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 IPXA11564093Skin Panel · delaminatedINSPECTION TYPE:C2 VERTICAL STAB, AREA OF DELAMINATION ON LT L/E FIXED PANEL, 24 INCHES FROM L/E, 11 INCHES FROM BOTTOM OF PANEL CUTOUT 322CL (HF ANTENNA). R & R PANEL ASSY IAW SRM 51-40-02.Dec 31, 2010 · N413UP · Boeing 75724APFSDR DALA1053140909Skin · gougedDURING HMV4, FOUND VERTICAL STAB LT SIDE STA YV-170 AND ZV-174 SKIN CUTOUT GOUGED IN RADIUS. MEASURED DEPTH OF GOUGE, .046 MEASURED ORIG MAT. 0.062 IAW SRM 55-32-00, FIG 3, SHT 2. REMAINING MAT. 0.016, FOUND TO BE OUT OF LIMITS IAW SRM 55-01, FIG 1, RECEIVEDDec 29, 2010 · N909DL · Doug MD88SDR DALA1036499864Skin · tornDURING M-CHECK, FOUND VERTICAL STABILIZER RUDDER TOP END, RT SIDE SKIN TORN AT EDGE. REMOVED DAMAGED AREA ON VERTICAL STAB RUDDER IAW SRM 51-70-06, FIG 2, SHT 1. HFEC INSP NO OTHER DAMAGE NOTED NDT SPM 06-10-01.001. FABRICATED AND DRILLED DOUBLER AND FILLERDec 22, 2010 · N773NC · Doug DC951SDR FDEA201011294513Skin · crackedVERT STAB INTERIOR AT BS 1303 VERT FRAME HAS 3 EA CRACKS ON LWR LT & RT WEB. CUTOUT DAMAGED AREAS AND FABRICATED REPAIR DOUBLERS & FILLERS & INSTALLED REPAIR DOUBLERS 2 EA & FILLERS 2 EA AT VERT STAB BS 1303 VERT FRAME WEB IAW SRM 53-10-9, FIG 4, SRM 55-30-2Nov 29, 2010 · N233FE · Boeing 727247SDR DALA1305130944Skin · wornDURING CHECK, WEAR DAMAGE WAS NOTED TO UPPER EDGE OF THE VERTICAL STABILIZER LOWER FIXED L/E DUE TO SKIN WASHER INSTALLATION. REPAIR IAW ERA 487430-14.Nov 22, 2010 · N944DL · Doug MD88SDR USAA2010121793130Access Panel · delaminatedSAL - MAJOR REPAIR - S5 CHECK - VERTICAL STABILIZER ACCESS PANEL 327AL HAS AREA OF DELAMINATION. REPAIRED VERTICAL STABILIZER ACCESS PANEL 327A IAW EA 133199.Nov 19, 2010 · N628AW · Airbus A320231SDR USAA2010111592608Skin Panel · delaminatedCLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER SKIN PANEL 6 INCHES AFT OF AUXILIARY SPAR AT STATION 120 IS DELAMINATED. REPLACED VERTICAL STABILIZER SKIN PANEL 6 INCHES AFT OF AUXILIARY SPAR AT STATION 120 IAW BOEING 757 DRAWING 175N2001.Nov 5, 2010 · N940UW · Boeing 7572B7SDR IPXA10563479Panel · delaminatedINSPECTION TYPE:C4, UPON REMOVAL OF RT VERT STAB PANEL, FOUND LT VERTICAL STA PANEL (PN 3175N2001-3) DELAMINATED ON INNER SURFACE. R & R PANEL IAW SRM 51-40-02-0G.Nov 1, 2010 · N453UP · Boeing 75724APFSDR USAA2010111592606Panel · delaminatedCLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER LEFT TORQUE BOX PANEL HAS DELAMINATION. REPAIRED VERTICAL STABILIZER LEFT TORQUE BOX PANEL IAW EA 139564.Oct 31, 2010 · N940UW · Boeing 7572B7SDR ZZDA2010550Skin · dentedVERTICAL FIN LEADING EDGE SKIN, STA 196.663 TO 205.663, DENTED. ACCOMPLISHED SKIN DOUBLER REPAIR PER B737 SRM 55-30-01 REPAIR 1.Oct 28, 2010 · N175AT · Boeing 73776NSDR DALA1029249003Skin · damagedELONGATED SCREW HOLE ON LOWER AFT SECTION OF VERTICAL STAB REMOVABLE LEADING EDGE AT STA ZFS = 54 RIGHT SIDE. REPAIRED PER ERA 485923-14 REV ORG. (DLM88102889)Oct 22, 2010 · N903DE · Doug MD88SDR DALA1029339003Skin · damagedELONGATED SCREW HOLES ON LOWER AFT SECTION OF VERTICAL STAB REMOVABLE LEADING EDGE LEFT SIDE REPAIR PER ERA 485924-14 REV ORG. (DLM88102902)Oct 13, 2010 · N903DE · Doug MD88SDR CALA2010100800471Skin · damagedSUPPORT TASK,VERTICAL STABILIZER L/E HAS A BIRD STRIKE APPROX 41 INCHES FROM LOWER END CUT OUT DAMAGED SECTION OF LEADING EDGE, FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR REF SRM 55-30-01.Oct 8, 2010 · N19638 · Boeing 737524SDR USAA2010101492286Skin Panel · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON OUTER SKIN OF RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL. INSTALLED SERVICEABLE RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL.Oct 7, 2010 · N942UW · Boeing 7572B7SDR REXA201000186Fairing · damagedRIGHT SIDE VERTICAL STABILIZER LOWER VISOR FAIRING AFT END DAMAGED. THE DAMAGE CONSISTS OF THE AFT FLANGE BEING DEFORMED / BENT AND POSSIBLE SEPARATION OF THE P/N 600-21134-14 RUBBING STRIP FROM THE VISOR FAIRING. REPAIRED IAW STS ENGINEERING EA 5-2010-213.Oct 6, 2010 · N8611A · Cndair CL6002B19SDR DALA1319369212Skin · damagedTHE HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL DAMAGED. REPAIRED IAW ERA 477402-14.Oct 5, 2010 · N912DN · Doug MD9030SDR IPXA10563191Skin Panel · delaminatedINSPECTION TYPE:C4, VERTICAL STAB, 2 AREAS OF DELAMINATION, APPROX 15" DIA, AND 5" DIA, AT RT SIDE L/E, 64" AND 89" FROM TOP OF FUSELAGE. R & R SKIN PANEL IAW SRM 51-30-01-0G & DWG 175N2001.Oct 3, 2010 · N453UP · Boeing 75724APFSDR DALA1024759009Panel · damagedVERTICAL STABILIZER/ LOWER FIXED L/E PANEL/ UPPER EDGE/ ZFS52/ HOLE DAMAGE. REPAIRED IAW ER/A 485868-14.Sep 28, 2010 · N909DE · Doug MD88SDR C2XA10TY128Panel · damagedPANEL 321CL INSIDE SURFACE HAS COMPOSITE DAMAGE NEAR L/E. REPAIRED PANEL IAW EMB 145 EC5530-01183.Sep 14, 2010 · N18982 · Emb EMB145LRSDR REXA201000130Fairing · crackedFLIGHT 4348, WAS PUSHED AT 19:24 OFF GATE A2 INTO AIRCRAFT 8903A. THE VERTICAL STABILIZER AFT FAIRING OF 8932C HIT THE LEFT LEADING EDGE OF 8903A. THEN, AS THE AIRCRAFT WAS BEING PUSHED FARTHER, THE LEFT HORIZONTAL STABILIZER OF 8903A WAS DRAGGED ALONG THE TSep 3, 2010 · N8932C · Cndair CL6002B19SDR DALA1020360911Skin · wornVERTICAL STABILIZER/ L/E SKIN UPPER REMOVABLE PANEL LOWER EDGE WEAR DAMAGE.Aug 23, 2010 · N911DL · Doug MD88SDR FDEA201008233112Skin · dentedDENT ON LT SIDE VERT STAB FSS-146 EVALUATED 2EA DENTS ON VERT STAB STA FSS-146. DENTS WITHIN 1SQ FT OF EACH OTHER. FOUND OUT OF LIMITS IAW SRM 55-30-01, FIG 101, DETAIL III NOTE "H". REPAIRED DENTS IAW SRM 51-70-10, REPAIR 2. CLASSIFIED CATEGORY "A" MAJOR Aug 23, 2010 · N902FD · Boeing 7572B7SDR FDEA201008233111Skin · dentedDENT IN LT SIDE OF VERT STAB FSS-153 EVALUATED 2EA DENTS ON STAB STAB STA FSS 153. DENTS WITHIN 1SQ FT OF EACH OTHER. FOUND OUT OF LIMITS IAW SRM 55-30-01, FIG 101, DETAIL III AND NOTE "H". REPAIRED DENTS IAW SRM51-70-10, REPAIR 2 CLASSIFIED CATEGORY "A" MAJAug 23, 2010 · N902FD · Boeing 7572B7SDR DALA1020020909Skin · chafedVERTICAL STAB REMOVABLE L/E LOWER FASTENERS LOOSE, SKIN WASHERS DIGGING INTO VERT SKIN.Aug 20, 2010 · N909DL · Doug MD88SDR IPXA10B62920Panel · misinstalledINSPECTION TYPE:C, RT OF VERT STAB FIN STA 245 TO STA 220 2FT AFT FROM FIN L/E 2 ROWS OF REPAIRED BLIND RIVETS WAS FOUND. RT VERT STAB FIN STA 220-245 2FT AFT FROM FIN L/E 2 ROWS OF REPAIRED BLIND RIVETS REPLACED WITH RIVET (BACR15FP6E3R) IAW HXRS R55-00-3681Aug 17, 2010 · N580UP · Boeing 747428FSDR IPXA10B62919Panel · misinstalledINSPECTION TYPE:C, LT OF VERT STAB FIN STA 169 TO STA 195 2 ROWS OF REPAIRED BLIND RIVETS. LT VERT STAB FIN STA 169-195 2 ROWS OF REPAIRED BLIND RIVETS REPLACED WITH RIVET (BACR15FP6E3R) IAW HX RS R55-00-36819, REV A & EO B747-5530-39812-A, TOTAL 125EA REPLACAug 17, 2010 · N580UP · Boeing 747428FSDR ZZDA2010407Skin · damagedLEFT SIDE VERTICAL STAB SKIN AND STRUCTURE, DAMAGED. ACCOMPLISHED DOUBLER AND SKIN REPAIR PER EA 17-55-02781IR.Aug 15, 2010 · N972AT · Boeing 717200SDR A6WA201040533Skin · gougedPANEL 326CR OUTER SKIN HAS NUMEROUS GOUGES, DEEPEST GOUGE .017". BLENDED GOUGES IAW REO 601R-55-32-267.Jul 7, 2010 · N402AW · Cndair CL6002B19SDR DALA1019799001Skin · chafedVERTICAL STAB STR LT SIDE LOWER AFT SIDE OF CUTOUT, SKIN PANEL CHAFED. BLENDED CHAFED AREA, FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW SRM 55-01, FIG 4.Jul 2, 2010 · N901DE · Doug MD88SDR DALA1016479001Skin Panel · crackedHMV3 VERTICAL STAB LOWER LT SKIN PANEL CRACKED AT LOWER AFT CORNER OF PANEL. CUT OUT REPAIR SKIN PANEL IAW SRM 55-01 FIG 2 55-32-0 (DLM88101838).Jul 2, 2010 · N901DE · Doug MD88SDR DALA1015280951Skin · wornVERT STAB LEADING EDGE LOWER SKIN HOLES WORN AT ZFS 52. REPAIRED PER ERA 483658-14 ON NR 31.Jun 25, 2010 · N951DL · Doug MD88SDR IPXA10660984Panel · delaminatedINSPECTION TYPE:C, EMP - VERTICAL STABILIZER RT L/E FIXED PANEL (FSS49 TO FSS59) FOUND DELAMINATION. METAL HOT BOND REPAIR CARRIED OUT IAW EO B767-5530-38665-A REFER RS R-55-30-36766, REV A.Jun 23, 2010 · N301UP · Boeing 76734AFSDR DALA1115930922Skin · damagedVERTICAL STABILIZER, L/E SKIN, UPPER REMOVABLE PANEL, LOWER EDGE WEAR DAMAGE REPAIRED IAW ERA 483216-14.Jun 18, 2010 · N922DL · Doug MD88SDR IXXA10SMN059SSkin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR ON THE VERTICAL STABILIZER L/E AT STA ZFS 292. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND REPAIR SPLICE. PERFORMED NDT INSP. NO DIJun 10, 2010 · N71CX · Doug DC862FSDR DALA1144820929Skin · crackedVERT STAB ZFS 44 LT SKIN, LT FWD SPAR CHORD AND WEB CRACK. REPAIRED IAW ERA 481559-14.Jun 9, 2010 · N929DL · Doug MD88SDR CA100706006Skin · crackedVERTICAL STAB SKIN CRACKED MID HEIGHT ALONG SPAR.Jun 3, 2010 · Cessna 208SDR DALA1202190931Skin · damagedVERT STAB L/E SKIN UPPER REM PNL LWR EDGE REPAIRED IAW ERA 482723-14.Jun 2, 2010 · N931DL · Doug MD88SDR ASAA1047858Access Panel · gougedVERTICAL STAB ACCESS PANEL 9503 IS GOUGED ON THE EDGES. FABRICATED AND INSTALLED NEW PANEL.May 11, 2010 · N708AS · Boeing 737490SDR USAA2010051790978Panel · debondedCLT - C2 - MAJOR REPAIR - NR 19-9755-8-0020 & 5003005 - DISBONDING ON RIGHT VERTICAL TORQUE BOX PANEL. REPAIRED RIGHT VERTICAL TORQUE BOX PANEL IAW B757 SRM 51-70-10 & US AIRWAYS EA 101928.May 5, 2010 · N941UW · Boeing 7572B7SDR IXXA100029SSkin · crackedDURING PREFLIGHT, FOUND VERTICAL STABILIZER L/E CRACKED AT STA ZFS 292 CTR LINE. REPLACED CRACKED L/E WITH INTERIM REPAIR IAW FVCI DWG NR 55-10165-1.May 1, 2010 · N71CX · Doug DC862FSDR UHLA2010042900046Skin · crackedMAJOR REPAIR - VERTICAL STAB RT SIDE SKIN IS CRACKED JUST ABOVE AFT UPPER HOIST POINT. PERFORMED DEFINITIVE REPAIR ON RT UPPER VERT STAB IAW ETD2010-170/02797. REMOVED DAMAGED AREA IAW ETD, PERFORMED EDDY CURRENT ON CUTOUT, NO CRACK LINE INDICATIONS FOUND IAWApr 29, 2010 · N637RW · Emb ERJ170100SUSDR WX0A070562Skin · chafedLEFT AND RIGHT AFT SECTION OF VERTICAL STAB HAS CHAFE MARK, BURNISHED OUT AND MEASURED, FOUND TO BE OUT OF LIMITS AS PER 55-01, MD80SRM. REMOVED SKIN SECTION AT LEFT AND RIGHT AFT VERTICAL STABILIZER AND REPLACED AS PER MD80 SRM 51-30-2.Apr 28, 2010 · N877GA · Doug MD83SDR WX0A070560Skin · gougedLEFT SIDE VERTICAL STABILIZER SKIN EDGE UNDER FWD LOWER BANANA FAIRING PREVIOUS GOUGE REPAIR IS GETTING WORSE. TRIMMED OUT DAMAGE, REMOVED PREVIOUS REPAIR AND INSTALLED NEW REPAIR AS PER RES 2002302-2.Apr 27, 2010 · N877GA · Doug MD83SDR UHLA2010041600046Skin · crackedMAJOR REPAIR - CRACK IN VERTICAL STAB JUST AFT OF RT UPPER HOIST POINT. STOP DRILLED CRACK TIPS AND PERFORMED NDI HFEC INSPECTION TO LOCATE CRACK TIPS IAW EMB 175 SRM 51-10-04. ACCOMPLISHED FINAL REPAIR TO RT SKIN OF VERTICAL STAB IAW ETD 2010-170/02797 REV Apr 16, 2010 · N208JQ · Emb ERJ170200LRSDR DALA1012420929Skin · crackedLT VERT STAB L/E SKIN, WEB AND CHORD CRACKED REPAIRED IAW ERA 481906-14. (DLM88101445)Apr 11, 2010 · N929DL · Doug MD88SDR DALA1111280915Skin Panel · damagedVERTICAL STAB UPPER FIXED L/E REMOVABLE PANEL OVERSIZED HOLES REPAIRED IAW ERA 481049-14.Mar 29, 2010 · N915DL · Doug MD88SDR IPXA10559171Skin · damagedINSPECTION TYPE:C2, LIGHTNING STRIKE ON VERT STAB SKIN WL574, 33.5" FROM TOP OF TIP. REPAIRED IAW ATS ER 10-2268.Mar 27, 2010 · N409UP · Boeing 75724APFSDR IPXA10559170Skin · damagedINSPECTION TYPE:C2, LIGHTNING STRIKE ON VERT STAB, WL576.8, FSS423. REPAIRED IAW ATS ER 10-2268.Mar 27, 2010 · N409UP · Boeing 75724APFSDR IPXA10559169Skin · damagedINSPECTION TYPE:C2, LIGHTNING STRIKE ON VERT STAB SKIN, WL572, FSS414.7 REPAIRED IAW ATS ER 10-2268.Mar 27, 2010 · N409UP · Boeing 75724APFSDR 2010FA0000312Skin · corroded(SPUY) DURING ROUTINE C-CHECK INSPECTION, VERT STAB - CORROSION BETWEEN SKIN AND BEADED DOUBLER (STA ZR 153.000 - 281.963).Mar 26, 2010 · N802DH · Doug DC873
Back to JASC 5532