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 CALA9901294Panel · crackedINSPECTION FOUND A 3 CRACK IN VERTICAL STABILIZER PANEL ON LT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, SHEET 2, 51-60-0, PAGE 5, 51-30-5, AND 51-30-2.SDR CALA9901200Panel · crackedINSPECTION FOUND CRACKS IN VERTICAL STABILIZER PANEL NR 6404. THE CRACKS WERE 1-2 INCHES LONG. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901199Skin · puncturedINSPECTION FOUND A HOLE THROUGH SKIN AND RIB OF VERTICAL STABILIZER AFT UPPER STRINGER TIP FAIRING. THE RIB AND SKIN WERE REPAIRED IAW SRM 55-01, FIGURES 2 & 4.SDR DL72L991931Skin · crackedTHE VERT STAB LT SKIN WAS FOUND CRACKED WITH A TIME LIMITED REPAIR LOCATED AT BS 1203 WL 295. THE RESULTANT TRIM OUT IS APPROX 1.25 IN DIAMETER. REPAIRED PER ERA 333479-14, REV C.SDR SWAA991416Skin · crackedDURING SCHEDULED D CHECK, FOUND LT SIDE OF VERTICAL STAB SKIN CRACKED, STA 91, JUST AFT OF FRONT SPAR. REPAIRED SKIN PER SRM.SDR DHL9972709CSkin · elongated holesAT C CHECK, FASTENER HOLES ELONGATED ON RT SIDE VERTICAL FIN L/E PANEL NR 9601. REPLACED PANEL ON LEFT SIDE VERTICAL FIN L/E USING 2024T3 .040 PER B727 SRM 51-30-2 20 X 15 N/R 4388.SDR DL72S991777Skin · crackedTHE SKIN ON THE RIGHT SIDE OF THE VERTICAL STABILIZER WAS FOUND CRACKED BETWEEN FS 1203 AND 1211. THIS DAMAGE WAS REPAIRED PER ERA 333422-14.SDR DL72S991773Skin · crackedTHE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT THE FRONT SPAR WHERE THE TORQUE BOX ATTACHES ON THE LEFT HAND SIDE. THE CRACK WAS FOUND AT HMV AND WAS REPAIRED PER ER/A 333420-14.SDR SWAA991268Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STAB CRACKED ON RT SIDE FIN STA 126.3, FWD OF VERTICAL TRAILING EDGE ON REAR SPAR CHORD SKIN. REPAIRED CHORD SKIN PER SWA RA NR 1-255-0306.SDR UF6A990776Skin · crackedSBN - THE LEFT SIDE OF THE VERTICAL STABILIZER IS CRACKED AT THE LOWER CORNER NEAR THE RECESS AREA FOR THE RUDDER, LOCATED BY THE BOTTOM HINGE. MAINTENANCE FABRICATED NEW SKIN PER SAMPLE WITH 2024T3 .020 INCH AND REPLACED DAMAGED AREA. ALL WORK WAS DONE IAW SDR UF6A990775Skin · crackedSBN - THE LEFT SIDE OF THE VERTICAL STABILIZER IS CRACKED AT THE TRAILING EDGE ABOVE RIB 29.53. MAINTENANCE FABRICATED NEW SKIN PER SAMPLE WITH 2024T3 .020 INCH AND REPLACED DAMAGED AREA. ALL WORK WAS DONE IAW WITH BAE ATP SRM 55-30-00, 51-10-00, AND 51-40-0SDR UF6A990770Skin · crackedSBN - THE VERTICAL STABILIZER NEAR ACCESS PANEL 321AL IS CRACKED. MAINTENANCE REMOVED DAMAGED AREA AND FABRICATED NEW SKIN WITH 2024T3 .050 AND INSTALLED. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-131. (M)SDR QXEA9901630Panel · gougedPDX - RECESSED AREA FOR ACCESS PANEL 322FR IS GOUGED ON LOWER FORWARD CORNER. REPAIRED IAW DHC8 SRM 55-30-16.SDR DHL9970308CPanel · crackedAT C CHECK, V STAB ACCESS PANEL NR 9774 HAS REPAIRS CRACKING UP L/S. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1 USING RESIN 1304, 6 INCH BY 4 INCH, N/R 4128.SDR CALA9900833Panel · corrodedINSPECTION FOUND VERTICAL STABILIZER L/E PANEL THIRD FROM THE BOTTOM CORRODED. THE CORROSION WAS REMOVED IAW EA 10-5533-2-A0440 AND ECRA 5533-01001.SDR UF6A990712Skin · damagedSBN - PIN HOLE VERTICAL STABILIZER AT STATION 351.75. MAINTENANCE REPAIRED THE HOLE IAW BAE SRM 51-60-01. (M)SDR EIA990241Panel · disbondedHKG - DURING C/D CHECK, VERTICAL STABILIZER T/E CAVITY ACCESS PANEL 324FL FOUND DISBONDED. ACCOMPLISHED A TIME LIMITED REPAIR PER RS-R-55-10-34113. (M)SDR CA990707049Skin · cracked(CAN) TWO CRACKS FOUND IN VERTICAL STABILIZER SKIN AT TOP RT REAR SPAR RIVET. REPAIR CARRIED OUT PER PILATUS DRAWING.SDR GTIA9901053Skin · misrepairedMHV - VERTICAL STABILIZER L/E ASSY AT STATION 2 FS 52.300 THERE IS AN EXISTING REPAIR THAT IS BLENDED AND FILLED WITH EPOXY 4 COUNTER SINKS BONDO HAS FALLEN OUT. CUT OFF BONDED FINGER DOUBLER FABRICATED TITANIUM REPAIR DOUBLER PER ENG G INSTRUCTION (DRAWING) SDR MZZA99121Skin · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RIGHT VERTICAL STABILIZER SKIN WAS FOUND CRACKED JUST AFT TO THE BS 1183 BULKHEAD AT APPROX WL 302. NO ADDITIONAL REWORK OF THE CRACK IS NECESSARY DUE TO WITHIN LIMIT. ISSUE A DIP NR CM558 TO INSPECTSDR GTIA9901019Panel · misalignedMHV - REPLACEMENT VERTICAL UPPER CENTER PANEL PN 9911940-403 ATTACH HOLES DO NOT ALIGN WITH AIRCRAFT STRUCTURE. FABED IN REF TO DC9 SRM 51-10 MANUFACTURED FOLLOWING ITEMS. 2 EACH CHANNELS 1 EA RT. 1 EACH LT. 2 INCH Z-CLIPS, 1 EACH RT, 1 EACH LT. 2 BULKHEASDR GTIA9901018Panel · crackedMHV - VERTICAL STABILIZER CENTER PANEL UPPER, PN 9911940-403, HAS CRACK RT AFT SIDE APPROXIMATELY 8 INCHES LONG. CENTER PANEL REPAIR AND INSTALLATION TO BE ACCOMPLISHED ON A092-A03-N065. (X)SDR GTIA9901011Panel · misalignedMHV - VERTICAL CENTER PANEL UPPER P/N 9911940-403 WHICH WAS REPLACED ON W/C NO062 HAS ATTACHING HOLES MISALIGNING WITH MATING HOLES ON VERT STRUT. PER ENG DWG NR 9909001 INSTALLATION COMPLETE PARTS FAB ON W/C A092-B10-N067 BRACKETS, CHANNELS, STRAPS ALL INSTASDR AU990585Skin · corroded(AUS) VERTICAL STABILIZER SKIN CORRODED INTERNALLY.SDR UPS99229651Skin · looseINSPECTION TYPE:C, VERTICAL STAB LT SIDE, SKIN LOOSE ADJACENT FASTENERS STR 57 AREA BELOW STAB GEARBOX FWD CUTOUT. REPAIR CARRIED OUT IAW SRM 55-30-5 FIG 4.SDR UPS99829390Skin · corrodedINSPECTION TYPE:C3 VERTICAL STAB L/E SKIN AT ZFS 30.5 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1 FIG 4.SDR EISA99090Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND VERTICAL STABILIZER SKIN CRACKED ON LEFT SIDE JUST BELOW SLIDING SEAL TRACK. STOP DRILLED CRACK PER SRM 55-30-3. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 55-30-3. (M)SDR HEEA061574Skin · damagedVERTICAL FIN HAD DEEP SCRATCHES ALONG LEADING EDGES AND TRAILING EDGES.SDR HEEA061573Skin · corrodedVERTICAL FIN CORRODED AND SEPARATED.SDR ASAA9910043Skin · dentedPHX - DURING D-CHECK, FOUND THE RIGHT SIDE OF THE VERTICAL STABILIZER DENTED 10 INCHES ABOVE PITOT TUBE FIN STATION 81.1. REPAIRED PER SRM 5530-30-3. (M)SDR QXEA9900943Skin · dentedPDX - DENT ON LEFT SIDE OF VERTICAL STAB AFT OF LEADING EDGE. REPAIRED IAW HORIZON AIR EA 4-55-122.SDR QXEA9900713Doubler · corrodedPDX - AFT CARGO BAY, THERE IS CORROSION ON AND IN THE NR 3 VHF COMM DOUBLER AND STIFFENER, LOCATED BETWEEN FRAMES 15635, 15205 AND STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C.SDR DHL9980707CPanel · crackedAT C-CHECK, VERTICAL STAB T/E AREA STA 195 REAR SPAR METAL COVER CRACKED. STOP DRILLED END OF CRACK, FABRICATED DOUBLER REPAIR 3 X 3 AND INSTALLED PER SRM 51-1-21.SDR DHL9980706CPanel · crackedAT C-CHECK, VERTICAL STABILIZER T/E AT STA 225 REAR SPAR COVER PANEL CRACKED. REMOVED PANEL, STOP DRILLED AND INSTALLED FIBREGLASS REPAIR PER SRM 51-3-0.SDR 99T64R379ARSkin · corrodedNR 066 - CORROSION ON VERTICAL STABILIZER UPPER AND LOWER ATTACH RUSTY SCREWS STA 185. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-046 WITH APPROVED FAA FORM 8110-3 DATED 3-3-99. REF: ARROW AIR, ARWA. (X)SDR DL72L990497Skin · crackedTHE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT FIN STA 42 AT STRINGER 1R BETWEEN RIB 3A AND 4. THE CRACK WAS LOCATED BELOW AN EXISTING REPAIR. THE EXISTING REPAIR WAS REMOVED AND BOTH DAMAGE LOCATIONS INCORPORATED INTO ONE REPAIR PER B727 SRM 55-30-3, FIGSDR ABXA9900247Skin · corrodedVERTICAL STABILIZER LEADING EDGE SKIN CORRODED. REPAIRED IAW DC8 SRM 51-1-21.SDR 9900639985Skin · crackedDURING PERIODIC CHECK, FOUND VERTICAL STABILIZER LEADING EDGE STRUCTURE FORMER CRACKED AT FS 36, 43, 50 AND 148. FABRICATED AND INSTALLED DOUBLERS PER EA 99-162413.SDR 99ZZZX1324Panel · corrodedDURING A C-CHECK, CORROSION NOTED ON PANEL NR 9501, VERTICAL STABILIZER.SDR DL72K990256Skin · crackedA SKIN PANEL REPAIR WAS FOUND ON THE RHS VERT STAB WHICH WAS INSTALLED W/ BLIND RIVETS PER SRM. REPAIRED PER ERA 332755-14.SDR AT9900222Skin · chafedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE VERTICAL STABILIZER LEFT HAND UPPER PANEL 3703A SKIN CHAFED. BLENDED OUT CHAFE ON LEFT HAND VERTICAL STABILIZER SKIN, TREATED, PRIMED IAW DC9 SRM 55-01-0, 55-32-0, 55-01-0, 51-10-3, AND RES NR 99573.SDR TWAA9902103Skin · crackedVERTICAL STABILIZER UPPER L/E HAD 5 BY 3 BY 0.400 INCH DEEP DENT AND 3 INCH CRACK. REPAIRED PER SPM 55-03, PAGE 5, CLASS B REPAIR. CHECK-C 4-10-98 STL.SDR MWEA99052Skin · crackedFOUND SMALL FAIRING LIFTING AND RIVETS PULLING THROUGH SKIN ON AFT OUTBOARD CORNER OF RIGHT ELEVATOR. MTC FABRICATED AND INSTALLED NEW DOUBLER AND SKIN.SDR TSAA9951036Skin · corrodedEXFOLIATION CORROSION NOTED ON VERTICAL FIN AT FS 60.0 LEFT HAND SIDE. REPAIRED PER ECO 2509 PART 2. TAT: 47,785.0 HOURS. TAC: 63,219. (X)SDR P5CA9900057Panel · delaminatedLEFT STABILIZER LOWER PANEL 344GB FOUND DELAMINATED. REPAIRED PER SRM 51-40-06.SDR P5CA9900056Panel · delaminatedLEFT STABILIZER PANEL 334 NBL FOUND DELAMINATED. REPAIRED PER SRM 51-40-01.SDR P5CA9900067Panel · dentedRIGHT STABILIZER PANEL 341BR-341CR FOUND DENTED. REPAIRED PER SRM 51-10-02 AND SRM 51-00-00.SDR P5CA9900066Panel · delaminatedLEFT STABILIZER PANEL 334MB FOUND DISBONDED. REPAIRED PER SRM 51-40-06.SDR AT9900084Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT VERTICAL STABILIZER LOWER AND UPPER SKIN CHAFED, CORRODED AND HOLES MISDRILLED IN PREVIOUS REPAIRED. MECHANICALLY REMOVED CORROSION, FABRICATED DOUBLERS, HEAT TREATED PARTS AND INSTALLED ALL PARTS IAW DC9SDR AT9900035Skin · chafedSCHEDULED INSPECTION AT AERO CORP, FL. RIGHT HAND AFT VERTICAL SKIN IS CHAFED. REMOVED AND REPLACED THE SKIN IAW DC9 SRM 55-32-0 FIG 7, 51-10-2, 51-10-3 AND RES NR 982300.
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