JASC 5532
Service difficulty reports · 1,754
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 USAA970104Panel · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK AFT OF REAR SPAR, 18 INCH BELOW NR 4 RUDDER HINGE VERTICAL STABILIZER PANEL. INSTALLED DOUBLER, REPAIRED PER EA 42154. (M)SDR USAA970103Panel · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG CRACK RIGHT SIDE VERTICAL STABILIZER 18 INCH BELOW NR 4 HINGE STRUCTURAL PANEL. INSTALLED REPAIR DOUBLER, REPAIRED PER EA 42154. (M)SDR ABXA9700301Skin · crackedDURING C INSPECTION, FOUND THE VERTICAL STABILIZER SKIN GOUGED, CRACKED AND PUNCTURED ON RIGHT SIDE NEAR THE JACK SCREW. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-10-8.SDR ABXA9700338Skin · chafedDURING C INSPECTION, FOUND A GROOVE CHAFED INTO THE LEFT SKIN ON THE VERTICAL STAB NEAR THE FAIRING ATTACH BRACKET. REPLACED VERTICAL STAB SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.SDR UPS97822362Skin · corrodedINSPECTION TYPE-C, VERT STAB LE RT CORROSION BLEND OUT IS BEYOND LIMITS, ZFS 140. REMOVED DAMAGE, FABRICATED FILLER, DOUBLER AND INSTALLED IAW SRM 55-2-1, 55-30-01 AND 51-1-11.SDR DL72S970402Skin · crackedFOUND A 1 INCH CRACK ON THE VERTICAL STAB SKIN LT SIDE BELOW LOWER VORTEX GENERATOR. REPAIRED PER MM 55-30-0.SDR 97ZZZX2704Skin · delaminatedDURING POST-FLIGHT, NOTICED SKIN DELAMINATION ON THE INBOARD/LOWER PART OF THE LEFT ELEVATOR (ABOUT ONE-THIRD OF THE BOTTOM IN LENGTH). ALSO, ABOUT 4 INCHES IN DIAMETER IN THE OUTBOARD/LOWER SECTION OF THE SAME ELEVATOR.SDR CALA9700481Skin · crackedINSPECTION FOUND A .25 INCH CRACK JUST FORWARD OF RT FAN COWL HINGE AREA IN VERTICAL STABILIZER SKIN PANEL. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-33-01, 55-00-01 AND 51-31-01.SDR USAA970044Skin · crackedPIT - DURING B-CHECK, FOUND 1.5 INCH CRACK IN VETICAL SKIN PANEL AT LEFT SIDE, VERTICAL STABILIZER SKIN, BENEATH DRAG ANGLE. REPAIRED DOUBLER .032 TITANIUM PER EA 46218. (M)SDR 9700329956Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE RIGHT SIDE OF VERTICAL STABILIZER TAIL SECTION AFT OF ELEVATOR SECTORS. REPAIRED PER EA 99-111991.SDR USAA960792Skin · gougedPIT - DURING Q-1 CHECK, FOUND 1.125 INCH LONG, .1875 INCH WIDE (AT TOP) .09375 INCH WIDE (AT BOTTOM) .029 INCH DEEP GOUGES AT LEFT SIDE OF THE VERTICAL STAB SKIN AT RIB 5.0 AND RIB 3.6. BURNISHED GOUGE AREAS AND INSTALLED AN EXTERNAL DOUBLER PER EA 34175. (MSDR 9627621153Skin · delaminatedDURING PERIODIC CHECK, DELAMINATION OF THE VERTICAL STABILIZER SKIN AT STR 375 TO 405 RIGHT SIDE. REPAIRED PER EA 11-120122 (P/N ANC7047-2).SDR CALA9700395Panel · gougedINSPECTION FOUND A GOUGE AT CORNER EDGE OF VERTICAL STABILIZER ACCESS PANEL NR 373EL. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-00-01, FIGURE 3 AND 51-21-01.SDR 97ZZZX712Skin · corrodedFOUND HEAVY TO SEVERE CORROSION, POPPED RIVETS, THROUGHOUT THE VERT FIN. CESSNA DID NOT PRIME ANY INTERNAL PARTS DURING MANUFACTURE RESULTING IN AN UNSAFE CONDITION. REPLACED PART, CLEANED, TREATED, AND PRIMED WITH EPOXY PRIMER. RECOMMEND CESSNA DO LIKEWISESDR ABXA9700193Panel · chafedDURING C-CHECK, VERTICAL STABILIZER SKIN PANEL WAS FOUND CHAFED NEXT TO HORIZONTAL STABILIZER, NR CF-818. REPLACED THE SKIN PANEL IAW DC-9 SRM 51-10-4.SDR 97ZZZX1764Skin · chafedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LT VERTICAL SKIN CHAFED AT BANNANA FAIRING. BLENDED OUT CHAFE MARKS IAW DC9 SRM 51-10-3. VERIFIED OUT OF LIMITS PER DC9 SRM 55-01 FIG 1. REMOVED PANEL IAW DC9 SRM 51-30-2. FABBED NEW SKIN (SDR TSAA9655093Skin · corrodedDURING C-CHECK VISIT, CORROSION NOTED ON VERTICAL STABILIZER LEFT SIDE BETWEEN FS 111 - FS 113. REPAIRED PER ECO 2509 R2. AIRCRAFT RETURNED TO SERVICE. (M)SDR MWEA96626Skin · chafedDURING C-CHECK, FOUND LT VERTICAL STABILIZER SKIN GOUGED UPPER AND LOWER SECTIONS WHERE FAIRINGS CHAFING. REPLACED UPPER AND LOWER SKIN SECTIONS IAW SRM 51-30-2.SDR ZIAA961122Skin · corrodedMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED VERT STAB LT SKIN CORRODED. ZR45. REPAIRED IAW DWG A74-R29; SRM 51-1-8. (X)SDR ZIAA96069Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. VERT STAB EXT LT SKIN, LT ATTACH ANGLE. RT SKIN ZR 225, RT SKIN ZR 270. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR CA970311052Vertical Fin · cracked(CAN) CRACK IN RIGHT HAND TRAILING EDGE SKIN AND FORWARD UPPER CASTING MOUNT. EXCESSIVE GAP (3MM) WHEN ATTACHED. BOLT HOLES IN CASTING MOUNT ELONGATED.SDR DL72L962142Skin · crackedA .25 INCH CRACK AT FASTENER HOLE LT SIDE OF VERT STAB AT BASE AT STR 10L. INSTALLED DOUBLER PER MM 55-30-0 PG 801.SDR COEA9672002Skin · dentedUPON ARRIVAL INTO SBA FROM ONT, MECHANIC OBSERVED BLOOD ON THE VERTICAL STABILIZER LEADING EDGE WHILE PERFORMING THE WALK AROUND. MAINTENANCE DISCOVERED A DENT FROM AN APPARENT BIRD STRIKE. THE STRUCTURAL DAMAGE EXCEEDS SRM PARAMETERS. PARTS ARE CURRENTLY ESDR AALA961359Skin · crackedTUL - FOUND CRACK IN SKIN RIGHT SIDE OF VERT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 55-30-07-1 PG 3. (M)SDR MWEA96511Skin · chafedDURING INSP, BOTH LT AND RT SIDES OF VERT STAB CANOE FWD END EXTERNAL SKINS WERE HEAVILY CHAFED FROM THE FAIRINGS. REPLACED THE SKINS IAW SRM 55-31-0.SDR MWEA96497Skin · chafedDURING INSP, LT AND RT SIDES OF THE VERTICAL STAB CANOE AFT END EXTERNAL SKINS WERE HEAVILY CHAFED FROM THE FAIRINGS. REPLACED SKINS IAW SRM 55-31-0.SDR P5CA9600718Skin · delaminatedROUGH REPAIL LIFTED OUT, DELAMINATED ON RIGHT VERTICAL STABLIZER LOWER SKIN. REPAIRED AREA PER BAC SRM 51-40-06.SDR CALA9601155Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN RT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 180, STRINGER 7. THE CRACKED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-30-3, FIGURE 1.SDR CALA9601157Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF LEFT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 157 BETWEEN STRINGER S 4 AND 5. THE CRACKED SECTION OF SKIN WAS REMOVED IAW SRM 55-30-3. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3 AND SRSDR UPS96220806Skin · corrosionINSPECTION TYPE SI, CORROSION AROUND FASTENERS ON LT FIN MIDSPAR AT FIN STA 194 TO FIN STA 210. REPAIRED LT SKIN AT FIN STA 194 TO FIN STA 210.SDR CALA9601156Skin · crackedINSPECTION FOUND TWO .25 INCH CRACKS AT FASTENER HOLES IN RIGHT SIDE VERTICAL STABILIZER EXTERNAL SKIN JUST BELOW PANEL 9516. THE PANEL WAS REMOVED FOR ACCESS. THE CRACKED SKIN WAS CUT OUT IAW SRM 54-30-3. REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTSDR USAA960598Skin · chafedYYC - DURING FC-06 CHECK, FOUND CHAF IN SKIN LEFT SIDE 4.5 INCH BY 2 INCH AND RIGHT SIDE 2.75 INCH BY 1.25 INCH FORWARD OF INTERIM SPAR 2 OF RIB 5, LEFT AND RIGHT SIDE OF VERT STAB TORSION BOX. AREAS BLENDED, FILLED, AND REPAIR PATCHES INSTALLED PER FOKKER FASDR MALA965033Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT VERTICAL STABILIZER SKIN CRACKED AFT OF THE CUT OUT FOR THE HORIZONTAL STABILIZER SPAR. PERFORMED REPAIR TO RIGHT VERTICAL STAB SKIN BY REMOVAL OF PREVIOUS REPAIR. STOP DRILLED NEW CRACK. FABSDR DL72W961309Skin · crackedTWO, .75 INCH CRACKS IN VERTICAL STAB SKIN FWD OF SADDLE PANEL RT SIDE ABOVE PANEL 9516. REPAIRED PER M/M 54-30-0.SDR DL72W961257Skin · crackedFOUND DURING A-2 LETTER CHECK, TWO .25 INCH CRACKS AT CONSECUTIVE RIVET HOLES LT SIDE OF VERT STAB 10 FT AFT OF NR 2 ENG INLET. REPAIRED PER M/M 54-30-0 FIG 801.SDR MALA964987Skin · crackedMSP - DURING AN INSPECTION, MAINTENANCE FOUND 3 CRACKS IN RT VERTICAL STABILIZER SKIN ALONG FORWARD AUXILIARY SPAR RIVETS MEASURING .380 INCH AT WL 140.0, .880 INCH AT WL 144.0, .750 INCH AT WL 148.0. REPAIRS WERE COMPLETED BY STOP DRILLING CRACKS AND INSTALLSDR EISA96090Trailing Edge · separationVERTICAL STABILIZER TRAILING EDGE, JUST ABOVE RUDDER TAB, AREA STARTING TO SEPARATE. CUT OUT DAMAGE AND ACCOMPLISHED FIBERGLASS REPAIR PER SRM 51-40-06. (M)SDR DL72L961069Skin · cracked.75 INCH CRACK EXTENDING FROM RIVET HOLE AT LT VERTICAL STABILIZER SKIN 6 INCHES FORWARD OF FRONT SPAR BASE. REPAIRED PER M/M 54-30-0, PG 801.SDR CKSA96044Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER SKIN SEPARATING AND CORRODED, VERTICAL STABILIZER RIGHT SIDE APPROXIMATELY STA XR284 TO XR230 AFT SPAR AREA. LEVEL 2 TASK NR 61999. REPLACED UPPESDR CKSA96043Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER, VERTICAL STABILIZER SKIN LEFT SIDE APPROXIMATELY STA XR230 TO XR310 AFT SPAR AREA CORRODED AND SEPARATING. LEVEL 2 TASK NR 61998. RESEALED BONDESDR EISA96040Skin · debondedLEFT ELEVATOR INBOARD TRAILING EDGE IS STARTING TO SEPARATE. CLEANED AREA BONDED WITH A-B STRUCTURAL ADHESIVE REPAIR PER 51-40-06. (M)SDR 96ZZZX2630Skin · corrodedDURING C-CHECK, FOUND VERTICAL FIN, RT FORWARD EDGE WITH CORROSION ON SKIN AND SCREWS. REMOVED DAMAGED AREA AND FABRICATED DOUBLER PER SRM 53-2-1. INSTALLED DOUBLER PER SRM 53-2-1. REF: OPERATOR CONTROL NR 0683.SDR 96ZZZX2629Skin · corrodedDURING C-CHECK, FOUND VERTICAL STABILIZER, L/E CORRODED AT APPROXIMATELY STA 179.750. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 55-2-1, TREATED AND PRIMED IAW 51-1-8. SEALED AREA IAW SRM 51-1-16. REF: OPERATOR CONTROL NR 1707.SDR IXXA9668Le Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND ON THE VERTICAL STABILIZER LEADING EDGE. DAMAGE WAS AT STA ZFS 173, RIGHT, ATTACHMENT SCREW HOLE. THE CORROSION WAS REMOVED, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW WITH THE AIRCRAFT SRM 5SDR CAL960496Skin · crackedGSO - INSPECTION FOUND A 4 INCH BY 2 INCH HOLE AND SEVERAL CRACKS TOTALING 12 INCHES IN LENGTH IN SKIN PANEL ABOVE RUDDER ON RIGHT SIDE OF VERTICAL STABILIZER. THE DAMAGED SKIN WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-SDR MWEA96086Skin · gougedFOUND VERTICAL STAB SKIN LT SIDE UPPER FWD SURFACE HAS SEVERAL DEEP GOUGES. INSTALLED REPAIR IAW SRM 55-01 PG 1.SDR DL72W960611Skin · crackedFOUND DURING E-2 LETTER CHECK - 2 EA, .25 INCH CRACKS EXTENDING FROM RIVET HOLES, RT VERTICAL STAB SKIN, JUST BELOW SADDLE PLATE 9501. REPAIRED PER M/M 54-30-0.SDR UPS96805853Skin · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STABILIZER T/E, BOTH SIDES HAVE CORROSION BETWEEN NR 4 RUDDER SUPPORT FITTING. REPLACED SKIN PANEL BY REBONDING NEW ONES IAW SRM 51-1-19.SDR DL72S960396Skin · crackedA 1 INCH CRACK AT CENTER ENGINE INLET HOUSING OUTER SKIN BELOW PANEL 9523. REPAIRED PER MM 54-30-0.SDR E9WASkin · damagedCLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STATION 218 RIGHT TRAILING EDGE PANEL. COMPOSITE REPAIRED AS PER BOEING SRM 51-40-13. (M)
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