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 06FDEA0312Skin · crackedVERTICAL FIN SKIN HAS POSSIBLE CRACK RT SIDE STR 10 ABOVE BODY TORQUE BOX BS 1342. REPAIRED RT VERTICAL FIN SKIN PER FED-EX E.A. 7-5540-96829.Jan 22, 2006 · N490FE · Boeing 727200SDR IXXA06SMN018SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT VERT STAB SKIN CORRODED, AT STA ZR 101.856. REMOVED LEVEL 1 CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. MEASURED: THICKNESS 0.025, BLEND OUT 0.002, REMAINING MATERIAL 0.023 FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 55-2-Jan 5, 2006 · N722CX · Doug DC872SDR CA051220003Skin · damagedDURING A SCHEDULED DESTRUCTIVE TEST, FOUND SOME STABILIZER SKINS DAMAGED WITH TOOL MARKS AT SOME INSERT HOLES.Dec 16, 2005 · Bell 206L4SDR CA051220002Skin · damagedDURING A SCHEDULED DESTRUCTIVE TEST, FOUND SOME STABILIZER SKINS DAMAGED WITH TOOL MARKS AT SOME INSERT HOLES.Dec 16, 2005 · Bell 407SDR AU510002148Panel · misinstalledVERTICAL STABILIZER RT LOWER PANEL INCORRECTLY FITTED BETWEEN FORWARD AND AFT ATTACHMENT POINTS.Dec 11, 2005 · Boeing 737476SDR DL75K050573Skin · puncturedGROUND DAMAGE OCCURRED TO VERTICAL STABILIZER, FWD TORQUE BOX, RIGHT, LOWER SKIN, JUST FWD OF THE STAB FRONT SPAR. DAMAGE CONSISTS OF PUNCTURE TO THE OUTER SKIN, CORE, AND INNER SKIN. REPAIRED PER DELTA ERA 450853-14.Sep 29, 2005 · N655DL · Boeing 757232SDR 05FDEA03116Panel · delaminatedVERTICAL STAB PNL 325DL DELAMINATED AT LOWER END SCREW HOLE.Sep 26, 2005 · N425FE · Airbus A310203SDR 05FDEA02866Skin · damagedDURING AIRPLANE' S CONVERSION FROM P TO F FOUND VERTICAL STABILIZER ON RUDDER RT SIDE STA ZFR 320.125, SEVERAL SWELLING THE SKIN. REPAIRED DAMAGED SECTION OF SKIN IAW 55-10-00 FIG 3 VOL I.Sep 14, 2005 · N571FE · Doug MD1010FSDR UPS05245266Skin · corrodedINSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND CORAug 6, 2005 · N919UP · Boeing 72730CSDR MHI2005F00000Skin · cracked(REF NR: 104942) DURING INSPECTION, FOUND THE UPPER STABILIZER FIN, RT LWR DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVET OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER. (K)Jul 21, 2005 · N406LH · Aerosp AS355F1SDR 05FDEA01809Skin · canningVERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BR. RIGHT I/B FLAP UPPER SKIN BETWEEN 140.6 TO 147.3, 03 EACH EXISTING DENTS SMOOTHENED OUT AND REPROTECTED AS PER SRM 51-21-01 VOL II, DEEPEST DENT IS 0.025", DIAMETER: 1/2" FOUND WITHIN LIMIT AS Jul 5, 2005 · N575FE · Doug MD11SDR 05FDEA01808Skin · canningVERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BL. REPAIR DOUBLER INSTALLED IAW SRM 51-35-01. [CLOSED]Jul 5, 2005 · N575FE · Doug MD11SDR 2005UALA00610Skin · lightning strikeLIGHTNING STRIKE ON VERT FIN RT SIDE BETWEEN RIB 10 AND UPPER LEADING EDGE. MAJOR REPAIR ACCOMPLISHED PER EVA 50378AJun 30, 2005 · N456UA · Airbus A320232SDR ABXA050115Skin · crackedVERTICAL STAB JUST ABOVE AFT TIP OF RUDDER, LEFT SIDE, CRACKED AND MISSING FASTENERS. REPAIRED AREA IAW DC-9 SRM 55-01.May 3, 2005 · N946AX · Doug DC931SDR USAA050502Skin · chafedCLT - FOUND SKIN CHAFED 1 INCH BY 1 INCH, UNDER LE OF DORSAL FIN. INSTALLED DOUBLER IAW EA 96445. (M)Apr 13, 2005 · N440US · Boeing 7374B7SDR ASAA0580204Skin · chafedOKC - FOUND DURING C-CHECK, VERTICAL STABILIZER SKIN CHAFED AT HORIZONTAL STABILIZER FAIRING. REPLACED DAMAGED SECTION. (M)Apr 4, 2005 · N950AS · Doug DC983SDR DHL2005740565Skin · dentedVERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF IS DENTED NEAR T/E. EVALUATED DENTED AREA AT VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF TRIM OUT DAMAGED SKIN SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3 AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.5"Mar 24, 2005 · N740DH · Boeing 7272Q9SDR DHL2005782543Skin · damagedREPLACE INTERIM REPAIR LOCATED ON THE RT VERTICAL STABILIZER BY REPLACING THE PANEL AFT OF THE REAR SPAR WITH A SERVICEABLE PANEL. REMOVED AND REPLACED VERTICAL STAB SKIN PANEL RT AFT OF THE REAR SPAR PN 6517561-234 PO NR 503010 IAW 727 SRM 51-30-2.Mar 15, 2005 · N782DH · Boeing 727227SDR GTIA050118Fairing · gougedVERT STAB TIP FAIRING HAVE SCRATCHED/GOUGED ON BOTH SIDE. BLENDED DAMAGED AREA AT VERT STAB MATERIAL LOSS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER IAW SRM 55-01 FIG 4. TREATED AND PRIMED, INSTALLED FILLER AND DOUBLER IAW SRM 51-30-Mar 10, 2005 · N821NK · Doug DC982SDR DHL2005782567Panel · dentedDURING AN A-CHECK, THE FOLLOWING DISCREPANCES WERE NOTED LWR VERTICAL PNL LT SIDE HAS 2 EA DENTS. CUT OUT DAMAGED AREAS APPROX 1 INCH ROUND AND 2 INCHES ROUND IAW B727 SRM 51-40-2 FIG 30, FABRICATED ONE FILLER 1 INCH ROUND AND ONE FILLER 2 INCHES ROUND AND ONMar 10, 2005 · N782DH · Boeing 727227SDR UPS05444193Skin · chafedINSPECTION TYPE:C VERTICAL FIN LT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH 2 LOCATIONS CHAFE BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT DEPTH 0.025 & 0.022 INCH. SKIN REPAIRED AT BS 2310-2360 STR 3L AREA AS PER SRM 53-30-03 FIG 1 & BS 2360 - 2380Mar 9, 2005 · N682UP · Boeing 747121SDR UPS05444192Skin · chafedINSPECTION TYPE:C VERTICAL FIN RT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH ONE LOCATION OF SKIN BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT 0.029 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A AT STA 2360 TO 2394 STR 3R AREA.Mar 9, 2005 · N682UP · Boeing 747121SDR 05FDEA00326Panel · dentedRT HORIZ STAB NR 5 BALANCE BAY UPPER SKIN PANEL HAS A SHARP PROTRUSION ON THE OTBD END. THE PANEL HAS CREASE ON O/B END. THE SRM REPAIRS FOR THIS PANEL ARE FOR CRACKS AND NOT DAMAGE OF THIS SIZE. (APPROX 3 INCH BY 1 1/2 INCH). FED-EX DRAWING SR27-55-0004 AMar 2, 2005 · N496FE · Boeing 727227SDR CA050225006Doubler · cracked(CAN) WHILE ACCOMPLISHING AD 80-19-14 STABILIZER FITTING INSPECTION, 2 CRACKS WERE NOTICED ON THE BOTTOM RIB P/N 220000-033 OF THE VERTICAL FIN. CRACKS ARE LOCATED INTHE REAR 90 DEGREE BEND OF THE RIB, RADIATING INWARDS FROM THE RADIUS CUT OUT. CRACKS WERE BOFeb 24, 2005 · Piper PA60600SDR ASAA0580089Panel · chafedOKC - DURING C-CHECK, VERTICAL STABILIZER PANEL 6308C IS CHAFED. REPLACED PANEL. (M)Feb 7, 2005 · N960AS · Doug DC983SDR C2XA05TY013Rivet · looseTYS, DURING A SCHEDULE INSPECTION, SMOKING RIVETS WHERE FOUND ON THE BASE OF THE VERTICAL STAB (LEFT AND RIGHT SIDES). MAINTENANCE REMOVED THE OLD RIVETS, FABRICATED AND INSTALLED DOUBLERS, (4 ON EACH SIDE) I/A/W-EC5510-01109, EMB145-SRM-51-40-02, IC2005-145/Feb 7, 2005 · N17928 · Emb EMB145ERSDR 2005UALA00107Skin · dentedVERTICAL STAB LEADING EDGE IS DENTED AT L/E STA 104. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR.Jan 30, 2005 · N302UA · Boeing 737322SDR 2006FA0000152Skin · delaminatedBOTH LT AND RT VENTRAL FINS SHOWED AREAS OF DELAMINATION ON FWD TOP CORNERS. DELAMINATION WAS BEYOND REPAIR LIMITS IAW SRM AND REQUIRED DER APPROVAL. FOUND INNER CORE MATERIAL WET DAMAGE WAS APPARENTLY CAUSED BY FREEZE CYCLES. WATER WAS FOUND ALONG TOP OF FJan 24, 2005 · N843E · Beech 1900DSDR 2004UALA01256Skin · dentedVERTICAL FIN L/E SKIN HAS A DENT AT LES 132. DENT IS 1.55 BY 0.046 INCH DEEP. DENT IS A ZONE 3 DENT. INSTALLED FLUSH REPAIR.Dec 27, 2004 · N306UA · Boeing 737322SDR CA050119004Skin · cracked(CAN) CRACK WAS FOUND AT VERTICAL FIN. THIS FIN WAS SENT TO MFG FOR REPAIR.Dec 13, 2004 · Snias AS350B3SDR DHL2004873551Skin · corrodedRT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 140.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R16, REV IR DATED 11-18-04 FAA FORM 8110-3 DATED 11-30-04. REMOVED L/E SKIN PANEL AND REPAIR PARTS FROM INTERNAL STRUCTURE IAW DWG W90-R16, SRM 51-1-Dec 1, 2004 · N873SJ · Doug DC873FSDR DHL2004873534Skin · corrodedLEFT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 98.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM LEFT VERTICAL STABILIZER, L/E STA ZFS 98.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRMNov 29, 2004 · N873SJ · Doug DC873FSDR DHL2004873532Skin · corrodedRIGHT VERTICAL STABILIZER L/E LWR SKIN CORRODED, STA ZFS 80.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM RIGHT VERTICAL STABILIZER L/E LWR SKIN STA ZFS 80.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF Nov 29, 2004 · N873SJ · Doug DC873FSDR CA041108005Skin · corroded(CAN) VERTICAL STABILIZER REMOVED TO ACCESS FUSELAGE SIDE SKIN REPLACEMENT (COSMETIC) WITH STABILIZER ON WORKBENCH, VISIBLE ACCESS TO INTERNAL STRUCTURE REVEALED CONSIDERABLE SURFACE CORROSION EVERY WHERE INTERNALLY. EXTERNAL UNIT LOOKS FINE. RECOMMEND REMONov 1, 2004 · Cessna 180CSDR COOSDR040043Panel · corrodedVERTICAL STABILIZER, LT SIDE PANEL CORRODED AND DELAMINATED, LOCATED FROM STA ZR 253.000 TO STA ZV 299.125. (K)Oct 15, 2004 · N825BX · Doug DC871FSDR IXXA060028SSkin · dentedDURING ROUTINE C CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED OUT OF LIMITS AT STATION ZFS149. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER, AND FASTENERS WET WITH SEALANT FROM STATOct 9, 2004 · N825BX · Doug DC871FSDR IXXA060031SSkin · corrodedDURING ROUTINE C CHECK, FOUND VERTICAL STABILIZER LEFT SIDE PANEL INTERNAL SKIN CORRODED BETWEEN STATION ZR253 AND STATION ZR299.125. REMOVED EXISTING STRUCTURE FROM DAMAGED PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS. LOCATED, DRILLED, TRIMMED, TREATED, Oct 3, 2004 · N825BX · Doug DC871FSDR IXXA060039SSkin · dentedDURING ROUTINE C-CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED AT STATION ZFS 121. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS WET WITH SEALANT FROM STATION ZFS 114.5 Sep 30, 2004 · N825BX · Doug DC871FSDR GTIA040835Skin · damagedSAS B0017605R00118; VERTICAL STABILIZER UPPER (VOR) L/E LOWER MOUNT HOLES, COUNTERSINKS BEYOND SKIN, OFF CENTER HOLES ELONGATED, INTERIOR SURFACE CHAFED. INSTALLED REPAIR DOUBLER IAW SRM 51-30-5, TOPCOATED IAW SRM 51-10-3, BLENDED OUT CHAFED AREA IAW SRM 55-Sep 30, 2004 · N823NK · Doug DC982SDR DHL2004780515Skin · dentedDURING A "C" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER FIN STA 157.5 (LT SIDE RUDDER). DENT FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-40-1. FABRICATED DOUBLER 2024T-3 .040 PO NR 9001359 4 1/2/ X 2 1/2 IAW B727 SRM 55-40-2 Sep 30, 2004 · N780DH · Boeing 727223SDR DHL2004780514Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER APPROX STA FIN 177 (LT SIDE RUDDER). DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-40-1 FABRICATED DOUBLER 2024T-3 .040 4.5 X 2.5 PO NR 9001359 IAW SRM 55-40-2 AND 55-20-3 TSep 30, 2004 · N780DH · Boeing 727223SDR ASAA0480515Skin · chafedOKC - C-CHECK, RT VERTICAL STAB LOWER SURFACE CHAFED IN 5 EA SPOTS INNER BANANA FAIRING PANEL 3802A, ATTACHMENT AREA. REMOVED DAMAGED SKINS, ORDERED AND INSTALLED NEW SKINS IAW SRM 51-30-2.Sep 24, 2004 · N973AS · Doug DC983SDR MALA040638Skin · dentedDURING 4Y/2Y INSPECTION IN BNA, NOTED 14 DENTS IN RT STAB TOP SKIN. DENTS ARE WITHIN ALLOWABLE LIMITS. CLUSTERS AT INBOARD AND REPAIRED IAW EO S55017. AIRCRAFT RETURNED TO SERVICE 9/11/2004.Sep 10, 2004 · N418XJ · Saab 340BSDR DHL2004745563Skin · delaminatedDURING A C-CHECK, RT VERT STAB LWR AFT AREA AT ABOUT STA 1381 (TRAPAZOID) COMPOSITE PANEL IS DELAMINATED AROUND PREVIOUS REPAIR. CUT OUT DELAMINATED AREA OF RT VERTICAL STAB TRAPAZOID PANEL AT PREVIOUS REPAIR APPROX 8 INCHES DIA, FABRICATED FILLER APPROX 8 INAug 20, 2004 · N745DH · Boeing 727224SDR DHL2004745562Skin · dentedDURING A C-CHECK, RT VERT STAB- RUDDER EXTERIOR SKIN (LWR RUDDER) AT ABOUT FIN STA 162.5 SKIN SURFACE HAS SEVERAL DENTED CREASES. FABRICATED DOUBLER 7 X 2 INCHES. TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON R/W VERT EXTERIOR SKIN LWAug 20, 2004 · N745DH · Boeing 727224SDR IXXA0500009SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION MAINTENANCE PERFORMED A MAJOR REPAIR ON VERTICAL STABILIZER L/E UPPER SKIN. FOUND CORROSION AT STA ZFS 179.000. REMOVED CORROSION FROM VERTICAL STABILIZER L/E UPPER SKIN STA ZFS 179.000 IAW DC8 SRM 51-1-8 PGS 17, 18. FOUNAug 18, 2004 · N606AL · Doug DC873FSDR P5CA0401159Panel · delaminatedHORIZONTAL STABLIZER RT PANEL NR 344 I/B DELAMINATED ON BACK SIDE. REMOVED AND BONDED AREA PER SRM 51-40-15.Aug 2, 2004 · N920FT · Boeing 747249FSDR DHL2004745521Panel · dentedDURING A C-CHECK, VERTICAL FIN BASE COMPOSITE PANEL LT SIDE BELOW AND FWD OF THE NR 2 ENGINE CHANGE FIXTURE CAVITY WITH DENTS. CUT OUT 3 EA SHARP DENTED AREAS APPROX 2.25 X .5 INCH, 2.25 X .5 INCH & 1 DIA. FABRICATED 2 EA FILLERS APPROX 2.25 X .5 INCH & 1 EAJul 6, 2004 · N745DH · Boeing 727224SDR COOSDR040007Panel · debondedVERTICAL STABILIZER TRAILING EDGE SECTION, UPPER AND LOWER PANELS WITH SKIN DEBONDING.Jun 30, 2004 · N41CX · Doug DC862FSDR SIMA200415413Skin · dentedABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON THE RIGHT SIDE OF THE VERTICAL STAB AND MBV INSPECTION. CUTOUT TWO DISBOND DENTS. THIRTEEN ABOVE VOR ANTENNA 6.0 AND 9.0 FORWARD OF TRAILING EDGE. FABRICATED TWO FILLERS, FILLER CUT OUT CORES WITH LY/HY 50May 26, 2004 · N388AE · Saab 340B
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