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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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 CARRIEDSDR DALA1222049261Skin · crackedDORSAL FIN FWD LOWER PANEL CUTOUT UPPER CORNER CRACKED. INSTALLED DOUBLER REPAIR PER SRM 51-70-01 VOL I.SDR 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 RSDR 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.SDR DALA1220280997Skin · crackedVERTICAL STAB REMOVABLE LEADING EDGE HAS CRACK INDICATION AT LOWER LEFT AFT CORNER HOLE. REPAIRED PER ERA501898-14AD REV ORIGINAL.SDR 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.SDR 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.SDR ASOA201200944Skin · dentedDURING BIRD STRIKE INSPECTION, FOUND DENTS IN VERTICAL STAB L/E. REPAIRED IAW SRM 51-40-11-001-001SDR 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.SDR 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.SDR 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 SDR 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.SDR IPXA12572088Panel · damagedINSPECTION TYPE: C, VERTICAL STAB PANEL, 322DL, HAS HOLES WITH EXPOSED COMPOSITE. REPAIRED PANEL 322DL IAW SRM 51-70-17-0G.SDR 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.SDR 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 WESDR 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.SDR DALA1201280998Skin · damagedTOOLING DAMAGE ON RT VERTICAL STAB STA ZFS=56 DAMAGE. REPAIRED ON ERA 499262-14AD.SDR 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.SDR DALA1170920929Skin · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR DOUBLER AND REPAIR STRAP STA ZFS=52.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR QMLD201111212663Skin · crackedA SMALL CRACK IS EVIDENT WHERE THE CAMLOCK FASTENER RIVETS INTERNALLY ON THE SPAR IN THE VERTICAL FIN.SDR 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.SDR 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 WSDR 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, REPAIRSDR 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 NSDR 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 CRASDR 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.SDR 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.SDR 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 51-40-02SDR 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 SDR 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. (SDR IPXA1M69059Skin · dentedLWR VERT STAB RT SIDE PANEL PN AJC7078-2 DENT D460282. REPAIRED IAW EO MD11-5530-43926-B PERM REPAIR D460282 CLEARED.SDR 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.SDR DALA1155699013Skin Panel · damagedDRILLED COUNTERSINK ON VERTICAL STABILIZER REMOVABLE LEADING EDGE HOLES. REAMED AND INSTALLED BUSHINGS AND DOUBLER IAW AMR0955182.SDR UIEA2011082700475Access Panel · damagedLEFT VERTICAL STABILIZER 324GL ACCESS PANEL HAS ELONGATED HOLES.SDR 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 & SDR 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 IASDR DALA1147699016Skin · damagedPER EA 09-470871-12 OPN 0801 STEP 3. SUBMIT SDR VERTICAL STAB LEADING EDGE SKIN REPAIR WAS ACCOMPLISHED PER THE REF EA.SDR 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.
Back to JASC 5532