrodedINSPECTION TYPE:C3 RIGHT SIDE OF VERTICAL STAB UPPER SKIN HAS 5 SHEARED FASTENERS AND POSSIBLE CORROSION UNDER SKIN. REMOVED PANEL NR 5647796-37 AND REMOVED CORROSION THAT WENT OUT OF LIMITS IAW SRM 51-03-00-0. REPLACED SKIN PANEL NR 5647796-37 IAW SRM 51-1-Jun 6, 2007 · N810UP · Doug DC873FSDR 2007UALA01558Tape · peelingSTRONG VIBRATION IN AFT GALLEY REPORTED BY FLT ATTENDANTS. STRONG ENOUGH TO VIBRATE ITEMS OFF COUNTER. SUPPLEMENTAL DATA UPDATE PERFORMED RUDDER FREEPLAY CHECK AND FOUND WITHIN LIMITS. FOUND EROSION PROTECTOVE TAPE PEELING FROM LEADING EDGE OF VERTICAL STABILMay 20, 2007 · N476UA · Airbus A320232SDR UPS07549871Skin · delaminatedINSPECTION TYPE:C VERTICAL STAB LEADING EDGE PANEL NR 321CL INNER SURFACE DELAMINATED (PANEL RACK). REMOVED DAMAGE, FABRICATED REPAIR PARTS FROM 2024-T3.016 BAT 1138598 PO MST0021331, PREPPED SURFACE AREAS & BONDED WITH BMS 5-101 PER FINAL EA 757-5530-27-A166May 7, 2007 · N404UP · Boeing 75724APFSDR 2007UALA01332Skin · damagedFIN STA 145, BETWEEN FWD AND AFT SPAR HAS DAMAGE. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIRS & DAMAGED SKIN SECTION. FABRICATED & INSTALLED EXTERNAL SKIN SPLICE REPAIR PLATES AT UPPER & LOWER ENDS OF NEW SKIN PANEL SECTION. DOUBLER IApr 29, 2007 · N367UA · Boeing 737322SDR UPS07549868Skin · delaminatedINSPECTION TYPE:C VERTICAL STAB RT SIDE SKIN PANEL P/N 175N2001-4 HAS DELAMINATION IN 2 PLACES, 41.0" X 19.0" OF DELAM 4.0" FROM TOP OF PNL, 7.0" FROM FWD EDGE. 10.0" X 5.0" OF DELAM 68" FROM TOP, 18" FROM FWD EDGE OF PANEL REF: D348458, PANEL P/N 175N2001. Apr 15, 2007 · N404UP · Boeing 75724APFSDR 07FDEA01457Panel · delaminatedDELAMINATION AT VERTICAL STABILIZER L/E PANEL NR 3. REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW. SRM 51-77-12 / FIG.211, APPROVED BY EA 6-5532-101302 AND RAS/DAHAM/4020826/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310SDR UPS07849745Skin · corrodedINSPECTION TYPE:C1 EVIDENCE OF CORROSION UNDER VERT STAB SKIN, RIGHT SIDE LARGE AREA OF PILLOWED SKIN WITH SEVERAL FAILED RIVETS. EXTERIOR ZR252-296 ALONG REAR SPAR. REMOVED AND REPLACED RIGHT VERT STAB SKIN IAW SRM 51-1-21, 51-1-20D, AND 51-3-0.Apr 10, 2007 · N819UP · Doug DC873FSDR COMA0760304Panel · warpedYAW MOTION NOTED DURING CLIMB, AUTOPILOT ON AND OFF. RETURNED TO CMH. FOUND THE RIGHT LOWER VISOR PANEL BOWED OUT, REPLACED THE VISOR PANEL.Apr 8, 2007 · N595SW · Cndair CL6002B19SDR TRAX200700491Skin · crackedVERTICAL L/E UPPER CORNER CRACKED ON RIGHT SIDE. CUT AWAY DAMAGED AREA (C/W STEPS 1AND 2) IAW REO 601R-55-32-165 CB7015474. SUPPLEMENTAL - SDR CLOSED 04/16/07.Apr 8, 2007 · N856AS · Cndair CL6002B19SDR 07FDEA01318Skin Panel · gougedRT VERTICAL STAB SKIN/WEB HAS (2 EA) TOOLING GOUGES LOCATED UNDER PANEL 9706. GOUGES ARE LOCATED NEAR FASTENER ROW FOR L- ANGLE AND 23", 24" FROM FRONT OF PANEL. REMOVED DAMAGE PER EA I070144. VERIFY DAMAGED REMOVED BY HFEC IAW 727 NDT MAN, PART 6, 51-00-00Apr 4, 2007 · N463FE · Boeing 727225SDR 07FDEA01209Panel · delaminatedVERTICAL STABILIZER PANEL 9511 IS DELAMINATED REMOVED DAMAGE AND REPAIRED PANEL, THEN APPLIED CONDUCTIVE COAT, PRIMED AND PAINTED REFERENCE SRM 51-40-09 PAGE 4, AND MM 51-21-121-7.Mar 30, 2007 · N463FE · Boeing 727225SDR 2007FA0000467Skin · damagedVERTICAL STABILIZER LEADING EDGE SKIN ATTACH RIVETS WORKING. FOUND THAT THE ORIGINAL UNIVERSAL HEAD RIVETS WERE REPLACED WITH FLUSH RIVETS. THE SKIN WAS COUNTERSUNK TO ACCOMMODATE THE RIVETS, HOWEVER THE SKIN WAS TOO THIN TO COUNTERSINK AND EVENTUALLY WORKEDMar 16, 2007 · N135YV · Beech 1900DSDR HAG07002Panel · crackedDURING INSPECTION, FOUND RT SIDE VERTICAL STABILIZER CENTER BULLET FAIRING PANEL CRACKED IN 5 LOCATIONS.Feb 22, 2007 · N451WM · Lear 45LEARSDR QXEA200603318Skin · damagedC3 - VERTICAL STAB LEFT SIDE OUTER SKIN HAS SCRATCH AT ACCESS PANEL 325EL, TOP EDGE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 51-25-01-001-001-A01.Dec 13, 2006 · N614QX · Cndair CL6002C10SDR 06FDEA04188Stringer · crackedLT VERTICAL STAB INTERIOR STRINGER 9L IS CRACKED AT INSPAR RIB CHORDS AT FIN STA 157.2. REMOVED DAMAGE AND REPAIRED REF SRM 51-40-4 FIGURE 3, PAGES 14-17. CLASSIFIED AS A MAJOR REPAIR ON WO 34160, SNRM NR N00685.Dec 7, 2006 · N244FE · Boeing 727277SDR QXEA200603112Skin · gougedC4 PDX - RIGHT SIDE VERTICAL STAB SKIN HAS A GOUGE AT LOWER FORWARD CORNER OF ACCESS PANEL 322GR. REPAIRED IAW SRM 51-20-11 AND RD8-55-1774.Nov 19, 2006 · N361PH · Dhav DHC8202SDR QXEA200603377Skin · gougedC4 PDX - RIGHT SIDE VERTICAL STAB SKIN HAS A GOUGE APPROXIMATELY 2" LONG AT LOWER FORWARD CORNER OF ACCESS PANEL 322GR OPENING. REPAIRED IAW RD 8-55-1774 AND SRM 51-20-11.Nov 18, 2006 · N361PH · Dhav DHC8202SDR ASAA0681177Skin · chafedVERTICAL STABILIZER LEFT SIDE SKIN IS CHAFED AT AFT END OF HORIZONTAL STABILIZER LOWER FAIRING. REPLACED DAMAGED SKIN PANEL PER SRM 51 10 4 AND 51 30 2.Nov 6, 2006 · N979AS · Doug DC983SDR ASAA0681176Skin · chafedVERTICAL STABILIZER RIGHT SIDE SKIN CHAFED AT AFT END OF HORIZONTAL STABILIZER LOWER FAIRING. REPLACED DAMAGED SKIN PANEL PER SRM 51 10 4 AND 51 30 2.Nov 6, 2006 · N979AS · Doug DC983SDR 20060023Skin · crackedDURING HEAVY MAINTENANCE INSPECTION A CRACK WAS FOUND ON THE RT VERTICAL STABILIZER SKIN. THE CRACK IS 7.5 INCH LONG AND IS 4.5 INCH FROM THE REAR SPAR RIVET LINE.Oct 19, 2006 · N822MD · Emb ERJ170100SDR QXEA200602694Skin · damagedC4 YYC - VERTICAL STAB RIGHT SKIN HAS A 2" SCRATCH IN IT, RIB 8 BETWEEN MID SPAR AND AFT SPAR. REPAIRED IAW RD8-55-1758.Oct 4, 2006 · N360PH · Dhav DHC8202SDR C1HA200697005Shear Tie · corrodedVERT STAB NR 3 TENSION TIE MOUNT HOLE PITTED. REAMED HOLE TO REMOVE PITTING IAW B727 CHAMPION AIR M/M 55-30-61 FIG 604 AND INSTALLED A FASTENER HOLE REPAIR IAW EO- 727- 5531-02.Sep 25, 2006 · N697CA · Boeing 727270SDR C1HA200697004Tension Tie · corrodedVERT STAB TENSION TIE AFT END CORRODED. REMOVED AND REPLACED VERT STAB TENSION TIE IAW B727 MM 55-10-01 AND MM 55-30-51.Sep 25, 2006 · N697CA · Boeing 727270SDR 2006FA0000989Panel · crackedDURING MAINTENANCE, DISCOVERED PANEL HAD 6 INCHES LONG CRACK RUNNING VERTICAL AT FWD ATTACH HOLES. PANEL WAS REPLACED. (K)Sep 22, 2006 · N10J · Lear 45LEARSDR QXEA200602515Skin · tool damageC4 YYC - VERTICAL STABILIZER LEADING EDGE REBATE ON STABILIZER RIGHT HAS SEVERAL TOOLING MARKS. REPAIRED IAW RD8-53-584.Sep 5, 2006 · N357PH · Dhav DHC8202SDR ASAA0640723Skin · gougedLT UPPER VERTICAL STAB HAS A GOUGE 2.5 FEET LONG AT BSTA 220 LEADING EDGE. REPAIRED VERTICAL STAB PER EA 5530 01142.Jun 29, 2006 · N709AS · Boeing 737490SDR 2006UALA01264Skin · dentedLT STAB HAS A DENT AT THE LEADING EDGE. MEASURED DENT 3 INCHES LONG,1.5 INCHES ACROSS. [06-29-07] MAJOR REPAIR: INSTALLED LEADING EDGE FLUSH DOUBLER.Jun 27, 2006 · N941UA · Boeing 737522SDR HALA0600480Skin · lightning strikeWHILE WORKING TAIL 5033 DISCOVERED FIN LEADING EDGE PANEL 326A HAS LIGHTING STRIKE DAMAGE AT LEADING EDGE 7" FROM TIP. REMOVED AND REPLACED FIN LEADING EDGE PANEL 326A REF, SOPM 20-50-01.Jun 21, 2006 · N594HA · Boeing 767300SDR 06FDEA2004Skin · damagedFOUND DRILL STARTS IN VERTICAL STAB SKIN AT TOP 2 HOLES THROUGH STAB SKIN BEHIND RT FWD LOWER SLIDE SEAL TRACK. REPAIRED STAB SKIN PER SRM 55-30-3 FIG 2.May 24, 2006 · N493FE · Boeing 727227SDR TAMF20060030SSkin Panel · delaminatedDURING C CHECK INSPECTION FOUND A DELAMINATION ON LT VERTICAL STABILIZER SKIN PANEL, STA FSS 170.259 - 195.390. DELAMINATED PANEL PN: 175T2001-3 WAS REMOVED IAW SRM 51-40-02 PAGE 1 AND SENT TO REPAIR. PANEL WAS REPAIRED AND INSTALLED IAW BOEING MESSAGE NUMBEMay 23, 2006 · N768QT · Boeing 767200SDR DU4R2006479Skin · crackedVERTICAL STAB LT SIDE HAS A CRACK IN L/E SKIN AT LT SIDE OF APU INLET, NEXT TO ACCESS COVER. STOP DRILLED CRACK IAW DC-9/MD-80 SRM 55-05 FIG 3. FABRICATED AND INSTALLED REPAIR DOUBLER 3-3/8" BY 3-1/2" FROM 2024-T3 .063 IAW DC-9/MD-80 SRM 51-10-3 AND 55-05 FIMay 17, 2006 · N923DL · Doug MD88SDR QXEA200602219Skin · scratchedPDX: VERTICAL STAB LT EXTERNAL SKIN SURFACE HAS A SCRATCH ADJACNET TO ACCESS HOLE REBATE FOR PANEL 322EL. MAINTENANCE REPAIRED IAW Q400 SRM TASK 51-14-00-350-803 AND SRM 51-25-10-370-801.May 9, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602218Skin · scratchedPDX: VERTICAL STAB LT EXTERNAL SKIN SURFACE HAS A SCRATCH ADJACENT TO ACCESS OPENING REBATE FOR PANEL 322CL. MAINTENANCE REPAIRED IAW Q400 SRM TASK 51-14-00-350-803.May 9, 2006 · N424QX · Bombdr DHC8402SDR CA060421030Skin · dented(CAN) SKIN HAS A DENT IN VERTICAL STAB RT SIDE 12 INCHES AFT OF UPPER END AND REPAIRED IAW CUSTOMER EA. (TC NR 20060421030)Apr 21, 2006 · Boeing 737290CSDR USAA060584Panel · delaminatedAPPROX FIN STA 133.10 (FWD LOWER LT VERT TAB) DELAMINATED. REMOVED DELAMINATED PORTION, FABRICATED CORE, INNER SKIN AND SPLICE DOUBLER & INSTALLED PER EA 97589, DEFECT SIZE: 34" X 15" OUTER SKIN & 58" X 15" INNER SKIN.Apr 11, 2006 · N630AU · Boeing 7572B7SDR CA060402001Skin · crackedTRAILING EDGE SKIN, RT SIDE CRACKED APPROX 1 INCH AT MAIN SPAR STATION. CRACK STARTS AT ONE JO BOLT FASTENER LOCATION AND GOES DOWN TO EDGE OF SKIN. MOST OF THE CRACK WAS HIDDEN BY THE LOWER RIGHT STABILIZER ATTACH/FAIRING ANGLE P/N 97-440025-14.Mar 27, 2006 · Beech 100BEECHSDR QXEA200600898Skin · bentPDX: H-STAB RT ELEVEATOR TRAILING EDGE BENT/DAMAGE AT STA YH-130.4. MAINTENANCE REPAIRED IAW HORIZON EA 6-55-133, RD 8/4-55-251, NDTM PART 6, 51-00-02 AND Q400 SRM 51-25-05-370-801.Mar 17, 2006 · N407QX · Bombdr DHC8402SDR ASAA0610253Skin · dentedDENT IN THE VERTICAL STAB RIGHT SIDE 12 INCHES AFT OF UPPER DORSAL FIN. REPAIRED PER ASA EA 5530 01139 AND CASCADE AREOSPACE ERO 5492.Mar 11, 2006 · N742AS · Boeing 737290CSDR QXEA200600593Skin · damagedPDX: LT SIDE OF VERTICAL STAB SKIN LEADING EDGE IS BENT BETWEEN RIBS 10 AND 7. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02-250-801 AND HORIZON EA 6-55-109.Feb 15, 2006 · N417QX · Bombdr DHC8402SDR UPS06846156Skin · corrodedINSPECTION TYPE:C1 INTERGRANULAR CORROSION 2 1/2" BY 2 1/2" AREA WHERE LWR VERT STAB L/E AND MIDDLE VERT L/E MATE. REMOVED CORROSION IAW SRM 55-02-00-0, CUT OUT AREA IAW SRM 55-02-01. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55--2-01-0 FIG 4 AND SJan 31, 2006 · N814UP · Doug DC873FSDR 06FDEA0421Skin · crackedVERTICAL FIN SKIN HAS POSSIBLE CRACK LT SIDE STR 10 ABOVE BODY TORQUE BOX BS 1342. REPAIRED CRACK AT BS 1342 STR 10 PER FED EX EA 7-5540-96829.Jan 29, 2006 · N490FE · Boeing 727200SDR USAA060151Skin · erodedLWR END OF VERT STAB L/E. SANDED AND REPAIRED AREA WITH COMPOSITE REPAIR, DEFECT SIZE: 6 INCHES X 3 INCHES.Jan 27, 2006 · N784AU · Boeing 7374B7
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