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 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.SDR 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.SDR 2007UALA03209Skin · damagedDORSAL FIN SKIN STA 860 PHENOLIC STRIP TORN AND POSSIBLE SKIN WEAR WHERE STRIP WAS TORN. REPAIRED AND INSTALLED DORSAL FIN.SDR 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.SDR 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.SDR 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.SDR 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 SDR 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 SDR 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-SDR 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 STABILSDR 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-A166SDR 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 ISDR 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. SDR 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).SDR 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.SDR 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.SDR 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.SDR 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, 51-00-00SDR 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.SDR 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 WORKEDSDR HAG07002Panel · crackedDURING INSPECTION, FOUND RT SIDE VERTICAL STABILIZER CENTER BULLET FAIRING PANEL CRACKED IN 5 LOCATIONS.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 2006FA0000989Panel · crackedDURING MAINTENANCE, DISCOVERED PANEL HAD 6 INCHES LONG CRACK RUNNING VERTICAL AT FWD ATTACH HOLES. PANEL WAS REPLACED. (K)SDR QXEA200602515Skin · tool damageC4 YYC - VERTICAL STABILIZER LEADING EDGE REBATE ON STABILIZER RIGHT HAS SEVERAL TOOLING MARKS. REPAIRED IAW RD8-53-584.SDR ASAA0640723Skin · gougedLT UPPER VERTICAL STAB HAS A GOUGE 2.5 FEET LONG AT BSTA 220 LEADING EDGE. REPAIRED VERTICAL STAB PER EA 5530 01142.SDR 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.SDR 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.SDR 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.SDR 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 NUMBESDR 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 FISDR 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.SDR 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.SDR 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)SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SSDR 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.SDR USAA060151Skin · erodedLWR END OF VERT STAB L/E. SANDED AND REPAIRED AREA WITH COMPOSITE REPAIR, DEFECT SIZE: 6 INCHES X 3 INCHES.
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