JASC 5542
Service difficulty reports · 1,373
Reports filed under 5542 · Rudder, 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 = '5542' 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 = '5542' 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 YENA201812030956Skin · damagedDURING BASIC 6 CHECK AT YRQ DATED 11/18, OBJECT IMPACT AND PERFORATION DAMAGE WAS FOUND ON THE RUDDER P/N 190-09910-431 S/N 0000261387 RT SKIN PANEL P/N 190-63064-409. SEE REF. (1) FOR DETAILS. ULTRASONIC INSPECTION WAS ACCOMPLISHED ON THE AREAS SURROUNDING THSDR V6NA2019012404Skin · crackedAT SCHEDULED INSPECTION, DISCOVERED RUDDER LOWER LEADING EDGE SKIN CRACKED. REPLACED RUDDER LOWER LEADING EDGE SKIN.SDR SIMA2018121020005Skin · damagedNUTPLATE ON RUDDER II LH SIDE ELONGATED HOLES-C/A-ACCOMPLISHED PERMANENT REPAIR OF RUDDER II BOTTOM LH SIDE SKIN IAW ERS-EM-55MR-717SDR SIMA20181107001Skin · damagedRUDDER 1 TOP SKIN SURFACE HAS AREAS OF DAMAGE. R&R RUDDER I TOP SKIN/RIB IAW SRM 51-40-02.SDR DALA2018102406297Skin · puncturedRUDDER LEFT SIDE SKIN, SMALL PUNCTURE, AND DISBOND AFT OF MIDDLE PCA C/W SRM 51-60-03 AND 55-40-01.SDR ASOA2018101854057Doubler · unknownIAH - MAINTENANCE REMOVED AND RPLACED A REPAIR DOUBLER ON 2 BETWEEN STATION ZV2357 & ZV2648 AND THE AIRCRAFT WAS APPROVE FOR RETURN TO SERVICE.SDR CALA2018101302104Skin Panel · corrodedRUDDER TIP RT SIDE HAS CORROSION AND HAS NUMEROUS EXPOSED MATERIAL ON FAIRING MOUNTING SURFACE, OFF ACFT PART. REMOVED DAMAGE FROM RUDDER TIP AND REPAIRED IAW SRM 55-44-0 0-300-012 FIG 20109. THIS REPAIR IS CONSIDERED MAJOR REPAIR IAW GMM 03-20-20 AND SRM 51-1SDR DALA2018101005976Rudder · damagedCOMPOSITES SHOWING ON MULTIPLE AREAS ON RUDDER. REMOVED RUDDER ON WORKCARD 2720-4187. INSTALLED NEW RUDDER ON WORKCARD 2720-4421. RIGGED RUDDER ON WORKCARD 2720-7454.SDR FDEA201810043132Skin · dented3 DENTS ON TOP OF EMPENNAGE JUST TO THE LEFT OF RUDDER . REQUIRE EVALUATION REPAIRED IAW SRM 53-80-01 FIG 1 R2 SH1 & 51-70-10-2R REPAIR 4SDR AALA201810299008Skin · saturatedAIRCRAFT IN BASE MAINTENANCE. RUDDER RIGHT HAND SIDE SKIN HAS INDICATION OF TRAPPED WATER NEAR RIB 9 AND 14.5" FROM THE TRAILING EDGE. REPAIRED RUDDER PER SRM 55-41-13-300-026.SDR IPXA2018092874483Skin · splitLOWER AFT RUDDER, AFT LOWER T/E, ZAR 310, HAD A 10 INCH SPLIT IN COMPOSITE. REPAIRED RUDDER T/E IAW SRM 55-40-02, REPAIR 2, FIG 201. MAJOR.SDR R61A201809120954Skin · tornMAJOR, RUDDER COMPOSITE SKIN IS TORN 3" IN LENGTH ON RT SIDE AT THE NR 2 HINGE POINT. COMPLIED WITH ETD2018-170-*090470 FOR REPAIR OF RT SIDE AT NR 2 HINGE POINT RUDDER COMPOSITE SKIN. AIRCRAFT REMAINS IN HEAVY CHECK BNA.SDR SRXR201808210024Skin · corrodedUPPER FWD RUDDER HAD CORROSION ON THE LOWER RT SIDE. REPAIRED IAW SRM 55-40-01, REPAIR 1, FIG 201.SDR DALA2018080874950Skin · crackedDURING INSPECTION, FOUND TWO CRACKS ON THE RT HORIZONTAL STAB LOWER SKIN MID SECTION LES=133.15. THE SKIN WAS REPAIRED IAW SRM 55-10-01, REPAIR 11.SDR CVGA20180809001Skin · crackedLOWER LEFT OF RUDDER LEADING EDGE WAS FOUND TO BE SCRATCHED. REMOVED PAINT AND FOUND A CRACK IN LEADING EDGE SKIN. CRACK WAS BEYOND LIMITS AND THE LOWER LEADING EDGE SKIN WAS REPLACED.SDR ASOA201807177133Skin · damagedA/C WAS IN FOR A A-CHECK WHEN INSPECTION FOUND SMALL HOLE IN THE RUDDER SKIN ON THE 32 RUDDER LEFT SIDE LOWER AFT CORNER. MAINTENANCE REPAIRED THE SMALL HOLE PER ETD 2018 145-077751. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.SDR FDEA2018071641707Skin · corrodedUPPER AFT RUDDER ASSEMBLY LT UPPER SKIN FOUND WITH CORROSION AT APPROX ZAR 554.920. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS AS PER SRM 55-00-00-2R FIG 202. ORIGINAL THK 0.016", THK REMOVED 0.015", THK REMAINED 0.001". CARRIEDSDR SWIA2018081444996Skin · scratchedLEFT SIDE OF THE RUDDER TRAILLING EDGE HAD A SCRATCH ABOUT 12 INCHES LONG, AT ABOUT THE MIDDLE OF THE RUDDER. REPAIRED THE RUDDER TRAILLING EDGE IAW REO.SDR AALA201807099017Skin · corrodedCORROSION FOUND ON THE RUDDER, RIGHT SIDE TRAILING EDGE APEX STRIP. REPAIRED THE RUDDER IAW SRM 55-41-19-300-006.SDR SIMA201806180002Skin · crackedRUDDER 2 RT TRAILING EDGE HAD PULLED RIVETS, AND FOUND TO BE CRACKED .196 FROM A RIVET TO THE TRAILING EDGE. REPAIRED THE RUDDER TRAILING EDGE IAW ERS-EM-55MR-680.SDR AALA2018052989014Skin · splitMAINTENANCE FOUND THREE PULLED RIVETS AND A 7.250" SPLIT AT TAIL END OF RUDDER, APPROXIMATELY 25 INCHES FROM BOTTOM. AIRCRAFT WAS GROUNDED. REPLACED THE RUDDER IAW AMM 27-21-41.SDR ASOA201805197086Skin · dentedTYS A/WAS IN FOR A A-CHECK WITH A RUDDER INSPECTION TASK CARD AND FOUND THE RUDDER 1 LE SKIN DENTED ON THE LEFT SIDE APPROXIMATELY 3 FEET FROM THE BOTTOM OF THE RUDDER. MAINTENANCE CUTOUT A 4 INCH X1.5 INCH SECTION OF SKIN AND INSTALLED A FILLER AND DOUBLER IASDR ASOA201805167082Skin · damagedDURING A C CHECK, FOUND THE RUDDER 2 LOWER LT SIDE WITH A HOLE IN THE SKIN AND A DESCENDING CRACK EXTENDING APPROXIMATELY 1.5 INCHES FROM THE HOLE. REPAIRED IAW ETD2018-145-048501.SDR JGVR20180515002Panel · corrodedFOUND SEVERELY CORRODED FWD WEDGE PANEL OF THE RUDDER FAIRING ASSEMBLY. REPLACED PART WITH NEW P/N 6912670-5 PER SRM 51-20-01, 51-40-03, 51-40-04 AND SPM 20-40-20.SDR WVER201807250286Skin · damagedLEFT SIDE OF RUDDER, APPROXIMATELY 18 INCHES FROM BOTTOM EDGE, THREE GOUGES AND DENTS.SDR DALA2018042702845Skin · damagedFOUND DAMAGED ALUMINUM FLAME SPRAY, LT & RT SIDES, SEVERAL AREAS. ON THE RUDDER. THE FRAME SPRAY WAS REPARIED IAW ERA.092613-14MA, REV C.SDR SIMA201804181004Skin · puncturedRUDDER, RT SKIN PUNCTURED BETWEEN RIBS ZV2938.0, AND 3229. THE RUDDER SKIN WAS REPAIRED IAW SRM 55-40-01.SDR DALA2018032801980Skin · damagedPAINT ON LEFT AND RIGHT SIDE OF RUDDER MISSING DOWN TO COMPOSITE LEVEL. RUDDER WAS REPLACED.SDR GTIA2018031602521Skin · damagedRUDDER, RT SIDE SKIN SHELL DENTED AND DEBONDING.SDR ASOA201803097031Skin · crackedDURING A C-CHECK, FOUND A CRACK ON THE RT TRAILING EDGE OF THE VERTICAL STAB BETWEEN THE FIRST ROLL OF BEARINGS AND THE 2ND ROLL. MAINTENANCE INSTALLED A REPAIR TO THE CRACKED AREA OF THE RUDDER TRAILING EDGE IAW EC/TC ETD 2018-145-019454.SDR YENA201803080903Skin Panel · debondedAT C6 CHECK LCQ DATED 02/18, DURING RUDDER INSPECTION PER TC A320-55-40-00-210-001, DISBOND DAMAGE WAS FOUND ON THE RUDDER P/N D5547100400000 S/N TS4250 LT SIDE SIDE SHELL SKIN PANEL AT THE LOWER FORWARD NR 2 HOIST POINT. SEE REF /2/ FOR EXACT LOCATION AND DAMSDR YENA201803080129Skin · debondedDURING HEAVY MAINTENANCE, THE LT SIDE OF RUDDER WAS FOUND DISBONDED AT LOWER FORWARD NR 2 HOISTING POINT FROM 2 O'CLOCK TO 6 O'CLOCK POSITION EXTENDING AFT. REPAIRED IAW TD 80422 4941-005-2018A, AND EC A18-145-01.SDR DALA2018022801259Skin · damagedDAMAGE T, DURING WEIGHT AND BALANCE CHECK ON RUDDER, SKIN CUT OUT OF HINGES WERE DAMAGED. RUDDER OF THE VERTICAL STABILIZER WAS REPAIRED PER SRM VOL I 55-41-01 PARA 22, WEIGHT AND BALANCE CHECK WAS PERFORMED PER SRM VOL II 55-40-01.SDR 2018FA0000064Skin · corrodedCORROSION ON THE RUDDER TE SKIN. ACCOMPLISHED LETTER DQ11021M1.SDR DALA2018022101114Skin · damagedLEFT RUDDER SKIN DAMAGED. COMPLIED WITH ERA 565993-14, REV ORIGINAL. SECTION II.SDR AALA201802199025Skin · delaminatedCRACK AND DELMAINATION FOUND ON THE RUDDER LOWER AFT TRAILING EDGE. REPLACED THE RUDDER IAW AMM 27-21-41-400-801-C.SDR IPXA2018021626578Skin · delaminatedDISBONDED AREA ON THE RT SIDE OF THE RUDDER, HAS TRAPPED WATER INDICATION. FOUND JUST BELOW RUDDER STATION 869, TWO INCHES AFT OF T/E SCREWLINE. REPAIRED IAW 55-41-12 PARA 22 FIGURE 220.SDR AALA201803199006Skin · damagedTRAPPED WATER INDICATION ON RUDDER LEFT SHELL HONEYCOMB CORE CELL LOCATED BETWEEN BR 6 TO BR 7, 3.40 INCHES FROM BR 6, AND 16 INCHES FROM TRAILING EDGE VERTICAL STABILIZER AROUND HOISTING POINT NR 3 UPPER POSITION. REPAIRED THE LEFT RUDDER SKIN IAW EA 277765SDR AALA20180204007Skin · crackedCORRODED AND CRACKED RUDDER SKIN LOWER AFT CORNER. REPAIRED THE RUDDER SKIN IAW EA 276776, AND SRM 55-40-01.SDR SIMA20180130008Skin · dentedRUDDER LOWER RTH SKIN DENTED BETWEEN RIBS ZV 920 AND ZV 1164. THE RUDDER SKIN WAS REPAIRED IAW SRM 55-40-01, ITEM 2.SDR AALA201802289004Skin · saturatedAIRCRAFT IN BASE MAINTENANCE. TRAPPED WATER INDICATION ON RUDDER BETWEEN BR 1 TO BR 2 AT 23 INCHES TO BR 1 AT 5 INCHES FROM LEADING EDGE FASTENER ROW, LEFT HAND SHELL AROUND THE LOWER FORWARD HOISTING POINT ON VERTICAL STABILIZER. REPAIRED RUDDER PER EA 277362SDR SIMA20180125004Skin · chafedRUDDER 1 HAS CHAFE ABOVE PANEL 326AL. REPAIRED THE SKIN IAW ERS-EM-55MR-633.SDR SIMA20180121001Skin · puncturedRIGHT SIDE OF RUDDER HAS A HOLE IN THE SKIN NEAR THE LOWER AFT CORNER. REPAIRED THE RUDDER LOWER SKIN IAW ERS EM-55MR-632.SDR AALA201802269070Skin · damagedTRAPPED WATER FOUND ON THE RUDDER LEFT SURFACE BETWEEN HSS 463 AND 576, AND BETWEEN BR 4 TO BR 5. REPAIRED THE RUDDER SURFACE IAW EA 276974.SDR AALA201802229001Skin · contaminatedTRAPPED WATER INDICATION ON RUDDER LEFT HAND SHELL HONEYCOMB CORE CELLS BETWEEN RUDDER RS 274 AND 327 AND BETWEEN BR 1 AND 2. REPAIRED RUDDER PER EA 276924.SDR AALA201802209017Skin · contaminatedTRAPPED WATER INDICATED ON THE RUDDER SHELL ASSEMBLY, LOCATED BETWEEN RS 463 AND 576 AND HINGE BEARING 4 AND 5. REPAIRED THE RUDDER SKIN IAW EA 276924.SDR GTIA2017122202315Skin · damagedRUDDER SHELL AT THE NR 2 HOIST POINT DAMAGED 1,350 SQMM. REPAIRED THE RUDDER SHELL.SDR SIMA20171221001Skin · puncturedFOUND A PUNCTURE IN THE RUDDER ON THE RIGHT SIDE 20 MM FROM BOTTOM AND 45MM FROM AFT EDGE. PERFORMED A PERMANENT REPAIR TO THE RUDDER IAW ERS-EM-55MR-614SDR DALA2017122008795Skin · delaminatedLEFT RUDDER SIDE SHELL HAS THREE LOCATIONS OF DELAMINATION AND/OR WATER INGRESS AND WERE MEASURED TO BE 15 SQUARE INCHES, 24.75 SQUARE INCHES, AND 20 SQUARE INCHES. ALL OF THE DAMAGE LOCATIONS ARE WITHIN THE CFRP AREAS AND ARE 114 INCHES FROM THE BOTTOM EDGE, SDR DALA2017122008756Skin · damagedDAMAGED METALIZED ON RUDDER SKIN RT AND LT SIDE (EHV). REPAIRED PER ERA 092613-14 MA, REV C.
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