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 WX0A070920Skin Panel · gougedVERTICAL STAB UPPER AFT FAIRING CHAFED AND GOUGED ON LEFT SIDE. REMOVED, FABRICATED AND INSTALLED NEW SKIN PANEL IAW EA 14482 REV 1R DATED 3 AUG 2011 AND MD80 SRM 51-10-4, 51-30-2.Aug 8, 2011 · N864GA · Doug MD83SDR WX0A070919Skin Panel · gougedVERTICAL STAB UPPER AFT FAIRING CHAFED AND GOUGED ON RIGHT AFT SIDE. REMOVED, FABRICATED AND INSTALLED SKIN PANEL IAW EA 14483 REV 1R DATED 3 AUG 2011, MD80 SRM 51-30-2, 51-10-4.Aug 8, 2011 · N864GA · Doug MD83SDR USAA2011081200007Access Panel · delaminated2S CHECK - DELAMINATION ON ACCESS PANEL 325AL LEFT ON VERTICAL STABILIZER. REPLACED ACCESS PANEL 325AL LEFT ON VERTICAL STABILIZER IAW A319 SRM 53-55-11 & 51-72-11.Aug 2, 2011 · N722US · Airbus A319112SDR USAA2011081100009Access Panel · delaminated2S CHECK - DELAMINATION ON ACCESS PANEL 325AR RIGHT ON VERTICAL STABILIZER. REPLACED ACCESS PANEL 325AR RIGHT ON VERTICAL STABILIZER IAW A319 SRM 53-55-11 & 51-72-11.Aug 2, 2011 · N722US · Airbus A319112SDR DALA1146329872Fairing · damagedPER ERA 495027, REPAIR MUST BE COMPLETED ON THE VERTICAL STABILIZER UPPER TIP FAIRING ON THE LHS. ACCOMPLISH SECTION I TEMPORARY REPAIR PRIOR TO FLIGHT FROM DAY. ACCOMPLISH SECTION II PERMANENT REPAIR NTE THE ONE CYCLE MAINTENANCE FERRY FLIGHT FROM DAY TO ATLAug 2, 2011 · N781NC · Doug DC951SDR DALA1143999017Plate · crackedDURING PSV VISIT IN MSP FOUND CRACK ON VERTICAL LEADING EDGE ZFS26.8 LEFT SIDE FWD OF CUTOUT. REMOVED DAMAGE INSTALLED FILLER AND DOUBLER PER MD-88 SRM 53-01 FIG 4. WORKED ON N/R 101.Jul 19, 2011 · N917DE · Doug MD88SDR DALA1147739016Skin · damagedEA 09-470871 REV D ME04. ELONGATED HOLES ON VERTICAL STABILIZER FIXED LEADING EDGE STA ZFS=52.267. BUSHING REPAIRS INSTALLED IAW MD88 SG09550004 REV A.Jul 12, 2011 · N916DE · Doug MD88SDR USAA2011081900007Doubler · damagedC4 CHECK - PART OF BONDED REPAIR DOUBLER MISSING ON LEFT SIDE OF VERTICAL STABILIZER AT FSS195. REPLACED REPAIR DOUBLER WITH NEW ON LEFT SIDE OF FORWARD LOWER TORQUE BOX PANEL ASSY FSS195 IAW EA141709 & EA141711.Jul 11, 2011 · N203UW · Boeing 75723NSDR DALA1142510943Panel · damagedVERTICAL STABILIZER LEADING EDGE PANEL FASTENER HOLES WERE FOUND DAMAGED AND REPAIRED PER DC9/MD-80 SRM 53-03D FIG 30.Jul 5, 2011 · N943DL · Doug MD88SDR USAA2011070700007Skin · debondedC3 CHECK - DISBONDED INNER SKIN ON VERTICAL STAB, RIGHT FORWARD LOWER PANEL ASSEMBLY BETWEEN FSS149.765 TO FSS162.890. REPAIRED INNER SKIN ON VERTICAL STAB, RIGHT FORWARD LOWER PANEL ASSEMBLY BETWEEN FSS149.765 TO FSS162.890 IAW EA 130616.Jun 30, 2011 · N935UW · Boeing 7572B7SDR DALA1140209008Skin · wornFOUND THE VERTICAL STAB L/E UPPER REMOVAL PANEL RT SKIN WITH MULTIPLE WORN HOLES ALONG THE LOWER L/E ISSUED ERA 493753-14 REV ORG DATED 06/19/2011.Jun 19, 2011 · N908DE · Doug MD88SDR AALA20110613TUL03Skin · damagedVERTICAL LEADING EDGE HAS ELONGATED HOLE. INSTALLED DOUBLER PER 55-30-00.Jun 13, 2011 · N969TW · Doug DC983SDR DALA1138809880Skin · wornRT SIDE VERTICAL STABILIZER LEADING EDGE TIP SKIN HAS A DEEP WEAR AREA APPROX 22 INCH LONG, CAUSED BY BANANA FAIRING. BLENDED AREA REF SRM 55-01 FIG 1. LOWER BLEND FOUND OUT OF LIMITS & WAS TRIMMED OUT. A REPAIR DOUBLER MADE AND INSTALLED. REF COMPLIED ER/Jun 9, 2011 · N675MC · Doug DC951SDR DALA1139510993Skin · damagedVERTICAL STAB REMOVABLE L/E HOLES COMMON TO LOWER SPLICE - HOLES / COUNTERSINKS WORN. REPAIRED PER ER/A 493465-14 REV ORIG ON NRC 95.Jun 6, 2011 · N993DL · Doug MD88SDR IPXA1M67045Skin · dentedLOWER VERTICAL STAB LT SIDE REAR CTR PANEL DAMAGED. REPAIRED IAW EO MD11-5430-41892-B.Jun 6, 2011 · N293UP · Doug MD11FSDR FDEA201105302029Panel · debonded1EA DISBONDED AREA (2" X 3") WAS FOUND AT 321AL PANEL R/H SIDE. ( 14" FROM LEADING EDGE AND 20" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DISBONDED AREA 3"X2.5". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH REFER TO A310 SRM 55-May 30, 2011 · N429FE · Airbus A310203SDR FDEA201105302027Panel · debonded1EA DISBONDED AREA (2.5" X 1.8") WAS FOUND AT 322BL PANEL L/H SIDE. (6" FROM LEADING EDGE, 27" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DIMENSION OF THE DISBONDED AREA 9" X 8.5". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH REFMay 30, 2011 · N429FE · Airbus A310203SDR USAA2011053100019Panel · debondedCLT - RON - DEBONDED FIXED PANEL ON LEADING EDGE OF RIGHT OF VERTICAL STABILIZER BETWEEN FSS 0 TO FSS 119.46. REPLACED FIXED PANEL ON LEADING EDGE OF RIGHT OF VERTICAL STABILIZER BETWEEN FSS 0 TO FSS 119.46 IAW B757 AMM 06-42-00-201.May 29, 2011 · N906AW · Boeing 7572S7SDR DALA1137199866Skin · chafedVERTICAL STAB LT SKIN CHAFED AFT OF LEADING EDGE. REMOVED AND REPLACED LT SKIN PN H5912130-71 PO 1130960 IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5 P-243.May 29, 2011 · N775NC · Doug DC951SDR ASAA11410037Skin · dentedVERTICAL STAB L/E HAS A DENT WITH SCRIBE LINE LOCATED 7 FT FROM TOP OF VERTICAL STAB L/E FIN STA 231 231. REPAIRED DAMAGED AREA IAW B737 400 SRM 55 30 01.May 27, 2011 · N768AS · Boeing 737490SDR IPXA11667148Panel · delaminatedINSPECTION TYPE:8C, VERTICAL STAB LT FSS 11.787 TO 92.250 FIXED PANEL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 50.May 27, 2011 · N310UP · Boeing 76734AFSDR USAA2011052600004Panel · debondedDISBONDING ON LEFT SIDE OF VERTICAL STABILIZER. NOTE: A SUPPLEMENT WILL BE SUBMITTED UPON COMPLETION OF REPAIR.May 24, 2011 · N906AW · Boeing 7572S7SDR FDEA201105201898Skin · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LWR PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REV 46. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.May 20, 2011 · N589FE · Doug MD11FSDR DALA1144750929Panel · damagedVERTICAL STAB LOWER FIXED LEADING EDGE PANEL, UPPER EDGE ZFS 52 HOLE DAMAGE. REPAIRED IAW ERA 481558-14.May 18, 2011 · N929DL · Doug MD88SDR DALA1144810929Panel · damagedVERTICAL STAB LEADING EDGE UPPER REMOVABLE PANEL UPPER AND LOWER EDGE HOLE DAMAGE. REPAIRED IAW ERA 481683-14.May 16, 2011 · N929DL · Doug MD88SDR WX0A070845Skin Panel · chafedVERT STAB CHAFE ON LT LOWER BANANA PANEL AREA AFT END. VERT STAB LT SIDE LOWER SKIN PANEL REPAIRED IAW EA 14379 REV I/R.May 13, 2011 · N875GA · Doug MD83SDR WX0A070843Skin · chafedVERTICAL STAB TIP FAIRING CHAFED ON RT AFT SIDE OUT OF LIMITS. REMOVED & REPLACED FAIRING SKIN IAW EA 14380 REV I/R DATED 06/MAY/2011.May 12, 2011 · N875GA · Doug MD83SDR P5CA2011051100044Skin · damagedFASTENER HOLE ON VERTICAL STABILIZER LEADING EDGE SKIN AT STATION 473 & NBSP; FOUND TO BE ELONGATED. PERMANENT REPAIR ACCOMPLISHED IAW EI T2011A55B-1158.May 11, 2011 · N450PA · Boeing 74746NFSDR A6WA201140476Skin · corrodedLT LOWER 9 OF VERTICAL L/E HAS MINOR CORROSION AT THE MATING SURFACE BLENDED OUT MINOR CORROSION TO A SMOOTH FINISH IAW SRM 51-12-00.May 4, 2011 · N460AW · Cndair CL6002B19SDR DALA1134739007Skin · damagedHOLES/COUNTERSINKS WORN FIXED L/E, V/S HOLES COMMON TO SPLICE WITH REM L/EApr 28, 2011 · N907DE · Doug MD88SDR DALA1127760923Panel · looseDURING PSV "N" CHECK IN MSP, FOUND LOOSE FASTENERS IN VERT STAB L/E PANEL AT ZRS52.267. REPAIRED IAW ER/A 455844-14.Apr 22, 2011 · N923DL · Doug MD88SDR DALA1127640923Skin · crackedVERTICAL STAB LT DORSAL SIDE SKIN WAS FOUND CRACKED AT THE LOWER AFT CORNER OF THE RAM AIR INLET ACCESS DOOR CUTOUT. REPAIRED IAW ER/A 491888-14.Apr 21, 2011 · N923DL · Doug MD88SDR IPXA11666265Skin · misrepairedINSPECTION TYPE:C, LT VERTICAL STABILIZER LOWER PANEL EXTERNAL AREA (NON-STANDARD REPAIR). METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 3, REV 59.Apr 11, 2011 · N582UP · Boeing 7474R7FSDR IPXA11665996Panel · delaminatedVERTICAL STAB PANEL DELAMINATED, AREA MEASURING 11.5 BY 6.5" 18" FROM FWD EDG E PF PANEL AND 39" UP FROM THE BOTTOM. REPAIRED REF EO B767-5530-41998-B.Apr 10, 2011 · N317UP · Boeing 76734AFSDR FDEA201104061341Panel · crackedVERTICAL STABILIZER LT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REVISION 46 AND SRM 51-33-01 REVISION 46. OPS TEST OF THE ENG IGNITION/FADEC MODE SWITCH AND ADVISORY LIGHTS CARRIED OUT AS PER AMMApr 6, 2011 · N616FE · Doug MD11FSDR FDEA201104061340Panel · crackedVERTICAL STABILIZER RT CTR SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REVISION 46 AND SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 6, 2011 · N616FE · Doug MD11FSDR DALA1122050976Skin Panel · damagedWHILE IN LTR CK IN ATL MULTIPLE HOLES LOCATIONS WERE FOUND DAMAGED ON LT & RT EDGES OF VERTICAL STAB L/E UPPER REMOVABLE PANEL SKIN, 26 DAMAGED HOLES ON RT & 59 DAMAGED HOLES ON THE LT SIDE.Mar 27, 2011 · N976DL · Doug MD88SDR DALA1118799212Fastener · looseSCREWS ARE LOOSE ON L/E OF VERTICAL STAB. REPAIRED PER EA 02-470871-12 REV A ME-05.Mar 15, 2011 · N912DN · Doug MD9030SDR IPXA1665754Skin · delaminatedINSPECTION TYPE:C, EMP - LT VERT STAB AUX SPAR TO FRONT SPAR FIXED PNL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 3, REV.49. REF RS R55-31-36990, REV A AND EO B767-5530-41990-A.Mar 14, 2011 · N319UP · Boeing 76734AFSDR IPXA11M64913Finger Doubler · corrodedINSP TYPE:3C, VERTICAL STAB PANEL, 373HL CORROSSION AT FASTENER HOLE. BLENDED OUT VERT STAB PANEL 373HL AND FOUND OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED REF EO MD11-5530-41592-A AND STA, SA, EA 011-5530-01-A2911.Feb 8, 2011 · N287UP · Doug MD11FSDR IPXA11B65554Panel · misrepairedINSPECTION TYPE:C, CLARIFY THE EXISTING REPAIR CONFIGURATION ON VERTICAL STAB LT LWR AREA CORRELATE TO SRM REPAIR SURVEY SEQ NR 583-S4-01. VERT STAB LT LWR AREA REF SURVEY SEQ 583-S4-01 METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR4 FIG201 SHT3Feb 2, 2011 · N583UP · Boeing 7474R7FSDR REXA201100066Fairing · damagedDAMAGE WAS FOUND ON THE RIGHT VERTICAL STABILIZER LOWER VISOR FAIRING (P/N 600-21134-44). DAMAGE CONSISTS OF A TEAR OFF THE AFT TIP WHERE THE FAIRING ATTACHES TO THE RUB STRIP. TEMPORARY REPAIR IAW STS ENGINEERING EA 9-2011-20. WITHIN 100 FLIGHT HOURS, ACCOJan 26, 2011 · N8505Q · Cndair CL6002B19SDR UIEA2011011700127Skin · scratchedFOUND SCRATCH MARK (APPROX 1.5") ON VERTICAL STABILIZER LEADING EDGE CAP AT LE STA 135.581, BLENDING CARRIED OUT ON SCRATCH MARKS ON ABOVE SAID LOCATION. FOUND OUT OF LIMIT AS PER SRM 55-30-01. FIG 1 DETAIL I. DEPTH FOUND IS 0.018" L/E CAP REMOVED FOR S/M REPAJan 17, 2011 · N355MC · Boeing 747341SDR DALA1103730629Skin · debondedHORIZONTAL STAB HAS DISBONDED CORE AND INNER SKIN. FOUND IN INSP ON 01/16/11. REPAIRED IAW ERA NR489056-14, REV ORG.Jan 16, 2011 · N629DL · Boeing 757232SDR COEA2011011109805Skin Panel · damagedHEAVY CK COE / MAJOR REPAIR: RT VERTICAL SKIN AT VOR ANTENNA LOCATION HAD DAMAGE TO SKIN AND BAD NUT PLATES. MAJOR REPAIR PER ATR SRI.Jan 11, 2011 · N805FX · Aerosp ATR72212SDR COEA2011011108805Skin Panel · damagedHEAVY CK COE / MAJOR REPAIR: LT VERTICAL SKIN AT VOR ANTENNA LOCATON HAS DAMAGE TO SKIN AND BAD NUT PLATES. MAJOR REPAIR PER ATR SRI.Jan 11, 2011 · N805FX · Aerosp ATR72212SDR DALA1102060124Skin · dentedLT V-STAB EXTERIOR AROUND FS STA 270.784 FOUND DENT DURING HMV INSP AT SIN; C/A-DENTED SURFACE TRIMMED OFF. REPAIR PART FABRICATED IAW SRM 51-70-01, FIG 201, OT IS REPAIR PARTS BONDS IAW SRM 51-71-10.Jan 10, 2011 · N124DE · Boeing 767332SDR DALA1102346903Skin · delaminatedTHE VERTICLE STAB SKIN WAS DELAMINATED. THE PANNEL WAS REMOVED AND ROUTED TO SHOP 382. THE PANEL WAS REPAIRED IAW ERA 488591-14 REV B ON 01/12/11. THE PANEL WAS COMPLETED.Jan 5, 2011 · N757AT · Boeing 757212SDR DALA1103610961Skin Panel · crackedHORIZ STAB REAR SPAR UPPER CAP AFT SKIN INSP EA 09-460214-12, REV D, ME07, ME13, ME14 SPLICED LT UPPER SKIN PANEL ON HORIZ STAB.Jan 3, 2011 · N961DL · Doug MD88SDR DALA1103166903Skin · delaminatedDELAMINATION FOUND ON LT SIDE OF VERTICAL STABILIZER TIME LIMITED REPAIR DONE IAW ERA 488591-14, REV 0. A PERMANENT REPAIR DONE BY COMPOSITE SHOP ON NR 001 IAW ERA 488591-14, REV B.Jan 2, 2011 · N757AT · Boeing 757212
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