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 DHL9872694DPanel · damagedAT D CHECK, PANEL 9604 HAS ELONGATED SCREW HOLES. INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-8, N/R 4238.SDR DL72K980426Skin · crackedFOUND DURING B-2 LETTER CHECK, 2 EA .75 INCH CRACKS IN VERTICAL STAB RT SKIN AT BASE FS 1342 STAB STR 10. REPAIRED PER M/M 55-30-0.SDR QXEA9800382Skin · crackedPDX - RIB 3.4 IN VERTICAL STAB IS CRACKED AT LEFT AND RIGHT AFT CORNERS AT COVE ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-55-46.SDR QXEA9800316Panel · crackedRIB 3.4 IN VERTICAL STAB IS CRACKED AT LEFTHAND AND RIGHTHAND AFT CORNERS AT COVE ATTACH POINT. SPLICED FLANGE ON NOTED RIB PER EA 4-55-46.SDR QXEA9800315Panel · looseVERTICAL STAB COVE PANEL LEFTHAND AND RIGHTHAND FLAGS HAS LOOSE RIVETS ALMOST ENTIRE LENGTH. REPAIRED IAW FOKKER SRM 51-31-01, 51-31-05, 55-31-01, FIGURE 1.SDR P5CA9800217Panel · delaminationCOMP PANEL NR 324L ON LT SIDE OF VERTICAL STAB HAS 3 AREAS OF DELAMINATION. FABRICATED NEW PANEL MATERIAL, CUT NEW CORE, HOT BONDED CORE TO MATERIAL, CURED, TRIMMED TO FIT, PRIMED PER SRM 51-40-06.SDR DL72E980299Skin · crackedFOUND DURING B-1 LETTER CHECK, 1.3125 INCH CRACK VERTICAL STAB SKIN AT BASE LT SIDE JUST ABOVE FUSELAGE STA 1340. REPAIRED PER M/M 55-30-0.SDR CALA9800127Skin · crackedINSPECTION FOUND A .5, 1, AND 2 CRACK IN RT SIDE OF VERTICAL STABILIZER SKIN LOWER SECTION AT STA 1343. THE AREA WAS REPAIRED IAW ECRA 5530-01190.SDR DL72K980126Skin · cracked1 CRACK ACROSS RIVET HOLE AT VERT. STAB SKIN FWD OF R/H LWR CORNER OF SADDLE PANEL CUT OUT. FOUND ON B-2 LETTER CHECK INSTALLED DOUBLER PER M/M 54-30-0 #1SDR AALA980165Skin · crackedTUL - VISUAL INDICATION OF CRACK ON VERTICAL STABILIZER SKIN RT SIDE AT FRONT SPAR WHERE STABILIZER AND FUSELAGE MEET. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 6-23-95. TST: 56,192 HOURS. CYCLES: 34,665. (X)SDR MWEA97855Skin · errodedDURING C-CHECK, FOUND ERROSION FASTENERS ON LEADING EDGE OF VERTICAL STABILIZER JUST BELLOW Q BELLOWS PITOT TUBE. MTC INSTALLED REPAIR IAW SRM 55-01 PG 7.SDR DL72S972485Skin · crackedA .1875 INCH CRACK IN SKIN RT LOWER FWD CORNER OF VERTICAL STAB SADDLE PLATE CUTOUT (PANEL 9501). INSTALLED DOUBLER PER M/M54-30-0 FIG 802.SDR MWEA97844Skin · gougedDURING C-CHECK, FOUND RT LOWER VERTICAL SKIN GOUGED .036 DEEP AT RT AFT CORNER. MTC REPAIRED IAW SRM 51-10 51-30-2 AND 55-31-0 FIG 7.SDR DL72K972444Skin · crackedA 1 INCH CRACK VERT STAB SKIN BELOW ROUND ACCESS PANEL 9523. REPAIRED PER MM 54-30-0 PG 803.SDR DL72K972443Skin · crackedA 1 INCH CRACK AT VERT STAB SKIN BELOW ROUND ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803.SDR ABXA9701809Skin · crackedDURING C-CHECK, FOUND THE VERTICAL STABILIZER LT LOWER AFT SKIN CRACKED. REPLACED SKIN IAW DC9 SRM 51-30-2.SDR ABXA9701751Skin · chafedDURING C-CHECK, FOUND THE VERTICAL STABILIZER CHAFED AND GOUGED ON THE RIGHT SIDE. REPLACED SKIN PANEL IAW DC9 SRM 51-30-2 AND 51-30-8.SDR DL72S972483Skin · crackedVERTICAL STAB SKIN CRACKED. DRILLED REPAIR DOUBLER PER SRM 55-30-3, CUTOUT DAMAGE PER SRM 55-30-3. VERIFIED CRACK REMOVAL AND INSTALLED REPAIR DOUBLER PER SRM 55-30-3.SDR DL72S972482Skin · crackedVERTICAL STAB SKIN CRACKED. CUT OUT CRACK PER SRM 55-30-3 AND VERIFIED CRACK REMOVAL. FABRICATED REPAIR AND INSTALLED DOUBLER/REPAIR.SDR UPS97824719Skin · corrodedINSPECTION TYPE-C, VERTICAL STAB L/E SKIN AT STA ZFS 179.00 CORROSION OUT OF LIMITS. REPAIRED IAW SRM 55-2-1.SDR HEEA0011445Fin Assy · corrodedFIN ASSY SKIN CORRODED BEYOND LIMITS AT THIS STATION.SDR SWAA970882Skin · dentedDURING SCHEDULED D-CHECK, FOUND SHARP DENT ON VERTICAL FIN AT FS 287. REPAIRED PER BOEING SRM.SDR AWXA9700656Skin · crackedDURING SCHEDULED C-23 INSPECTION, EXTERNAL REPAIR ON RT FIN SKIN FIN WL 178, 24 FWD OF REAR SPAR USING BLIND FASTENERS (REF 55-30-03, FIGURE 1, PAGE 1). REPAIRED VERT FIN SKIN PER ER 2-55-30-01.SDR CALA9701445Skin · crackedVERT STAB RT SKIN JUST BELOW PANEL 9524 CRACKED IN TWO PLACES (2 AND 3). CUT OUT CRACKED SKIN. FABRICATED AND INSTALLED FILLER AND DOUBLER PER EC/RA 5530-01190.SDR 97ZZZX4043Stabilizer · rivets looseDURING INSPECTION, FOUND WORKING RIVETS ON TOP OF STABILIZER SKIN JUST UNDERNEATH FAIRING FOR HORIZONTAL STABILIZER TO FUSELAGE.SDR MWEA97738Skin · gougedDURING D-CK, FOUND GOUGES AFT UP SKIN LT/RT OF VERT STAB CANOE FAIR. MTC REPAIRED IAW SRM 51-10-2A.SDR QXEA9700704Skin · crackedPDX - VERTICAL STABILIZER AFT SKIN 3 CRACK STN 1016 RIGHT-HAND SIDE. REPAIRED IAW SRM 55-31-01.SDR DL72S971483Skin · crackedTHE LT AND RT SKINS OF THE VERTICAL STABILIZER WERE FOUND CRACKED AT THE FRONT SPAR JUST ABOVE THE FUSLEAGE CREASE. ON THE LT SIDE, A TOTAL OF FOUR FASTENER HOLES HAVE CRACKS EMANATING FROM THEM. TWO ARE IN THE TYPICAL LOCATION OF THE SRM 55-30-3, FIGURE 7 RSDR 97ZZZM881Skin · corrodedDURINC C-CHECK, FOUND VERTICAL STABILIZER RIGHT SIDE FIN STATION 86 HAS CORRODED FASTENER HEADS AND BULGE AT THE SEAM. REMOVED CORRODED SKIN FROM STATION 86 CUT ACCESS HOLE BETWEEN STATION 1179-1271. FABRICATED SKIN REPAIR FROM 2024 T3 .40 IAW SRM 55-30 AND ESDR MWEA97641Skin · chafedDURING C-CHK, 2 MD CHAFE AREAS FOUND LT SIDE VERT STAB. MAINT REPAIRED IAW SRM 51-30-2, 51-10-3.SDR MWEA97640Skin · gougedDURING C-CHK, MOD GOUGE ON VERT STAB LT SIDE TWO FEET OF HORIZ STAB PIVOT. MAINT REPAIRED IAW SRM 55-01 FIG 4 SHT 2 AND 51-10-3.SDR MWEA97639Skin · gougedDURING C-CHK, FOUND 10 INCHES ABOVE TOP AFT CORN RUDDER, VERT STAB LT SIDE AFT GOUGED/DENTED. MAINT REPAIRED IAW SRM 51-30-2/51-10-3.SDR MWEA97605Skin · crackedDURING C-CHK, FOUND LINE CRACK ON VERT SKIN AFT OF ELEV HINGE. MAINT REPAIRED IAW SRM 51-30-2.SDR MWEA97602Skin · gougedDURING C-CHK, FOUND DEEP GOUGES ON UP AFT RT/LT SKIN VERT STAB. MAINT REMOVED AND REPLACED SKINS IAW SRM 55-01.SDR HEEA0010240Stabilizer Assy · corrodedSTAB ASSY CORRODED THROUGH SKIN.SDR P5CA9701170Access Panel · delaminatedDELAMINATED ACCESS PANEL ON VERTICAL STABILIZER LOWER. REPAIRED PER BOEING SRM 51-40-06.SDR HEEA0010190Fin Assy · separationFIN ASSY HAS SEPARATION ON TRAILING EDGE.SDR QXEA9700456Panel · crackedLEFT SIDE VERTICAL STABLIZER PANEL 57V DOUBLER CUTOUT IS CRACKED. INSTALLED NEW DOUBLER PER FOKKER SRM 51-10-04.SDR CALA9700947Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 8 AND STRINGER 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.SDR CALA9700946Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 2 AND STRINGER NR 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.SDR MWEA97395Panel · crackedCRACKS ON VERT STAB LOWER AFT PANEL BELOW HORIZ STAB. REMOVED AND REPLACED PANEL IAW SRM 53-01 PAGE 1 AND 55-03 FIG 4.SDR HAIHEEA9841Fin Assy · corrosionFIN ASSY CORROSION THROUGH EXISTING METAL. SKIN BEYOND LIMITS.SDR UPS97823091Skin · corrosionINSPECTION TYPE:C/CK, CORROSION AND DAMAGED NUT PLATES INSIDE AREA OF VERTICAL STAB LOWER LT AT REMOVED SKIN PANEL. REMOVED DAMAGED FABED FILLER AND DOUBLER IAW REO 036197, ALODINED AND PRIMED IAW DC8 SRM D51-1-8, INSTALLED FILLER AND DOUBLER IAW DC 8 SRM 51-SDR DL72S970801Skin · crackedFOUND TWO CRACKS AT RT SIDE OF VERTICAL STABILIZER SKIN APPROX STA 1203. REPAIRED PER MM 54-30-0.SDR DL72S970770Skin · crackedA 1 INCH CRACK ACROSS RIVET HOLE AT RT SIDE OF VERT STAB BELOW ACCESS PANEL APPROX 10 FT AFT OF L/E. REPAIRED PER SRM 54-30-0.SDR DL72S970767Skin · crackedFOUND 3 CRACKS EXTENDING FROM RIVET HOLE AT BASE OF VERTICAL STABILIZER LT SIDE APPROX 10 FT AFT OF L/E. REPAIR PER MM 54-30-0.SDR HAIHEEA9525Stabilizer Assy · holedSTAB HAS HOLE IN TOP SKIN.SDR TSAA9755049Skin · damagedDURING HEAVY MAINTENANCE VISIT AT TIMCO, FOUND VERTICAL STABILIZER L/E STA 245 DENTED. FABRICATED DOUBLER IAW B737 SRM 55-30-6. RPAIRED IAW B737 SRM 51-30-0 AND FINISHED IAW SRM 51-10-2. AIRCRAFT RETURNED TO SERVICE. MATERIAL I.D. .063 INCH 2024-T3 ALUMINUSDR CKSA97121Skin · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION RIGHT HAND VERTICAL STABILIZER LEADING EDGE SURFACE CORROSION AROUND FASTENERS. REMOVED CORROSION, INSTALLED REPAIR DOUBLER IAW DC8 SRM 55-2-1 FIGURE 4. CORROSION TASK CARD NUMBER 6000-0551. NON-ROUTINE SDR CKSA97120Skin · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION VERTICAL STABILIZER LEADING EDGE CORROSION AROUND SCREW HOLES AT STA ZFS179. REPAIRED LEADING EDGE PER SRM 55-2-1. CORROSION TASK CARD NUMBER 6000-0551. NON-ROUTINE TASK CARD NUMBER 95638.
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