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 DALA1222980930Skin · damagedDURING HMV, SUNKEN FASTENERS WAS FOUND ON VERTICAL STABILIZER LEADING EDGE SKIN TOW ROW OF FASTENERS BELOW THE SPLICE AT STA ZFS=52.2. VERTICAL STABILIZER SKIN WAS REPAIRED IAW EO 09-470871-12AD ME08 REV G AND DWG SG09550004 REV ORIG.Apr 14, 2012 · N930DL · Doug MD88SDR FDEA201204101333Skin · crackedLOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. NR 2 ENGINE FIRE DETECTION CONTROL UNIT CARRIEDApr 10, 2012 · N577FE · Doug MD11FSDR DALA1222049261Skin · crackedDORSAL FIN FWD LOWER PANEL CUTOUT UPPER CORNER CRACKED. INSTALLED DOUBLER REPAIR PER SRM 51-70-01 VOL I.Apr 5, 2012 · N961DN · Doug MD9030SDR FDEA201204021231Skin · puncturedVERTICAL STAB SKIN AT BS1898 PUNCTURED. REMOVED DAMAGE, CLEANED, PREPPED AND BONDED REPAIR AREA, FINISHED SANDED, PER SRM 51-71-00. TREATED AND PRIMED PER SRM 51-20-01. SEALED PER SRM 51-71-00. BONDED DOUBLER REPAIR IS AT BL0, BS 1898, ON SKIN. MAJOR RApr 2, 2012 · N962FD · Boeing 7572G5SDR WX0A071141Skin · crackedREPAIRED CRACK IN VERTICAL STAB LEADING EDGE RAM AIR DUCT SKIN IAW EA 10-2012-066 AND MD80 SRM 55-05 PAR 6. REPAIRED CRACK IN VERTICAL STAB LEADING EDGE RAM AIR INLET DUCT SKIN IAW AAR/STS 10-2012-2066 PERMANENT REPAIR.Mar 31, 2012 · N895GA · Doug DC982SDR DALA1220280997Skin · crackedVERTICAL STAB REMOVABLE LEADING EDGE HAS CRACK INDICATION AT LOWER LEFT AFT CORNER HOLE. REPAIRED PER ERA501898-14AD REV ORIGINAL.Mar 29, 2012 · N997DL · Doug MD88SDR EE4Y20120326149Skin · damagedVERTICAL STABILIZER RT SIDE BETWEEN RIB 3 AND RIB 4 SKIN WITH LIGHTNING STRIKE. DAMAGED AREA WAS REPAIRED IAW REPAIR GUIDELINES 70560175/006, UNDER THE NON ROUTINE ITEM: WO A1A079, SUB JOB 3, ITEM 11.Mar 26, 2012 · N522NK · Airbus A319132SDR FDEA201203201033Skin · crackedLOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Mar 20, 2012 · N576FE · Doug MD11FSDR ASOA201200944Skin · dentedDURING BIRD STRIKE INSPECTION, FOUND DENTS IN VERTICAL STAB L/E. REPAIRED IAW SRM 51-40-11-001-001Mar 18, 2012 · N730EV · Cndair CL6002C10SDR DALA1216160988Skin · damagedDURING PSV IN MSP AND DURING AD INSPECTION PER 09-470871-12AD REF "F DISCREPANT HOLES WERE FOUND COMMON TO THE LOWER FIXED L/E SKIN. THREE HOLES EXCEEDED THE LIMITS OF SG09550004 REV "A". SUBJECT HOLES WERE REPAIRED PER ER/A 501324-14AD.Mar 13, 2012 · N988DL · Doug MD88SDR C77A20130502010Skin · damagedDURING A POST FLIGHT, FOUND A HOLE IN THE VERTICAL STABILIZER. THE DAMAGE CONSISTS OF A CRACK WHICH IS 8.75" LONG AND A HOLE IN THE LOWER THIRD OF THE CRACK WHICH MEASURES APPROX 1.75" IN DIAMETER. THIS DAMAGE IS OUT OF SRM LIMITS.Feb 25, 2012 · N627CZ · Emb ERJ170200LRSDR C77A2013050100001Skin · damagedDURING A POST FLIGHT WALK AROUND INSPECTION, ACFT WAS REPORTED TO HAVE A HOLE IN THE VERTICAL STABILIZER. THE DAMAGE CONSISTS OF A CRACK WHICH IS 8.75" LONG AND A HOLE IN THE LOWER THIRD OF THE CRACK WHICH MEASURES APPROX 1.75" IN DIAMETER. THIS DAMAGE IS Feb 25, 2012 · N627CZ · Emb ERJ170200LRSDR DALA1211940925Fastener · missingDURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABILIZER LEADING EDGE. LEADING EDGE SKIN/SPLICE WAS REPAIRED IAW ERA 500113-14AD REV ORIG.Feb 25, 2012 · N925DL · Doug MD88SDR IPXA12572088Panel · damagedINSPECTION TYPE: C, VERTICAL STAB PANEL, 322DL, HAS HOLES WITH EXPOSED COMPOSITE. REPAIRED PANEL 322DL IAW SRM 51-70-17-0G.Feb 9, 2012 · N456UP · Boeing 75724APFSDR DALA1206640925Fastener · missingDURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABLIZER LEADING EDGE REF EA 09-470871-12.Feb 7, 2012 · N925DL · Doug MD88SDR DALA1204039210Skin Panel · wornNR 173 STRAP REPAIR REQUIRED ON VERTICAL L/E IF MORE THAN 24 HOLES HAVE BEEN BUSHED PER SRM 55-30-05 REPAIR 9-1. REPAIRED PER SRM 55-30-05 FIG 6 AND BOEING DWG SG0955004. RII COMPLIED WITH. OPN 0501, NR 151, 154, 156, 157, 173 ALSO PART OF REPAIRS. ADDED WEJan 26, 2012 · N910DN · Doug MD9030SDR IPXA12M71742Panel · bentINSPECTION TYPE: 4C, PANEL 363AL IS BENT AND CRACKED. REPAIRED LOWER VERTICAL STAB PANEL 363AL REF STA-SA EA 011-5430-01- A3658 AND MD11-5530-46019-A.Jan 17, 2012 · N253UP · Doug MD11FSDR DALA1201280998Skin · damagedTOOLING DAMAGE ON RT VERTICAL STAB STA ZFS=56 DAMAGE. REPAIRED ON ERA 499262-14AD.Jan 10, 2012 · N998DL · Doug MD88SDR DALA1201270998Skin · damagedDURING PSV VISIT IN MSP, AN ELONGATED HOLE WAS FOUND ON RT SIDE OF STABILIZER L/E SKIN STA ZFS 56. FOUND WHILE ACCOMPLISHING OPS 1008. REPAIR ACCOMPLISHED ON ERA 499268-14AD.Jan 10, 2012 · N998DL · Doug MD88SDR DALA1170920929Skin · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR DOUBLER AND REPAIR STRAP STA ZFS=52.Dec 24, 2011 · N929DL · Doug MD88SDR DALA1170930929Skin · damagedDURING HMV ELONGATED REPAIR BUSHINGS WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE REPAIRED SKIN STA ZFS=52-55. WILL BE REPAIRED WITH ERA CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88SDR DALA1170900929Doubler · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE PREVIOUS EXTERNAL REPAIR DOUBLER STA ZFS=53. REPAIRED WITH AN ERA CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88SDR DALA1170890929Doubler · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR EXTERNAL DOUBLER AND SKIN STA ZFS=50-52. WILL BE A ERA REPAIR CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88SDR ZZDA2012021Skin · damagedBIRD STRIKE ON UPPER VERTICAL STAB L/E. CUT OUT DAMAGED SECTION OF UPPER CAP L/E SKIN AND RIB. ACCOMPLISHED DOUBLER AND FILLER REPAIRS PER EA 17-55-03636IR AND B717 SRM 55-00-00.Dec 22, 2011 · N970AT · Boeing 717200SDR AALA20111217TUL07Skin · damagedDURING RE-INSTALLATION OF UPPER VERTICAL STAB LEADING EDGE, 20 HOLES FROM ZFS 52 UP, ON LOWER LEFT SIDE WAS FOUND TO BE DAMAGED. INSTALLED REPAIR DOUBLER AND AERO-FAIRING PER EA 020952 AND SRM 55-03-00.Dec 17, 2011 · N9405T · Doug DC983SDR IPXA1570711Access Panel · dentedVERTICAL STABILIZER ACCESS PANEL 322AL IN DENTED FROM HAIL DAMAGE. REPAIRED IAW SRM 51-70-07-0G, USING 250 DEG CURE METHOD AS ALLOWED FOR PERMANENT REPAIR LISTEN IN FIG 201, TABLE 2 OF SRM 55-30-01-2R4.Dec 16, 2011 · N453UP · Boeing 75724APFSDR DALA1169570975Skin · damagedVERTICAL STABILIZER RT SIDE EXTERIOR SKIN DAMAGED AT SCREW HOLE ONE FASTENER ABOVE ZFS 52.267. NOTE: DAMAGE ON REMOVABLE LEADING EDGE SECTION P/N 5930610-3.Dec 14, 2011 · N975DL · Doug MD88SDR DALA1169580975Skin · damagedVERTICAL STAB LF SIDE EXTERIOR SKIN DAMAGE AT SCREW HOLE 3 FASTENER BELOW ZFS 52.267. NOTE: DAMAGE ON STABILIZER ROOT SECTION BELOW REMOVABLE LEADING EDGE.Dec 13, 2011 · N975DL · Doug MD88SDR DALA1169420975Skin · damagedDURING PSV VISIT IN MSP FOUND ELONGATED HOLE WHILE PERFORM ACJIC 0401. DAMAGED HOLE FOUND ON RIGHT SIDE OF THE VERTICAL STAB FRONT SPAR CHORD JUST ABOVE ZFS=52.267. DAMAGE REPAIRED PER ER/A 498509-14AD. WORKED ON NRC 89.Dec 13, 2011 · N975DL · Doug MD88SDR DALA1169410975Skin · damagedDURING PSV VISIT IN MSP FOUND VERTICAL LEADING EDGE FASTENER HOLE OUT OF LIMITS PER ACJIC 0401. ELONGATED HOLE IS ON A/C LEFT SIDE FRONT SPAR CHORD 3 FASTENERS BELOW ZFS=52.267. THIS IS REPAIRED PER ER/A 498510-14AD. WORKED ON NRC 90.Dec 13, 2011 · N975DL · Doug MD88SDR FDEA201111305092Panel · crackedLEFT AIR INTAKE DUCT REAR CENTER SPAR TO REAR SPAR LOWER PANEL (363PL) FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02 FIG.201 REPAIR 2 REV.48 REPAIR CLASSIFIED AS MAJOR AS GMM 6-2-100 REVISION 113.Nov 30, 2011 · N586FE · Doug MD11FSDR QMLD201111212663Skin · crackedA SMALL CRACK IS EVIDENT WHERE THE CAMLOCK FASTENER RIVETS INTERNALLY ON THE SPAR IN THE VERTICAL FIN.Nov 21, 2011 · N159LM · Urocop BK117C1EUROSDR DALA1163350928Fairing · wornDURING HMV WEAR WAS FOUND ON OUTER OF VERTICAL STABILIZER TIP FAIRING BETWEEN STA YV=200 AND 220 AT RT AND LT SIDE. BLEND OUT DAMAGE RT SIDE WITHIN LIMITS REF MD88 SRM 55-01 FIG 1 THE LT SIDE WAS REPAIRED IAW ERA 451447-14 REV A.Nov 15, 2011 · N928DL · Doug MD88SDR UALA2011111506254Panel · damagedPANEL DAMAGED TOP OF VERT FIN AT TRAILING EDGE FIRST PANEL FWD OF RUDDER LT SIDE. PANEL HAS INTERIM REPAIR INSTALLED. REF IPC55-36-01-02 AREA A ITEM 35 THIS IS A VERTICAL STABILIZER TO RUDDER "SEAL". THIS SEAL (PANEL) WAS DAMAGED IN FLIGHT DUE TO HARDWARE WNov 14, 2011 · N772UA · Boeing 777222SDR ABXA20111108139Skin · gougedVERTICAL STAB LOWER SKIN GOUGED ON RIGHT SIDE OF VERTICAL STAB FROM HORSE COLLAR. GOUGES ARE LOCATED JUST FWD AND AFT OF STA 1809 SKIN SPLICE. REMOVED DAMAGED SKIN PANELS, FABBED NEW SKIN PANELS FROM 7075T-6 .061 PER MMDS-04; SRM 53-80-01, FIGURE 201, REPAIRNov 8, 2011 · N742AX · Boeing 767232SDR CA111031002Skin · cracked(CAN) DURING SCHEDULED 12 YEARS INSPECTION, A CRACK WAS FOUND ON VERTICAL STABILIZER T/E SKIN. A SMALL PORTION STARTED TO EMERGE (.50" LONG) BUT AFTER DISASSEMBLY FOUND (6.0" LONG). THE CRACK STARTING AREA BETWEEN 2 PARTS (FIN SPAR & SPLICING PLATE) AND WAS NOct 31, 2011 · Snias AS350BASDR CWQR20111006022Skin · damagedDURING A SCHEDULED INSPECTION, TECH NOTICED 2 RIVETS MISSING FROM THE LT DORSAL SKIN AFT OF THE NACA SCOOP. THE LOWER FASTENER HOLE ALSO APPEARED TO HAVE A CRACK ABOUT AN INCH LONG AND MOVING TOWARDS THE SECOND FASTNER HOLE. UPON DISASSEMBLE WE ALSO FOUND CRAOct 6, 2011 · N580QS · Cessna 560XLSDR UALA2011093005303Tape · peelingON WALKAROUND CREW FOUND LEADING EDGE TAPE ON VERTICAL STAB PEELING. AREA IS APPROX 8 INCHES AND 5 FT FROM BOTTOM OF STAB. ALSO APPROX 18 FT FROM BOTTOM OF STAB PER MT55-003. REPAIRED EROSION TAPE. MT 55-003.Sep 30, 2011 · N444UA · Airbus A320232SDR FDEA201109224050Skin · crackedEMP - AFC RT DOGHOUSE ENTRANCE CUTOUT FOUND CRACKED AT INBD FWD CORNER. REPAIR DOUBLER FABRICATED AS PER SRM 53-70-02 FIG.201 REV 47 REPAIR DOUBLER INSTALLED AS PER SRM 51-33-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 22, 2011 · N619FE · Doug MD11FSDR USAA2011102400017Panel · delaminatedC3 CHECK - DELAMINATION ON VERTICAL STABILIZER TORQUE BOX PANEL BETWEEN FSS119.467 TO FSS270.784. REMOVED RIGHT TORQUE BOX PANEL VERTICAL STABILIZER & SENT PANEL TO OUTSIDE VENDOR FOR REPAIR. INSTALLED SERVICEABLE RIGHT TORQUE BOX PANEL IAW B757 SRM 51-40-02Sep 16, 2011 · N937UW · Boeing 7572B7SDR CWQR20110915021Skin · damagedDURING A SCHEDULED INSPECTION, FOUND 2 FASTENERS MISSING FROM THE LT SIDE OF THE DORSAL FIN ASSY. UPON FURTHER INSPECTION, FOUND THE FRESH AIR DUCT ASSY TO BE CRACKED IN 2 PLACES. IT APPEARS THAT THE CRACKED DUCT ASSY ALLOWED AIR PRESSURE TO EXPAND THE DORSAL Sep 15, 2011 · N565QS · Cessna 560XLSDR UIEA2011091900514Skin · damagedDURING VOR ANTENNA REPLACEMENT, DISCOVERED THE VERTICAL STABILIZER - FIN WL339.5 SUSTAINED LIGHTNING STRIKE CAUSING DAMAGE TO THE VOR ANTENNA AND TO THE RT SIDE OF THE VERTICAL STABILIZER EXTERNAL SKIN CONSISTING OF A HOLE/PUNCTURE MEASURING 1.3 INCHES DIAM. (Sep 15, 2011 · N522MC · Boeing 7472D7BSDR IPXA1M69059Skin · dentedLWR VERT STAB RT SIDE PANEL PN AJC7078-2 DENT D460282. REPAIRED IAW EO MD11-5530-43926-B PERM REPAIR D460282 CLEARED.Sep 4, 2011 · N292UP · Doug MD11FSDR ZZDA2011674Skin Panel · puncturedVERTICAL FIN LEADING EDGE TOP CAP SKIN PANEL, PUNCTURED. ACCOMPLISHED TOP CAP SKIN PANEL REPLACEMENT PER B717 SRM 51-41-02 AND 51-41-05.Aug 29, 2011 · N608AT · Boeing 717200SDR DALA1155699013Skin Panel · damagedDRILLED COUNTERSINK ON VERTICAL STABILIZER REMOVABLE LEADING EDGE HOLES. REAMED AND INSTALLED BUSHINGS AND DOUBLER IAW AMR0955182.Aug 27, 2011 · N913DE · Doug MD88SDR UIEA2011082700475Access Panel · damagedLEFT VERTICAL STABILIZER 324GL ACCESS PANEL HAS ELONGATED HOLES.Aug 27, 2011 · N780BA · Boeing 747409SDR USAA2011091500023Panel · delaminatedC3 CHECK - DELAMINATION ON LEFT FORWARD VERTICAL STABILIZER PANEL BETWEEN FSS 120-129 & FSS 155-175 APPROX 7 INCHES FROM LEADING EDGE OF PANEL. PANEL REMOVED SENT TO OUTSIDE VENDOR FOR REPAIR & REINSTALLED IAW B757 SRM 51-40-02-0G PAR 4 & 7 FIG 3, 6, 7, 8 & Aug 19, 2011 · N206UW · Boeing 7572B7SDR IXXA20110813001Skin · corrodedDURING ROUTINE C-CHECK INSP, FOUND VERTICAL STABILIZER RT LATERAL SKIN CORRODED AT STA ZR 35.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAAug 13, 2011 · N41CX · Doug DC862FSDR DALA1147699016Skin · damagedPER EA 09-470871-12 OPN 0801 STEP 3. SUBMIT SDR VERTICAL STAB LEADING EDGE SKIN REPAIR WAS ACCOMPLISHED PER THE REF EA.Aug 13, 2011 · N916DE · Doug MD88SDR UALA2011081004205Skin · damagedGOUGE ABOUT 8" LONG ON LEFT SIDE OF VERTICAL STAB ABOUT 6' UP FROM FUSELAGE. DAMAGE IS EXPOSED COMPOSITE DUE TO PAINT SEPARATION ON VERTICAL STAB AT ZONE 323 STA 299 DAMAGE IS AN UNEVEN AREA EXTENDED OVER 10" LONG AND 4" WIDE. MADE TEMPORRAY REPAIR PER SRM. Aug 9, 2011 · N455UA · Airbus A320232
Back to JASC 5532