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 ASAA0480431Panel · chafedDURING HV CHECK, FOUND RIGHT VERT STAB UNDER PANEL 3804A HAS CHAFED SURFACE. REMOVED DAMAGED SKIN PANEL AND INSTALLED NEW PANEL IAW 51-20-8. (M)SDR IXXA0400075SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND VERTICAL STAB LE HAS AN INTERM REPAIR STA ZFS 179.750. REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1, FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1 PG 17 FIG 4. CLEANED, TREATED AND PRIMED AREA ANDSDR ABXA040168Panel · crackedLT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. P/N: 5912188-49 AND -50.SDR UPS04842329Skin · crackedINSPECTION TYPE: C-1, LEFT HORIZONTAL STAB LEADING EDGE INBD OF CENTER 3 EACH POPPED RIVETS REMOVED & INSTALLED LT HORIZONTAL STAP L/E 331F TO FOM IAW DC8 SRM 51-3 -0. RMVD FASTENERS IAW DC8 SRM 51-1-21A. FOUND SKIN TO BE CRACKED. CUT OUT DAMAGE & FAB REPAISDR USAA040106Skin · damagedPIT - FOUND VERTICAL STABILIZER SKIN WITH 6 INCH REPAIR, 15 INCHES AFT OF FSS 170. COMPOSITE LAY UP REPAIR PER SRM 51-70-10. (M)SDR PCAA0403183Seal · looseREPORTED A VIBRATION IN CRUISE FLT. THE CREW ELECTED TO MAKE A PRECAUTIONARY LANDING AT WILLIAMSPORT DUE TO BEING OVERHEAD THE AIRPORT AT THE TIME. MAINTENANCE FOUND THE SEAL ON THE LEFT HAND SIDE OF THE VERTICAL STABILIZER TO HORIZONTAL STABILZER LOOSE. THE SSDR DL76S040225Panel · delaminatedVERTICAL STABILIZER LEFT LOWER PANEL ASSY, FWD TORQUE BOX FSS 12 - FSS 271 DELAMINATION. REPAIRED PER ER/A 088833-14.SDR GTIA040186Panel · crackedFTW - FOUND DORSAL FIN PANEL FORWARD 9 EACH FASTENER HOLES CRACKED, CHAFED, AND BROKEN OUT. FABRICATED DOUBLER. BLENDED OUT CRACKED AREAS. INSTALLED DOUBLER. (M)SDR ASAA0480076Skin · gougedOKC - DURING HV1-CHECK, FOUND VERTICAL STABILIZER SKIN GOUGED JUST ABOVE HORIZONTAL STABILIZER RIGHT PIVOT POINT. REPLACED SKIN PER SRM 51-30-1 AND 51-30-2. (M)SDR DHL2004806580Skin · corrodedVERTICAL STAB L/E HAS HOLES CORRODED STA ZFS 179.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG 3. TRIMMED OUT AND REMOSDR DL73S030984Panel · delaminatedFOUND ON W-1 LETTER CHECK, VERTICAL STAB COMPOSITE T/E PANEL DELAMINATED 2 PLACES LEFT SIDE, 1 PLACE RIGHT SIDE. REPAIRED PER SRM 55-30-3 FIG 3.SDR DHL2003807502Skin · damagedVERTICAL STAB INTERIM REPAIR ON L/E LEFT UPPER SIDE, STA ZFS 350.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4. CLEANED, TREATED AND PRIMED AREA AND INNSDR MWEA030391Skin · gougedLEFT SIDE OF VERTICAL STABILIZER SKIN UNDER VERTICAL TO HORIZONTAL STABILIZER, FAIRING HAS A GOUGE FROM TOP SKIN RADIUS EXTENDING DOWN AT 1.5 INCHES. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR AUS20030960Skin · cracked(AUS) VERTICAL STABILISER TIP SKIN CRACKED IN TWO PLACES ON RT SIDE. ONE CRACK WAS APPROXIMATELY 304.8MM IN LENGTH RUNNING VERTICALLY ALONG THE RIVET LINE JUST AFT OF STA YV157 APPROXIMATELY 12.7MM AFT OF HORIZONTAL STABILIZER RUB STRIP. THE SECOND CRACK WAS ASDR UPS03440997Skin · damagedON WALKAROUND INSPECTION FOUND DAMAGE (FROM WING PANEL DEPARTING) ON VERTICAL FIN LT SIDE DAMAGE APPROX 24 X 15 INCHES. ACCOMPLISHED INTERIM REPAIR TO VERTICAL STABILIZER PER EO B747-5100-19 029.SDR UPS03241063Panel · crackedINSPECTION TYPE: C, VERTICAL FIN LEADING EDGE LOWER PANEL 9501, MATING STRAP HAS A CRACK IN THE OUTER SKIN. CRACK STOP DRILLED IAW SRM 51-10-01, REPAIR DOUBLER FABRICATED IAW SRM 51-20-01, FIG 7. REPAIR DOUBLER INSTALLED IAW SRM 51-30-02.SDR DHL2003873556Skin · damagedVERTICAL STAB L/E EXTERNAL PLATING SHOWS INTERIM REPAIR AT ZFS.96.000 RT SIDE (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4, PG 17. REMOVED FASTENERS AND INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FSDR DHL2003873551Skin · damagedVERTICAL STAB L/E EXTERNAL SKIN SHOWS INTERIM REPAIR AT ZFS142.250. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FIG 4 PG 17.SDR DHL2003873547Skin · damagedVERTICAL STABILIZER L/E EXTERNAL SKIN SHOWS INTERIM REPAIR AT ZFS 110.700. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 FIG 4 PG 17. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AEA IAW SRM 51-1-8B. FABRICATED DOUBLER IAW SRM 55-2-1 FISDR C2XA03SH200Skin · damagedDURING C-CHECK THE VERTICAL STABILIZER LEADING EDGE WAS FOUND TO HAVE COMPOSITE DAMAGE. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 51-70-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR 2003F00487Skin · erodedAT C-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE WITH EROSION STATION 4869. REPAIRED VERTICAL STABILIZER IAW SRM 55-30-00, PATE 123. (M)SDR 226050303ASkin · cracked3 INCH CRACK FOUND ON LEFT SIDE OF VERTICAL STAB. CRACK LOCATED APPROXIAMATELY 1INCH FROM AFT CORNER OF VERTICAL STABILIZER GOING FORWARD.SDR 226050303Skin · cracked3 INCH CRACK FOUND ON LT SIDE OF VERTICAL STAB. CRACK LOCATED APPROXIMATELY 1 INCH FROM UPPER AFT CORNER OF VERTICAL STAB GOING FORWARD.SDR GTIA030271Panel · chafedFOUND RIGHT VERTICAL STAB ACCESS PANEL CHAFING ON INTERIOR. FABRICATED DOUBLER. LOCATED AND DRILLED DOUBLER. INSTALLED DOUBLER. (M)SDR P5CA0300869Panel · delaminatedVERTICAL STAB AUX SPAR PANEL FIN STA 395 TO FIN 420 DELAMINATED. REPAIRED PER SRM 51-30-02 BOEING PAO SIN 03-00011M.SDR CA030409013Structure · cracked(CAN) WHILE IN CRUISE FLIGHT THE PILOT NOTICED A YAW TO THE RIGHT. UPON LANDING HE NOTICED THAT THE TAIL FELT TWITCHY AND SHUTDOWN TO INVESTIGATE. WHEN HE GOT OUT HE NOTICED THE TOP HALF OF THE VERTICAL STABILIZER BENT OVER TO THE RIGHT HANGING ON BY THE RT SKSDR CALA0300153Skin · dentedINSPECTION FOUND VERTICAL STABILIZER LEADING EDGE SKIN DENTED AT L/E STA 132.92 + 6 AND AT 226.54 + 1.3. THE DENTED AREAS WERE REPAIRED IAW SRM 55-30-01, FIGURE 203.SDR ASAA0380268Skin · gougedOAK - ON 15K CHECK, VERTICAL STABILIZER SKIN GOUGED ON LEFT SIDE AT LOWER FORWARD END OF CUTOUT FOR HORIZONTAL STABILIZER. BLENDED GOUGE AND INSTALLED DOUBLER PER SRM 55-01. (M)SDR ASAA0380234Skin · gougedOKC - DURING 30K CHECK, FOUND RUDDER LEADING EDGE UPPER SKIN GOUGED AND CREASED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM. (M)SDR R7MR34649Structure · crackedRT CRACK, THREE WORKING RIVETS. SUSPECT IMPROPERLY SHIMMED AT FACTORY INSTALLATION. NO SHIMS FOUND AT REMOVAL OF FIN. REPLACED WITH NEW UNIT CORRECTED PROBLEM.SDR R7M2003F00000Skin · crackedRT CRACK, THREE WORKING RIVETS. SUSPECT IMPROPERLY SHIMMED AT FACTORY INSTALLATION. NO SHIMS FOUND AT REMOVAL OF FIN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR AWXA200300169Panel · delaminatedLCQ - MAJOR REPAIR - DURING C-09 CHECK A 64" X 32" AREA OF R/H VERTICAL STABILIZER FORWARD LOWER COMPOSITE SKIN PANEL WAS FOUND DELAMINATED AT VERTICAL FIN STA 105 - 175. MAINTENANCE REMOVED R/H VERTICAL STABILIZER FORWARD LOWER COMPOSITE SKIN PANEL AT VERTICASDR MWEA030041Skin · chafedLEFT SIDE OF VERTICAL STABILIZER IS CHAFED FROM LEADING EDGE OF HORIZONTAL STABILIZER RUB STRIP/SEAL. CUT OUT DAMAGE, INSTALLED INTERNAL TITANIUM DOUBLER AND FILLER.SDR CA021212004Skin · cracked(CAN) WHILE ACCOMPLISHING AN INSPECTION 2 CRACKS WERE NOTED EMANATING FROM A FASTENER HOLE IN THE VERTICAL STAB SKIN. THE CRACKS WERE 5/16 INCH AND 3/16 INCH IN LENGTH. THE CRACKS WERE LOCATED AT WL 25.1, 4 FASTENERS ABOVE THE SB 218 KIT DOUBLER (REF AD95-13-0SDR CA021212003Skin · cracked(CAN) DURING INSPECTION PRIOR TO INSTALLATION OF SB218 KIT (REF AD95-13-02) TWO CRACKS WERE NOTED ON THE RT VERTICAL STAB SKIN AT FS 409.65 WL 5.10 AND 4.10. TH CRACK LENGTHS WERE 5/16 OF AN INCH.SDR ASAA0280621Skin · gougedOAK - FOUND C-CHECK, VERTICAL STABILIZER SKIN GOUGED AT UPPER ATTACH POINT FOR ELEPHANT EAR FAIRING. REPLACED DAMAGED SKIN PER SRM 51-10-4, 51-10-3, AND 51-30-2. (M)SDR QXEA0201921Skin · damagedPDX - SCRATCHES AND GOUGES EXIST IN APERTURE V STAB UNDER PANEL 322DL. REPAIRED IAW DHC-8 200 SRM 51-20-36, PAGE 2, SECTION A, PARAGRAPH 6.SDR QXEA0201920Skin · damagedPDX - APERATURE HAS SCRATCHES ON V STAB UNDER PANEL 322GR. REPAIRED IAW DHC-8 200 SRM 51-20-36, PAGE 2, SECTION A, PARAGRAPH 6.SDR QXEA0201919Skin · damagedPDX - SCRATCHES AND GOUGES EXIST IN APERTURE OV V-STAB UNDER PANEL 322HR. REPAIRED IAW DHC-8 200 SRM 51-20-36, PAGED 2, SECTION A, PARAGRAPH 6.SDR GTIA021201Skin · crackedFTW - FOUND FIN ASSEMBLY VERTICAL STABILIZER LOWER LEADING EDGE SKIN 5912188-35 ANGLE CRACK ON SKIN AT RIGHT FORWARD LOWER HOLE AT ZFS=26.812. REMOVED DAMAGED SKIN AREA. FABRICATED REPLACEMENT SKIN AND SPLICE. INSTALLED SKIN AND SPLICE. (M)SDR CA021029006Skin · cracked(CAN) DURING A 30 DAY INSPECTION IT WAS NOTED THAT THE VERTICAL STAB SKIN WAS CRACKED ON THE STARBOARD SIDE OF THE VERTICAL STABILIZER. THE CRACK IS LOCATED AT APPROXIMATELY VS STA 9.1 AND IS 1 INCH IN LENGTH. THE CRACK IS RUNING FORE AND AFT. THE AIRCRAFT WILSDR CA021016035Skin · cracked(CAN) PHASE 49 SKIN JOINT EDDY CURRENT INSPECTION INDICATED AN ANAMOLY AT FS 287.78 WL 146.6. FURTHER INVESTIGATION USING A 5000X MICROSCOPE REVEALED A 1 INCH LONG GOUGE AND CRACK IN SKIN DOUBLER BETWEEN SKIN EDGES. AIRCRAFT FERRIED UNPRESSURISED TO WICHITA CISDR AALA20021372Skin · damagedTUL - FOUND 19 FASTENERS LOOSE/PULLING THROUGH SKIN JUST ABOVE INTAKE AT BASE OF VERITCAL STABILIZER, ZFS 11.562. INSTALLED DOUBLER STRAPS PER ESO 80559. (M)SDR QXEA0201276Skin · dentedPDX- SKIN DENT DAMAGE BETWEEN FRAME NR 3, FRONT SPAR AND STRINGERS 28S-28P IN THE VERTICAL STABILIZER. REPAIRED IAW HORIZON AIR EA 2-55-69 -A-. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CALA0200434Skin · gougedINSPECTION FOUND THAT THE LEADING EDGE OF BOTTOM L/H BANANA FAIRING HAD GOUGED SKIN OF VERTICAL STABILIZER. THE LEADING EDGE PLATING WAS REMOVED AND REPLACED IAW SRM 53-30-0.SDR 02FDEA00532Panel · missingON POST FLIGHT INSPECTION FOUND SLIDE PANEL ON RIGHT SIDE OF VERTICAL STAB MISSING. FOUND HINGE ASSY TORN & BROKEN. REMOVED REMAINDER OF HINGE ASSY. ALSO NOTED FORWARD SLIDER TRACK HAS SECTION TORN OUT AND AFT TRACK WAS BENT. NOTED AFT HONEY COMB PANEL A DSDR DL72S020860Skin · crackedTHE LT BOX SKIN OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK EMANATING FROM A FASTENER COMMON TO THE REAR SPAR LOCATED 1 INCH ABOVE THE FUSELAGE SKIN INTERFACE. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383575-14,SDR DL72S020828Skin · crackedFOUND ON E-1 LETTER CK SKIN CRACKED AT BASE OF VERTICAL STAB RT SIDE ABOVE FWD END OF NUMBER 2 ENG CUTOUT AT STR 10. REPAIR PER MM 55-30-000-8.SDR SIMA200219126Skin · dentedVERTICAL STABILIZER RIGHT UPPER AREA HAS ONE DENT. PERFORMED EDDY CURRENT AND SONIC BOND CHECK. NO DEFECTS NOTED. DENT FOUND TO BE WITHIN SAAB 340 SRM 55-70-10 AND 51-10-10 LIMITS. (M)SDR 02FDEA00409Skin · corrodedWIDESPREAD CORROSION ON FUSELAGE SKIN ON THE OUTBOARD SIDES OF THE VERTICAL STAB LT & RT ATTACHMENT. R/R ALL TRACES OF CORROSION.
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