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 SWAA2015010535459Skin Panel · erodedVERTICAL FIN LE HF ANTENNA PANEL HAS A HOLE ERODED THROUGH. REPAIRED PANEL IAW EA.Nov 24, 2014 · N718SW · Boeing 7377H4SDR SWAA2014120234595Access Panel · crackedVERTICAL STABILIZER ACCESS PANEL 9502 PLATE CRACKED. R & R PANEL IAW SRM & DWG.Nov 12, 2014 · N603SW · Boeing 7373H4SDR SWIA201439890Skin · crackedDISCOVERED A TWO INCH CRACK ON LEFT SIDE VERTICAL STABILIZER SKIN JUST AFT AND BELOW RUDDER PCU ACCESS PANEL. REPAIRED VERTICAL STAB SKIN IAW ETD AND SRM.Nov 7, 2014 · N221SW · Emb EMB120ERSDR C77A20141106001Skin · damagedDURING BASIC CHECK, INSPECTION DISCOVERED THE VERTICAL STABILIZER LE PANEL PN 170-63643-409 SN 0445 TO HAVE THE FOLLOWING DAMAGE, MULTIPLE AREAS OF EROSION DAMAGE ON THE OUTER SKIN AT LT & RT SIDES, SEVERAL LT & RT FASTENER LOCATIONS ON THE INNER SURFACE WERE Nov 6, 2014 · N638CZ · Emb ERJ170200LRSDR FDEA201411043503Panel · delaminatedVERTICAL STAB HINGE PANEL 374EL HAS DELAMINATION. REPAIRED IAW SRM 51-71-00 VOL II .Nov 4, 2014 · N550FE · Doug MD1010FSDR FDEA201411043500Panel · delaminatedVERTICAL STAB FWD OF LOWER RUDDERS, HINGED PANEL 374CL HAS DELAMINATION. REPAIRED PANEL 374CL IAW SRM 51-71-00 & PAINTED IAW SRM 51-21-02 VOL II.Nov 4, 2014 · N550FE · Doug MD1010FSDR AALA20141019010Skin · crackedVERTICAL STABILIZER SKIN LT LOWER END AT FASTENER HOLE STATION 1425 CRACKED. INSTALLED FORMED ANGLE REPAIR IAW SRM 55-05-00-001.Oct 19, 2014 · N971TW · Doug DC983SDR HYIA20141017059Skin · corrodedUPON REMOVAL OF PAINT, SURFACE CORROSION LT SIDE OF THE VERTICAL STABILIZER. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS. IAW EOct 17, 2014 · N14834 · Aerosp ATR42320SDR WX0A2014101972204Channel · damagedVERTICAL STAB TIP FAIRING FWD LOWER LT & RT CHANNELS DAMAGED. REMOVED DAMAGE, FABRICATED PARTS, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-70-5 FIG 2. WORK ACCOMPLISHED ON WORK ORDER 234294 M301 ITEM 419 & WORK ORDER 1011332 3300-0095.Oct 15, 2014 · N879GA · Doug DC983SDR AALA20141003004Skin · damagedTWO HOLES WERE FOUND DISTRESSED AT ZFS 52.267. ACCOMPLISHED REPAIRED IAW SRM 55-03-00.Oct 3, 2014 · N454AA · Doug DC982SDR SWAA2014100332612Fairing · crackedVERTICAL STABILIZER LE RAM AIR FAIRING CRACKED. REPAIRED FAIRING IAW SRM.Oct 3, 2014 · N988AT · Boeing 717200SDR FXGA201409231438Skin · gougedVERTICAL STABILIZER LT TIP PLATING REPAIR FROM ZV73 TO ZV147 BETWEEN YV157 & YV172. GOUGES FOUND ON FWD LT SIDE OF VERTICAL STABILIZER UNDER UPPER & LOWER BANANA FAIRING.Sep 23, 2014 · N935CE · Doug DC933FSDR GLBA2014092200444Skin · dentedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND DENT IN THE VERT STAB LE, DENT AREA BEGINS AT CSS 54.026, JUST ABOVE RIB UPWARD TO CSS 66.00, DEPTH APPROX .5 INCHES TO .75 INCHES, ALLOWING FOR ORIGINAL CONTOUR AT LE. REPAIRED THE AFFECTED AREA & Sep 22, 2014 · N165YV · Beech 1900DSDR AALA20140915007Skin · wornLEADING EDGE OF VERTICAL BELOW ZFS 52.267 WORN. ACCOMPLISHED NESTED ANGLE REPAIR IAW SRM 55-03-00 FIGURE 29.Sep 15, 2014 · N468AA · Doug DC982SDR AALA20140915006Skin · wornVERTICAL STABILIZER LE JUST BELOW ZFS 52 HAS WORN HOLES. INSTALLED PLUG IAW EA MD80-55-036666.Sep 15, 2014 · N468AA · Doug DC982SDR DALA2014091805112Skin · corrodedCORROSION FOUND ON INBD AND OTBD FACE OF VERTICAL STABILIZER PLATES, ZRS= 178. CORROSION WAS REMOVED IAW SRM 55-02, PAR 24 AND 51-10-3, PAR 26, 21, 14.Sep 15, 2014 · N972DL · Doug MD88SDR AALA20140912010Skin Panel · wornFOUND WEAR IN FASTENER HOLES ON VERTICAL STABILIZER LE PANEL. INSTALLED REPAIR DOUBLER ON VERTICAL STABILIZER LE PANEL IAW SRM 55-03-00-001.Sep 12, 2014 · N468AA · Doug DC982SDR SWAA2014110433720Duct · crackedVERTICAL STABILIZER RAM AIR INLET DUCT LT SIDE CRACKED. REPAIRED DUCT IAW SRM.Sep 6, 2014 · N969AT · Boeing 717200SDR SWAA2014090931730Access Panel · crackedVERTICAL STABILIZER ACCESS PANEL 9523 CRACKED. R & R PANEL IAW SRM & DWG.Aug 23, 2014 · N397SW · Boeing 7373H4SDR IPXA2014082084040Skin · delaminatedVERTICAL STABILIZER LT SIDE LOWER PANEL DELAMINATED.. TRANSFERRED TO NRC 529065 FOR PANEL REPLACEMENT. COMPLETED PANEL REPLACEMENT IAW EO B7U67-5530-55201-A. MAJOR REPAIRAug 19, 2014 · N323UP · Boeing 76734AFSDR AALA20140818003Panel · damagedWORN FASTENER HOLES IN VERTICAL STABILIZER LE REMOVABLE PANEL. INSTALLED DOUBLER REPAIR STRAP IAW SRM 55-03-00 FIGURE 30.Aug 18, 2014 · N483A · Doug DC982SDR SWAA2014082831389Plate · crackedVERTICAL STABILIZER DOOR RUDDER FRONT SPAR ACCESS PANEL 9503 PLATE CRACKED. R & R PLATE IAW SRM & DWG.Aug 13, 2014 · N398SW · Boeing 7373H4SDR DALA2014080804449Skin · damagedSIX HOLES IN PREVIOUS REPAIR AT RT SIDE VERTICAL STAB L/E STA ZFS 52 UPPER SIDE, ELONGATED. REPAIRED IAW PRI 528091-14AD, REV 1. BROUGHT HOLES IN L/E AND FLANGE TO .265". REMOVED DOUBLER FROM L/E. FABRICTED -3 REPAIR STRAP, LOWER L/E DOUBLER AND RT & LT CUAug 8, 2014 · N939DL · Doug MD88SDR AALA20140731006Skin · damagedVERTICAL STABILIZER LE SKIN & SPAR DAMAGE. REPAIRED DAMAGED FASTENER HOLES IAW EA MD80-55-035970.Jul 31, 2014 · N501AA · Doug DC982SDR SWAA2014072830363Fairing · crackedVERTICAL STABILIZER LE RAM AIR FAIRING CRACKED. REPAIRED FAIRING IAW SRM.Jul 29, 2014 · N988AT · Boeing 717200SDR AALA20140722010Skin · damagedSEVERAL FASTENER HOLES IN VERTICAL STABILIZER LE ABOVE STATION ZFS 52.267 OVERSIZED BEYOND MANUAL LIMITS. INSTALLED REPAIR BUSHING IAW SRM 55-03-00-001 FIGURE 30.Jul 21, 2014 · N501AA · Doug DC982SDR SWAA2014072830405Plate · crackedVERTICAL STABILIZER ACCESS PANEL 9506R PLATE CRACKED. R & R PLATE IAW SRM & DWG.Jul 16, 2014 · N394SW · Boeing 7373H4SDR AALA20140713002Skin Panel · delaminatedVERTICAL STABILIZER LT SIDE HAS AN AREA OF DELAMINATION ON THE SIDE SKIN CENTERED 63 INCHES FROM THE LE & 58 INCHES UP FROM THE FUSELAGE. PANEL REPAIRED IAW EA B767-55-035420.Jul 13, 2014 · N386AA · Boeing 767323SDR DALA2014070803946Skin · delaminatedFOUND DELAMINATION ON VERTICAL STAB JUST AFT OF LOWER LEADING EDGE LT SIDE AT FSS 120- FSS 170. REPAIRED IAW ERA 527342-14 REV ORIG.Jul 7, 2014 · N519US · Boeing 757251SDR USAA2014072800034Panel · delaminatedC1 CHECK DELAMINATION ON RT VERTICAL STABILIZER LOWER TORQUE BOX PANEL AT FSS 220 APPROX 4 INCHES FROM LE OF PANEL. REPLACED RT VERTICAL STABILIZER LOWER TORQUE BOX PANEL AT FSS 220 IAW DWG 175N2001.Jul 2, 2014 · N935UW · Boeing 7572B7SDR DALA2014070103938Skin · crackedCRACK FOUND ON VERTICAL STABILIZER SKIN STA ZFS=18 LT SIDE FWD SECTION. INSTALLED REPAIR ON THE SKIN IAW SRM 55-01 FIG.2.Jun 30, 2014 · N969DL · Doug MD88SDR SWAA2014072230206Fairing · crackedLEFT VERTICAL STABILIZER TRANSITION FAIRING CRACKED. R & R FAIRING IAW SRM.Jun 27, 2014 · N959AT · Boeing 717200SDR SWAA2014070829729Access Panel · crackedVERTICAL STABILIZER RETAINER PLATE ACCESS PANEL 9502 CRACKED. R & R PANEL IAW SRM & DWG.Jun 25, 2014 · N392SW · Boeing 7373H4SDR AALA20140617001Skin · damagedVERTICAL STABILIZER LE SKIN BELOW THE ZFS 52.267 SPLICE HAS A NR OF HOLES DAMAGED IN THE SKIN & THE LT SPAR CAP. INSTALLED PLUG BUSHING IAW SRM 55-03-00 FIGURE 30 & INSTALLED EXTERNAL DOUBLER IAW SRM 55-03-00 & EA MD80-55-035355.Jun 17, 2014 · N403A · Doug DC982SDR DALA2014061803663Skin · damagedDAMAGE INSIDE FIRST THREE HOLES ABOVE SKIN SPLICE AT STA Z52 LT SIDE. REPAIRED DAMAGE IAW ERA 526640-14AD, REV O.Jun 17, 2014 · N953DN · Doug MD9030SDR DALA14036095806Skin · damagedLEFT SIDE OF VERTICAL STABILIZER, 17.5-26" AFT OF AUX SPAR /36.5 -37.5" ABOVE FUSELAGE: SEVERAL GOUGES IN SKIN EXTERIOR SURFACE AND THE AREA 17.5-18.5" AFT OF AUX SPAR IS DENTED. COMPLIED WITH ERA 525953-14, REV ORIGINAL PERMENANT REPAIR ON THE VERTICAL STABIJun 11, 2014 · N586NW · Boeing 757351SDR REXA2014061200473Fastener · burnedBURNED FASTENER HEAD ON THE LT VERTICAL STABILIZER SKIN. REPAIRED IAW EA CRJ255-02642.Jun 11, 2014 · N8969A · Cndair CL6002B19SDR WX0A071966Fairing · damagedVERTICAL STAB LE FAIRING AT SPAR CAP HAS ONE EACH ELONGATED HOLE, 2 ROWS ABOVE STATION ZFS 52.267 LT SIDE 6TH ROW FROM BOTTOM. REMOVED DAMAGE FOR BUSHING REPAIR, HFEC INSPECTED NO CRACKS NOTED IAW SRM 55-03 PARA 27. FABRICATED BUSHING & INSTALLED BUSHING IAWMay 28, 2014 · N887GA · Doug MD83SDR SWAA2014052028164Fairing · crackedVERTICAL STABILIZER LE RAM AIR FAIRING PREVIOUS WELD REPAIR CRACKED. REPAIRED STABILIZER IAW SRM.May 20, 2014 · N988AT · Boeing 717200SDR DALA14028339223Skin · wornVERTICAL STABILIZER L/E PANEL AT UPPER END OF ZFS52.267 HAS 14 EA FASTENERS WORN IN SKIN. HFEC HOLES. FABRICATED BUSHING ON N/R 14 IAW DWG SG09530004. INSTALLED REPAIR BUSHINGS.May 2, 2014 · N923DN · Doug MD9030SDR DALA14026330937Skin · crackedCRACK INDICATION ON VERTICAL STABILIZER CAP L/E FASTENER HOLE RT SIDE MARKED ON RED. REPAIRED IAW ER/A 525281-14AD REVISION ORIGINAL. PERFORMED RUDDER PITOT LEAK TEST IAW AMM 34-11-00. LEAK TEST GOOD. PERFORMED RUDDER PITOT HEAT TEST IAW AMM 34-11-02. HEATApr 26, 2014 · N937DL · Doug MD88SDR DALA14026340937Skin · crackedCRACK INDICATION ON LT VERTICAL STAB L/E CAP FASTENER. HOLE MARKED IN RED. REPAIRED IAW ER/A 525281-14AD, REV ORIGINAL. PERFORMED RUDDER PITOT LEAK TEST IAW AMM 34-11-00. LEAK TEST GOOD. PERFORMED RUDDER PITOT HEAT TEST IAW AMM 34-11-02. HEAT TEST GOOD. PEApr 25, 2014 · N937DL · Doug MD88SDR AALA20140424002Skin · damagedTHREE LOOSE FASTENERS FOUND ON DETAILED INSPECTION OF VERTICAL STAB LE AT STATION ZFS 52.267 ABOVE THE SPLICE. FURTHER INSPECTION FOUND 7 EXISTING FASTENER HOLES WITH REPAIR COUNTERSUNK BUSHINGS INSTALLED & 14 ADDITIONAL FASTENER HOLES THAT WERE ELONGATED. EApr 24, 2014 · N7541A · Doug DC982SDR AALA20140424001Doubler · damagedSEVEN LOOSE FASTENERS FOUND ON DETAILED INSPECTION OF VERTICAL STAB LE AT STATION ZFS 52.267 BELOW THE SPLICE. REMOVED EXISTING SMALL DOUBLER & FOUND 18 1/4 FASTENER & 11 3/16 FASTENER HOLES TO BE ELONGATED. INCREASED DIAMETER OF HOLES & INSTALLED STRAIGHT SApr 24, 2014 · N7541A · Doug DC982SDR WVER201404175048Skin · damagedRT VERTICAL STABILIZER SKIN DAMAGED .Apr 17, 2014 · N504MJ · Cndair CL6002C10SDR SWAA2014052728346Access Panel · crackedVERTICAL STABILIZER ACCESS PANEL 9536 CRACKED. REPAIRED PANEL IAW SRM.Apr 15, 2014 · N387SW · Boeing 7373H4SDR A6WA201441425Panel · crackedLEFT UPPER VISOR PANEL CRACKED FROM RIVET HOLE. R & R VISOR PANEL PN 600-21133-43.Apr 9, 2014 · N443 · Cndair CL6002B19SDR SWAA2014041427068Panel · damagedRIGHT SIDE VERTICAL STABILIZER BELOW ELEVATOR PITOT PANEL DAMAGED. R & R PANEL IAW SWA EA.Apr 7, 2014 · N268WN · Boeing 7377H4SDR DALA14020739203Skin · crackedCRACK FOUND VERTICAL STAB SKIN AT BS 1475, L2R. ERA 524612-14, SECTION I WAS ACCOMPLISHED IN MSP.Apr 5, 2014 · N903DA · Doug MD9030SDR IPXA2014041482628Panel · delaminatedINSPECTION: C9, RT LOWER VERTICAL STAB TORQUE BOX PANEL IS DELAMINATED SEVERAL AREAS. REPAIRED IAW REO-G17337, REV B & EO B757-5530-54064-A.Mar 27, 2014 · N458UP · Boeing 75724APF
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