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 DALA2019051903114Skin · bulgedV-STAB LT SURFACE FOUND 01 EA BULGE AT 28" TO FRONT SPAR AND 92" TO FUSELAGE. REPAIRED (LP 1081328)May 19, 2019 · N845MH · Boeing 767432ERSDR DALA2019050702949Skin · delaminatedLEFT VERTICAL STAB EXTERIOR SKIN IS DELAMINATED APPROX FSS 92.25. REPAIRED PER E/RA 577568-00. (LP 1062595)May 6, 2019 · N844MH · Boeing 767432ERSDR SWAA2022030878293Panel · crackedPANEL ASSY #323CR VERTICAL FAN R/H FLANGE CRACKED MKD DOT 60-120 / REMOVED & REPLACED FLANGE AT PANEL # 323CR VERTICAL FAN R/H IAW B737-700 SRM 51-40-02-0G-0May 1, 2019 · N735SA · Boeing 7377H4SDR DALA2019043002765Skin · delaminatedLEFT VERTICAL STAB FRONT SPAR SKIN AT FSS 65.75 TO FSS 92.25 AREA FOUND DELAMINATION. REPAIRED PER SRM 55-30-01-2R-1 & SRM 51-70-10. (LP 1051761)Apr 29, 2019 · N192DN · Boeing 767332SDR DALA2019043002734Access Panel · crackedCRACK ACCESS PANEL 322AL BOTTOM POSITION RH AND LH SIDE, TOP POSITION RH SIDE VERTICAL STABILIZER (1 EA). REPAIRED ACCESS PANEL 322AL ON VERTICAL STABILIZER AS PER PRI 577104-14 REV O AND ER/A 577104-14 REV ORIGINAL.Apr 29, 2019 · N337NB · Airbus A319114SDR FDEA201904171097Skin Panel · dentedDENT ON VERTICAL STABILIZER RT SIDE ON LOWER FWD PANEL, REQUIRES REPAIR IAW SRM 55-30-01AS DENTS RESULT IN DELAM REPAIRED DENT IAW SRM 55-30-01-0I FIG 1 (SHEETS 2 AND 3) AND SRM 55-30-01-2R REPAIR 5 AND SRM 51-70-10-2R REPAIR 2.Apr 17, 2019 · N927FD · Boeing 757204SDR DALA2019041502443Skin · delaminatedR/H VERT STAB EXTERNAL SURFACE AT FSS 39.25 TO FSS 65.75 AREA FOUND DELAMINATION. REPAIRED PER ERA 577019-14. (LP 1022939)Apr 9, 2019 · N1201P · Boeing 767332SDR HALA2019040300162Skin · corrodedVERTICAL STAB TRAILING EDGE RHS #3 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. // REMOVAL OF CORROSION CARRIED OUT IAW HAL A330 SRM 51-74-00 REV 98.01. CORROSION STILL EVIDENT IAW HAL A330 NTM 51-10-02-221-001-A REV 96. BLEND DEPTH OF .054" IS BEYOND 5Apr 3, 2019 · N393HA · Airbus A330243SDR CA190401015Skin · corroded(CAN) DURING INSPECTION CORROSION FOUND ON SKIN PLATE AT AFT FRAME 67.5%.Mar 29, 2019 · Cndair CL6002B19SDR DALA2019032801990Fastener · looseAWR. IN REFERENCE AMDS 5530-01045-05 STEP 2 LOOSE FASTENERS WAS FOUND ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26. FASTENERS ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26 WERE REPLACED PER ETI-88-19-028 REV.2 AND ERA 576759-14AD REV. ORIGINAL. SECTMar 27, 2019 · N977DL · Doug MD88SDR DALA2019032901993Skin · damagedSTABILIZERS VERTICAL FIXED LE SKIN, ZFS. ELONGATED HOLES. DTA MONITOR INSPECTION LOG REFERENCE ER/A 576759-14AD SECTION II REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS PENDING A DAMAGE TOLERMar 26, 2019 · N977DL · Doug MD88SDR DALA2019032801982Cover · missingPDA PART DEPARTED AIRCRAFT. A/C 3140 CLOSED LOG 5827099 FLT/CHK 0657. ON WALK-AROUND FOUND VERTICAL STAB HOIST POINT COVER MISSING. INSTALLED HOIST POINT COVER.Mar 21, 2019 · N340NB · Airbus A319114SDR DALA2019031501691Skin · crackedTWO CRACKS ON VERTICAL STAB LEADING EDGE STA Y=1095.868 AND Y=1133 LT/RT SIDE. (EHB). NRC 00050: CRACKS (2EA) ON VERTICAL STAB LEADING EDGE STA Y=1095.868 AND Y=1133 LT/RT SIDE WERE REPAIRED PER SRM 55-30-01-2R-5 FIG 201 AND 202 REPAIR 5, 51-41-02-0G, AND 51-4Mar 14, 2019 · N928AT · Boeing 717200SDR DALA2019031001548Skin · crackedINITIAL INSPECTION: CRACK ON SKIN APROX STA 916 BELOW CUT OUT THROUGH ACCESS PANEL 630 1 A AT VERT. EST. SKIN APROX STA 916 BELOW CUT OUT THROUGH ACCESS PANEL 6301 A AT VERT. EST. WAS REPAIRED PER SRM 55-05 FIG.3. (LP0977861)Mar 10, 2019 · N916DL · Doug MD88SDR DALA2019030501469Skin · crackedINITIAL INSPECTION: CRACK ON RT EXTERIOR SKIN AT VERTICAL STABILIZER, PROYECTION STA Y= 1420 APPROX. CRACK ON RT EXTERIOR SKIN AT VERTICAL STABILIZER, PROYECTION STA Y= 1420 APPROX WAS REPAIRED PER ER/A 575990-14AD REV. ORIGINAL (SECTION I PERMANENT REPAIR ) AMar 4, 2019 · N976DL · Doug MD88SDR DALA2019022801406Skin · delaminatedSHIP 685 SKIN DELAMINATION FOUND ON LEFT SIDE OF VERTICAL STAB. CORRECTIVE ACTION: REMOVED DAMAGE, REPAIRED REF ERA 575782-14 REV ORG AND W/O. (5559477)Feb 27, 2019 · N685DA · Boeing 757232SDR DALA2019022801359Panel · delaminatedSHIP 685 WHILE UNDERGOING SERVICE, THE SUBJECT LT LOWER, FORWARD TORQUE BOX PANEL WAS FOUND TO HAVE A LARGE AREA OF DELAMINATION IN THE MIDDLE CORE BAY (BETWEEN FSS 119.467 & FSS 195.390). THE DELAMINATION COINCIDES WITH AN EXISTING REPAIR THAT WAS ACCOMPLISHEFeb 27, 2019 · N685DA · Boeing 757232SDR DALA2019021901030Access Panel · crackedFOUND 2 CRACKS ON INTERNAL WEB AT ACCESS PANEL ON LH SIDE OF RAM AIR INLET. REMOVED FASTENERS, VERIFIED CRACK TERMINATION AND CONTAINMENT. DAMAGE CONTAINED BY INSTALLATION OF REPAIR DOUBLERS. FABRICATED AND DRILLED 2 INTERNAL DOUBLERS (FROM .063 T6) PER SRM 55Feb 17, 2019 · N915DN · Doug MD9030SDR FDEA201902160430Skin Panel · crackedEMPENNAGE : UPON REMOVAL VERTICAL STABILIZER RIGHT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 FOUND CRACK. VERTICAL STABILIZER RIGHT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 SKIN PANEL CRACKFeb 16, 2019 · N608FE · Doug MD11FSDR FDEA201902160429Skin Panel · crackedEMPENNAGE : UPON REMOVAL VERTICAL STABILIZER LEFT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 FOUND CRACK. VERTICAL STABILIZER LEFT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 SKIN PANEL CRACKEDFeb 16, 2019 · N608FE · Doug MD11FSDR DALA2019022741248Skin · crackedREF AA 5530-01048 AND AD 2018-10-08RIGHT HAND SIDE VERTICAL STAB LEADING EDGE ATTACH (2EA) HOLES HAVE CRACK INDICATIONS, FIRST 2 HOLES ABOVE SPLIT LINE (MKD). NRC 075-0001:5530-01048-02/002 00226: PRI 575376-14 REV 0-1. CRACK WAS REPAIRED PER ER/A 575376-14 REFeb 13, 2019 · N993AT · Boeing 717200SDR DALA201902110881Skin · crackedCRACKS 2(E/A) ON VERTICAL STABILIZER SKIN STA ZFS= 23.500 APROX. (EHV) PERMANENT REPAIR SECTION I WAS PERFORMED ON VERTICAL STABILIZER SKIN STA ZFS= 23.500 APROX. PER ER/A 575288-14 REV. ORIGINAL AND ETI-90-19-04 REV. 2. REPETITIVE INSPECTION WILL BE PERFORMEDFeb 9, 2019 · N918DH · Doug MD9030SDR DALA201902110871Skin · crackedINITIAL INSPECTION: CRACK ON VERTICAL STABILIZER LEADINGEDGE SKIN RH SIDE STA ZFS 17.65. VERTICAL STABILIZER LEADINGEDGE SKIN RH SIDE STA ZFS 17.65 WAS REPAIRED PER ER/A 575282-14 REV. ORIG. AND ETI-88-19-008 REV.1. PERFORM GENERAL VISUAL INSPECTION EVERY "C" Feb 9, 2019 · N973DL · Doug MD88SDR DALA2019021190880Skin · crackedCRACKS ON VERTICAL STABILIZER SKIN STA ZFS=-26.8 APROX. BELOW LL RAM AIR PER ER/A 575309-14AD REV. ORIGINAL AND ETI-90-19-006 REV. ORIGINAL REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL CYCLES ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIREDFeb 8, 2019 · N918DH · Doug MD9030SDR 2019F00128Fairing · crackedBULLET FAIRING FLANGES CRACKED.Jan 28, 2019 · N997QS · Cessna 750SDR DALA2019012500513Skin · crackedINITIAL INSPECTION: CRACK ON SKIN OF VERTICAL STABILIZER NEAR TO ACCESS PANEL 6301B RT SIDE. SKIN OF VERTICAL STABILIZER NEAR TO ACCESS PANEL 6301B RT SIDE (EHV) WAS REPAIRED PER ER/A 574758-14AD REV. ORIGINAL (SECTION 1 PERMANENT REPAIR) AND ETI 88-19-004 REVJan 24, 2019 · N974DL · Doug MD88SDR DALA2019012300489Skin · crackedDURING REPLACEMENT OF RH ATTACH ANGLE WAS FOUND A CRACK ON VERTICAL STABILIZER SKIN STA ZFS= -26.8. VERTICAL STABILIZER SKIN STA ZFS= -26.8 WAS REPAIRED (PERMANENT REPAIR) PER ERA 574733-14AD REV ORIGINAL AND ETI-90-19-03 REV 1. REPAIR APPROVAL IS LIMITED TO 6Jan 22, 2019 · N919DN · Doug MD9030SDR DALA2019012000397Skin · damagedVERTICAL STABILIZER LEADING EDGE AT SPLICE 52.267 SEVERAL COUNTERSINKS BAD (FASTENER BELOW SKIN SURFACE) IN LOWER ROW OF FASTENERS. REAMED 24 EA HOLES ON 1/4" FASTENER ROW AND 14 ON 3/16 " FASTENER ROW FOR SLUG BUSHING REPAIR ON FIXED (A/C SIDE) PER BAC DWG SGJan 19, 2019 · N925DN · Doug MD9030SDR DALA2023012400531Skin · crackedVERTICAL STAB LE INDICATES CRACKING AT 4EA HOLES OF DOUBLER REPAIR STRAP. COMPLIED WITH ERA 564482-14AD REV ORIG.Jan 17, 2019 · N891AT · Boeing 717200SDR DALA2023012400530Skin · crackedDURING INSPECTIONS PER WORKCARD 5530-01048-01 & AD 2016-09-05, MTC FOUND A CRACK INDICATION COMMON TO THE VERTICAL SPLICE BETWEEN LOWER DORSAL ASSEMBLY SKIN & FRONT SPAR FORWARD CAP ON LT OF STAB. WORKCARD DOES NOT GIVE INSTRUCTIONS IF A CRACK IND IS FOUND. EJan 16, 2019 · N891AT · Boeing 717200SDR V0XD2019011600003Access Panel · crackedAFT LWR VERT. STAB. VISOR PANEL 326CR IS DAMAGED. CORRECTIVE ACTION: REPAIRED VISOR PANEL 326CR IAW REO 670-55-32-248 REV.- DATED 2019-01-13.Jan 14, 2019 · N165GJ · Cndair CL6002C10SDR SWAA2022022872702None · elongatedPRIORITY 3 : VERTICAL STAB LEADING EDGE UPPER ATTACH FASTENERS 5 EA HAVE ELONGATED HOLES . / REPAIRED VERTICAL STAB LEADING EDGE UPPER ATTACH FASTENER HOLES IAW EA 190012 IR AND EA 1-755-4299 REV IR.Dec 3, 2018 · N724SW · Boeing 7377H4SDR SWAA2018121027487Skin · damagedVERTICAL STABILIZER RT SIDE, EDGE OF SKIN MATERIAL MISSING BETWEEN BS 238 TO BS 243. REPAIRED SKIN PER EA.Nov 30, 2018 · N7703A · Boeing 73776NSDR C77A2018112900005Skin Panel · crackedDURING BASIC CHECK IN BNA, AN APPROXIMATELY 4.5 INCH LONG CRACK WAS DISCOVERED ON THE VERTICAL STABILIZER RT SKIN JUST AFT OF THE HOISTING POINT. REQUESTED AND RECEIVED PERMANENT REPAIR APPROVAL IN THE FORM OF ETD2018-170-121165 AND ITS CORRESPONDING ANAC DER Nov 29, 2018 · N637CZ · Emb ERJ170200LRSDR DALA201811206695Skin · debondedFOUND VERTICAL STABILIZER PANEL 370TL LEADING EDGE DISBONDING. REMOVED PANEL 370TL AND ROUTED TO COMPOSITE SHOP. REMOVED DELAMINATED MESH AND DAMAGED PAINT IN PERPETRATION FOR REPAIR, MD90 SRM 55-41-01. REPAIRED COPPER LIGHTNING PROTECTION IAW MD90 SRM 55-41-0Nov 17, 2018 · N963DN · Doug MD9030SDR J7SA20181115001Fairing · erodedV-STAB TIP FAIRING IS SHOWING SIGNS OF EROSION AND PAINT PEELING. REMOVED AND REPLACED THE VERTICAL STABILIZER - AFT UPPER FAIRING AS REQUIRED.Nov 15, 2018 · N408FX · Emb EMB545SDR J7SA2018112015001Fairing · damagedV-STAB TIP FAIRING IS SHOWING SIGNS OF EROSION AND PAINT PEELING. THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Nov 15, 2018 · N408FX · Emb EMB545SDR J7SA20181114001Fairing · erodedV-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING, THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. REMOVED AND REPLACED VERT STAB AFT UPPER FAIRING REF AMM 55-32-31. DUE TO WATER INTRUSION. AFT RED BEACON WAS ALSO REPLACENov 14, 2018 · N406FX · Emb EMB545SDR J7SA2018112014001Fairing · damagedV-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING, THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Nov 14, 2018 · N406FX · Emb EMB545SDR FDEA2018111983301Skin · delaminatedR/H VERTREAL STAB HAS SUSPECT PANEL DAMAGE ON LOWER R/H SIDE FWD OF BSTA 1729. REPAIRED IAW SRM 55-30-01-2RNov 8, 2018 · N916FD · Boeing 75727BSDR J7SA20181107001Fairing · not reportedREMOVED AND REPLACED VERTICAL STABILIZER AFT UPPER FAIRING. REMOVED AND REPLACED VERTICAL STABILIZER AFT UPPER FAIRING.Nov 7, 2018 · N407FX · Emb EMB545SDR J7SA201811207001Cap · damagedVERTICAL STABILIZER TIP CAP (BULLET) PAINT DAMAGED, BLISTERING + PEELING. THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Nov 7, 2018 · N407FX · Emb EMB545SDR J7SA20181106001Fairing · erodedV-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING. THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. REMOVED AND REPLACED V-STAB TOP AFT FAIRING ASSY AS REQUIRED REMOVED AND REPLACED LIGHT ASSY WITH NEW AS REQUIRED PERFORMENov 6, 2018 · N405FX · Emb EMB545SDR J7SA201811206001Fairing · damagedV-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING. THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Nov 6, 2018 · N405FX · Emb EMB545SDR DALA2018110876540Skin · crackedWHILE IN ATL FOR C-CHECK MTC REPORTED A CRACK COMMON TO THE V. STAB. RAM INLET SKIN. THE CRACK IS LOCATED AFT OF WHERE THE REMOVABLE SKIN ATTACHES. THE ER/A 00-563320 ASSOCIATED WITH THIS LOGPAGE AUTHORIZES A CUTOUT AND DOUBLER. (LP# 0300535, 0296632)Nov 5, 2018 · N936DN · Doug MD9030SDR DALA2018110606453Skin · crackedTHE VERTICAL STAB LEADING EDGE SKIN COMMON TO THE RHS FRONT SPAR IS CRACKED COMMON TO THE 2ND FASTENER HOLE AS SEEN IN FIG 1. AN EXISTING EXTERNAL REPAIR IS INSTALLED ON THE LEADING EDGE SKIN IMMEDIATELY BELOW ZFS=52.267, INSTALLED IN 2016 PER SG95550001 AND ANov 5, 2018 · N922AT · Boeing 717200SDR JGVR20181026001Access Panel · crackedREMOVED CRACKED VERTICAL STABILIZER ACCESS PANEL 340ER AND INSTALLED NEW P/N 5531005-3.Oct 26, 2018 · N618QS · Cessna 560XLSDR IPXA2018101835116Skin Panel · erodedVERTICAL STAB RT L/E PANEL ABOVE HF ANTENNA ERODED. REMOVED ERODED COMPOSITE AND INSTALLED COMPOSITE REPAIR IAW SRM 55-30-01-2R-6 AND 51-70-17. (MINOR)Oct 17, 2018 · N337UP · Boeing 76734AFSDR FDEA201810112844Skin Panel · crackedEMPENNAGE/ VERTICAL STABILIZER LT LOWER SKIN PANEL PYLON CARRY THROUGH REAR CENTER TO REAR SPAR STATION 2164 FOUND CRACK AS MARKED. EMPENNAGE - VERTICAL STABILIZER LEFT HAND LOWER SKIN PANEL PYLON CARRY THROUGH REAR CENTER TO REAR SPAR STATION 2164 REPAIR CARROct 11, 2018 · N523FE · Doug MD11FSDR FDEA2018091422464Skin Panel · crackedEMPENNAGE LT SIDE LOWER VERTICAL STABILIZER IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN PANEL CRACKED. SKIN PANEL REPAIR CARRIED OUT AS PER EA 1-5530-T0342403 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 12, 2018 · N592FE · Doug MD11F
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