JASC 5512
Service difficulty reports · 7,887
Reports filed under 5512 · Horizontal 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 = '5512' 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 = '5512' 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 98ZZZX1390Skin · crackedDURING AN INSPECTION, A 4 INCH CRACK WAS FOUND ON TOP OF HORIZONTAL STABILIZER INBOARD OF THE HORIZONTAL SUPPPORT BRACKET. THE SKIN OF THE HORIZONTAL STABILIZER WAS REMOVED AND FOUND THE HORIZONTAL STABILIZER SPAR WAS CRACKED ALL THE WAY THROUGH.SDR 98ZZZX1389Skin · crackedDURING INSPECTION, A 1 INCH CRACK WAS FOUND ON TOP OF THE HORIZONTAL STABILIZER. ALSO, A .25 INCH CRACK WAS FOUND SAME AREA, BUT ON BOTTOM SIDE OF HORIZONTAL STABILIZER. THE PART WAS REMOVED FROM SERVICE.SDR 98FDEA00154Skin · crackedLT HORIZONTAL STABILIZER UPPER FWD PLANK CRACKED FROM FWD EDGE 1.3 AFT THROUGH FASTENER HOLE AND BEYOND, 13 INCHES OUTBOARD OF WORKING BULKHEAD. *S/D* INSTALLED DOUBLER PER SRM 55-20-00.SDR CKSA98074Plate · corrodedDURING LINE MAINTENANCE INSPECTION FOUND PANEL O/B OF O/B ELEV ON LOWER SURFACE HAS SMALL AREA OF CORROSION. REMOVED AND INSTALLED CORRODED FILLER PLATE IAW B747 SRM 51-10-01 AND 51-30-02 W/O 210-674. NON-ROUTINE TASK CARD NUMBER 12915.SDR 98ZZZX1369Skin · crackedDURING PHASE 1 AND 2 INSPECTIONS FOUND 2 CRACKS APPROXIMATELY 1 INCH LONG EMANATING FROM LT HORIZONTAL STABILIZER INBOARD LEADING EDGE RIVETS.SDR 98ZZZX974Rivets · failedDURING 100-HOUR INSPECTION, FOUND 4 OF THE AN426 RIVETS SECURING THE UPPER HORIZONTAL STABILIZER SKIN PULLED COMPLETELY THROUGH ON THE LEFT SIDE. ALL OF THE REMAINING RIVETS BOTH LEFT AND RIGHT SIDE SHOWED SIGNS OF WORKING THESE RIVETS ARE INBOARD UNDER THE SSDR CALA9800261Panel · damagedTHE RT HORIZONTAL STABILIZER LEADING EDGE PANEL SUSTAINED DAMAGE ON FOUR CORNERS WHEN IT WAS DROPPED DURING REMOVAL. THE PANEL WAS REPAIRED IAW SRM 55-12-01 AND ECRA 5510-01390.SDR P5CA9800294Skin · corrodedCORROSION INSIDE CENTER SECTION OF THE HORIZONTAL STABILIZER BETWEEN STRINGERS 54 AND 55, STAB RIGHT BODY LINE 15 TO 43.5. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.SDR P5CA9800285Panel · corrodedLEVEL 1 CORROSION, ON THE UPPER SURFACE OF ALL TRAILING EDGE FIXED PANELS ON THE RIGHT HORIZONTAL STABILIZER. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.SDR P5CA9800280Panel · corrodedLEVEL 1 CORROSION, ON UPPER SURFACES OF ALL TRAILING EDGE FIXED PANELS ON LEFT HORIZONTAL STABIBLIZER. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.SDR P5CA9800274Skin · crackedCRACK ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE FIXED PANEL INBOARD AREA. TRIMMED DAMAGE PER BAC SRM 51-10-01 AND MADE FIBERGLASS REPAIR PER SRM 51-40-06.SDR P5CA9800273Skin · delaminatedDELAMINATION IN SEVERAL OUTBOARD AREAS ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE FIXED PANEL. TRIMMED DAMAGE PER BAC SRM 51-10-01 AND MADE FIBERGLASS REPAIR PER SRM 51-40-06.SDR P5CA9800272Skin · corrodedLEVEL 1 CORROSION, DELAMINATION AND CRACK ON LEFT HORIZONTAL STABLIZER INBOARD TRAILING EDGE FIXED PANEL. DAMAGED AREA TRIMMED PER BAC SRM 51-10-01 AND FIBERGLASS REPAIR MADE PER SRM 51-40-06.SDR P5CA9800213Skin · dentedDURING AIRCRAFT SERVICING, DYNAIR HIGHLIFT FELL ONTO LEFT HAND STABILIZER. REPAIRED PER POLAR MA 5510-02:01.SDR TSAA9855085Skin · crackedDURING CPC CHECK, FOUND CRACKS AT HORIZONTAL STABILIZER LOWER SKIN ACCESS PANEL AT STATION 99.1 RT SIDE. REPAIRED PER ECO 2870 R2. (M)SDR RRXA98028Panel · corrosionDURING A MAINTENANCE VISIT, FOUND LEFT SIDE HORIZONTAL STAB UPPER TE PANEL CORRODED BEYOND LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04197.SDR DHL9880664CPanel · crackedAT C-CHECK, COMPLY WITH DHL MSI 806-0913-1001, REMOVE AND REPLACE HORIZONTAL STAB CENTER SECTION, DUE TO CRACKED FASTENER HOLE. REMOVED AND REPLACED AFT UPPER PANEL PER S/B 55-15.SDR 98ZZZX318Rib · crackedDURING ANNUAL INSPECTION, A CLICKING NOISE WAS HEARD WHILE PRESSING THE LEADING EDGE OF THE HORIZONTAL STABILIZER AT THE RIBS. WITH FURTHER INSPECTION, SEVERAL RIBS FOUND CRACKED ON BOTH LT AND RT SIDES OF THE STABILIZER. ALSO, FOUND ON THIS ACFT, RIB PN 123SDR 98ZZZX690Skin · crackedFOUND HORIZONTAL STABILIZER LEADING EDGE P/N 0532001-76 CRACKED AT INBOARD RIB P/N 0532001-50. SUBMITTER STATED CAUSED BY GROUND HANDLING. DAMAGE WAS DIFFICULT TO SEE DUE TO DARK PAINT COLOR AND CRACK WAS CLOSED UNLESS PRESSURE (DOWNWARD) WAS PUT ON L.E.SDR UPS98825428Skin · crackedINSPECTION TYPE-D, LT HORZ STAB I/B L/E SECTION EXTERIOR SURFACE AT STA XE29 CRACKED. REPAIRED IAW SRM 55-2-0.SDR UPS98825418Skin · crackedINSPECTION TYPE-D, LT HORIZ STAB I/B L/E SECTION SKIN EXTERNAL SURFACE AT APPROX STA XFS 293 HAS CRACK. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 55-3-1, 53-2-0, AND 51-1-20.SDR AU971630Skin · cracked(AUS) HORIZONTAL STABILISER LEADING EDGE SKINS CRACKED. CRACKS ORIGINATE FROM RIB RIVETS FOR THE OUTBOARD ELEVATOR HINGE. CRACK LENGTH 50.8MM (2IN). FOUND DURING INSPECTION IAW AD/MU2/35.SDR CALA9701715Skin · dentedTHE LT HORIZONTAL STABILIZER LEADING EDGE STRAPS HAD AN INTERIM REPAIR INSTALLED DUE TO A DENTS AND THE ITEM HAD BEEN PLACED ON DIP. THE DENTS WERE LOCATED AT STA XFS 172.161 AND 241.289. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5510-01352.SDR AU971505Skin · corroded(AUS) LH AND RH HORIZONTAL STABILISER UPPER AND LOWER LEADING EDGES CONTAINED CORROSION AROUND FASTENER HOLES. AIRCRAFT OPERATES IN A SALT LADEN ENVIRONMENT AND IS WASHED REGULARLY, HOWEVER THE HEIGHT OF THE TAILPLANE MAKES THE WASHING OF THIS AREA DIFFICULT.SDR AU971475Stabilizer · incorrect mod(AUS) STABILATOR INCORRECTLY MODIFIED IAW SI 1167. THE STABILISER HAD ONLY TWO INSPECTION PANELS FITTED TO THE UNDERSIDE INSTEAD OF THE FOUR STIPULATED IN SI 1167.SDR DLL14972480Skin · crackedLT AND RT HORIZ STAB UPPER SKINS WERE BOTH CRACKED IN IDENTICAL LOCATIONS, PANEL NR 4 AT HSS78.4 AT THE END OF BLADE 31 RUN OUT. REPAIRED PER ERA 330988-14.SDR 97FDEA00868Skin · crackedN00770, UPPER LEFT HORIZ STAB HAS A CRACK AT FWD SPAR AFT FLANGE AREA, ON SKIN AT CLOSING RIB PLANE, EMANATING FROM FASTENER HOLE .25 LONG. CUT OUT CRACKED AREA PER SRM 55-20-00. COMPLIED WITH HFEC, NO DEFECTS NOTED. FABRICATED DOUBLER PER SRM 55-20-00 FIG SDR 97FDEA00867Skin · crackedN00772, UPPER RT HORIZ STAB SKIN HAS A CRACK AT FWD SPAR AFT FLANGE AREA OF CLOSING RIB PLANE, RIGHT SIDE 1 LONG CROSSING HOLE FASTENER. CUT OUT CRACKED AREA AS PER SRM 55-20-00 FIG 10 AFTER CUT OUT COMPLETED HFEC. NO DEFECTS NOTED. FABRICATED DOUBLER REPAISDR MWEA97845Skin · chafedDURING C-CHECK, FOUND A SKIN CHAFE ON THE AFT RIGHT SIDE OF HORIZONTAL CANOE PANEL. MTC REPAIRED IAW SRM 51-10 AND SRM 55-31-0 FIG 7.SDR DHL9780254CPanel · damagedAT C-CHECK, HORIZ STAB RIGHT HAND ELEVATOR L/E HINGE NR 2 LOWER COVER PANEL DAMAGED. FABRICATED NEW PANEL 12 X 6 PER SRM 55-2-1.SDR CALA9701608Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER DENTED ON LOWER LEADING EDGE AT XE 332. THE ACCESS PANEL WAS REMOVED AND THE DENTED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-00.SDR 97ZZZX5115Skin · crackedAFTER REMOVAL OF THE SURFACE DE-ICE BOOT, A SMALL CRACK APPROXIMATELY .6250 INCH LONG WAS FOUND RADIATING FROM A RIVET HOLE ON THE LEFT HORIZONTAL STABILIZER AT STA 63.0. THE CRACK WAS RADIATING OUTBOARD AND AFT. CRACKED AREA WAS REMOVED AND A FLUSH DOUBLER SDR ABXA9701888Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE SKIN IS CORRODED AT STA XFS 178. REPAIRED IAW SRM 51-1-21 AND 51-1-26.SDR UPS97825157Skin · corrodedINSPECTION TYPE-D, FOUND CORROSION ON LT HORIZ STAB L/E AT XFS 178 UPPER SURFACE. REMOVED CORROSION, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 55-2-1, 51-1-21, 51-3-0.SDR UPS97824741Skin · corrosionINSPECTION TYPE-C, THE LT HORIZONTAL STAB L/E SKIN AT STA XFS 178.75 HAS CORROSION REMOVAL AREA BEYOND ALLOWABLE LIMITS. REPAIRED IAW SRM 55-2-1 AND 51-1-21.SDR P5CA9701750Panel · delaminatedDELAMINATION PANEL 334 6BL, LEFT HORIZONTAL STAB. REPAIRED PER SRM 51-71-00.SDR P5CA9701738Skin · scratchedSCRATCHES ON RT L/E HORIZ STAB. REPAIRED PER SRM 51-10-02, 55-10-01.SDR P5CA9701714Skin · delaminatedDELAMINATED L/HORIZ STAB LWR T/E. REPAIRED PER SRM 51-24-11 AND SRM 51-30-02.SDR CALA9701568Skin · puncturedINSPECTION FOUND A HOLE IN LEADING EDGE OF LEFT HORIZONTAL STABILIZER AT XFS 154.311. FILLER AND DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-35-01.SDR CALA9701534Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER OUTBOARD TRAILING EDGE JUST BELOW ELEVATOR OUTBOARD HINGE. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-6, FIGURE 2.SDR CALA9701443Skin · dentedRIGHT HORIZ STABILIZER DENT IN LOWER SKIN BY FRONT SPAR 30 FROM TIP. CUT OUT DENTED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 55-10-3.SDR DHL9774204CSkin · corrodedAT D-CHECK, LT HORIZ STAB UPPER TRAILING EDGE AT ELEVATOR STA 118 HEAVILY CORRODED. REMOVED AND REPLACED T/E CHORD PER SRM 51-30-2. N/R 4092.SDR DHL9774203CSkin · corrodedAT C-CHECK, LT HORIZ STABILIZER UPPER TRAILING EDGE AT AT ELEVATOR STATION 173.2 IS EXFOLIATING. REMOVED UPPER TRAILING EDGE CHORD AND REPLACED PER SRM 51-30-2. N/R 4093.SDR DHL9774202CSkin · corrodedAT C-CHECK, LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE AT ELEVATOR STA 191 IS EXFOLIATING. REMOVED UPPER CHORD AND REPLACED CHORD PER SRM 51-20-2. N/R 4094.SDR P5CA9701571Skin · delaminatedDELAMINATION ON THE LEFT HORIZONTAL STABILIZER TRAILING EDGE ADJACENT TO THE NAVIGATION LIGHT. REMOVED DELAMINATION, POTTED CORE AND INSTALLED AND BONDED FIBERGLASS OVERLAYS PER BAC SRM 51-40-14.SDR DHL9780769CSkin · crackedAS A RESULT OF ULTRASONIC INSPECTION ON HORIZONTAL STABILIZER CONTSTANT OUTBOARD SKIN PANELS FOUND A .75 INCH CRACK ON NR 3 PANEL EMANATING FROM BOLT HOLE NR 29 TO BOLT HOLE NR 30 RIGHT SIDE, REF TO DOUGLAS SB A55-16. REPAIRED PER S/B.SDR 98ZZZX792Skin · crackedIT APPEARS THAT VIBRATION AND LEFT HAND PROPELLER HARMONICS CAUSED OIL CANNING BETWEEN TWO STRINGERS THAT INDUCED THE ORIGINAL SKIN CRACK WHICH ENLARGED ITSSELF. FOUND DURING THE BEECH COMPLETE INSPECTION. SUBMITTER STATED IF GONE UNDETECTED COULD CAUSE HORISDR DHL9780763CSkin · corrosionEMPENNAGE AT APPROX STA 160,175, AND 291.0 ON THE UPPER L/E FASTENERS OF THE RT HORIZONTAL STA, THERE IS CORROSION. REMOVED CORROSION LEVEL 2. FABRICATED REPAIR PER DER 85530-2. CUT OUT DAMAGED AREA PER DER 85530-2. TREATED AND PRIMED PARTS AND AREA PER SRSDR DHL9780762CSkin · corrosionEMPENNAGE AT APPROX STA 141.200 ON L/E OF THE RT HORIZONTAL STAB HAS TWO AREAS OF CORROSION. REMOVED CORROSION LEVEL 2, NEED REPAIR. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PER DER 85530-2. TREATED AND PRIMED PER SRM 51-1-8. INSTALLED REPAIR PER DER 855SDR ZZDA5524097Panel · separatingDURING C-CHECK AT AERO CORP, RT HORIZONTAL STABILIZER INBOARD BALANCE PANEL BAY HAS A METAL BOND PANEL ASSY SEPARATING (OUTBOARD PANEL). REMOVED FASTENERS, STOP-DRILLED CRACK IAW B 737 SRM 51-10-1, FABRICATED DOUBLER REPAIR FROM 2024 T3 .016 INCH, DIMENSIONS
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