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 IXXA07SMN267SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT AT STATION ZR 87.000 TO STA ZR 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING PAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER. BONDED PARTS AS NEEDESDR DHL2007801523Skin · crackedLT RUDDER SKIN CRACKED 5" AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL 2024T3 0.016" IAW SRSDR DHL2007801522Skin · deformedRT RUDDER SKIN DEFORMED AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM IAW SRM 55-6-1 FIG 1 PG 2SDR DHL2007801532Skin · damagedRUDDER TIP SKIN BROKEN AT STA ZR 335.250 (DAMAGE CAUSED BY SEMAN). REMOVED BROKEN TIP IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TIP IAW SRM 51-1-21A. REFER TO JC EC-00592-001 (WO 2624) FOR FABRICATION AND NR 101137 FOSDR C2XA07TY060Doubler · missingTYS - A/C WAS FOUND WITH A NUT PLATE MISSING AND THE HOLE ELONGATED ON THE RUDDER 2. MAINTENANCE FABRICATED A FILLER AND A INTERNAL DOUBLER. ALODINED AND EPOXY PRIMED THE PARTS. INSTALL FABRICATED PARTS ON THE RUDDER IAW EC 5540--01077. ALL WORK WAS ACCOMPSDR 07FDEA04447Skin · delaminatedDELAMINATION FOUND AT RUDDER SIDE PANEL IN THE AREA OF ATTACH FITTINGS REPAIR PERFORMED IAW SRM 55-41-12 FIG 216.SDR 07FDEA04404Skin · delaminatedFOUND AT RUDDER TRAILING EDGE LOWER CORNER DELAMINTION NEAR RIB 0 REPAIR PERFORMED IAW SRM 55-41-12 FIG 208A.SDR CALA0700553Skin · delaminatedINSPECTION FOUND LT SIDE OF RUDDER T/E SKIN DELAMINATED AT STA 175.0. THE DELAMINATION MEASURED 0.4"L X 0.2"W. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5540-01243.SDR UPS07850780Skin · crackedINSPECTION TYPE:C1 RUDDER LEFT SIDE VERY LWR FASTENER HOLE CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER ON RUDDER SKIN LWR LEFT SIDE IAW SRM 55-02-00-0, AND SRM 51-1-21.SDR 07FDEA04345Skin · delaminatedFOUND DELAMINATIONS ON RUDDER SIDE PANEL IN AREA OF HINGE ATTACHMENTS AT ALL GFRP-FITTINGS LT AND RT: BR1, BR2, BR4 LOWER, BR4 CENTER, BR4 UPPER, BR5, BR6 AND BR7. DELAMINATION REPAIR OF GFRP FITTING CONNECTION AT ALL HINGE FITTINGS PERFORMED IAW SRM 55-41-12SDR 07FDEA04283Skin · delaminatedVERTICAL STAB UPPER RUDDER TAB UPPER END POTTING BROKEN OPEN AND SKIN DISBONDED ON BOTH SIDES, LEFT SIDE 6-12" FWD OF T/E, RIGHT 5-13" AND DOWN 4" ALSO T/E TIP CORNER OPEN. REPAIRED UPPER RUDDER TAB ON LEFT AND RIGHT SIDES REF SRM 51-40-20 PAR 7, 8, 14, 15, ASDR 07FDEA04282Skin · delaminatedVERTICAL STAB, UPPER RUDDER TAB HAS SPOT OF SKIN DISBOND, 2" BY 3" AREA AT 25" UP FROM LWR END 1" AFT OF FWD EDGE. REPAIRED UPPER RUDDER TAB REF SRM 51-40-20 PAR 7, 8, 14, 15, 19-22 AND APPLIED EXTERIOR PROTECTIVE FINISH REF MM 51-20-151-7.SDR 07FDEA04207Skin · delaminatedFOUND DELAMINATION AT RUDDER SIDE PANEL IN THE AREA OF HINGE ATTACHMENT FITTINGS, LT: BR1, BR4, BR5, BR6, BR7 RT: BR1-BR6 REPAIR PERFORMED IAW SRM 55-41-12 FIG 216.SDR 07FDEA04200Skin · damagedFOUND DAMAGED AREA ON RUDDER, TRAILING EDGE, LOWER SIDE. REPAIR PERFORMED BY LAMINATING THE EDGE IAW SRM 55-41-12/FIG 208A WITH GLASFABRIC.SDR 07FDEA04186Panel · crackedTWO CRACKS AT LEADING EDGE ACCESS PANEL NR 2 OF RUDDER INNER SKIN, HONEYCOMP CORE AND OUTER SKIN CRACKED AT ACCESS HOLE EDGES, MAX CRACK LENGTH = 75MM. REPAIR PERFORMED BY WET-LAY-UP REPAIR AS PER TD/K4/S1/19611/2005/A, APPROVED BY EA 6-5542-82890 AND RAS/DAHSDR ASAA0772053Skin · damagedCOMPOSITE DAMAGE ON LOWER RT SIDE OF RUDDER. REPAIRED IAW SRM 51-70-05 REPAIR 10.SDR MALA070160Skin · dentedLT ELEVATOR 2ND UPPER SKIN DENT 11.5" FROM THE INBD END 9.0" FWD OF THE T/E REPAIRED PER EOS51031.SDR MALA070151Skin · dentedLT RUDDER SURFACE HAS DENT. REPAIRED IAW EOS51031.SDR MALA070150Skin · dentedLT RUDDER SURFACE HAS DENT. REPAIRED IAW EOS55125
SDR ASMF200709001Skin · damagedDURING OVERNIGHT CHECK, DETECTED EXPOSED AND DEFORMED COMPOSITE MATERIAL IN RUDDER TRAILING EDGE OF 1.5 INCH OF LENGTH AND .6250 INCH DEEP AT STATION 235 AND BURNED SURFACE IN RUDDER TRAILING EDGE OF 2 INCH LENGTH AND .6250 INCH DEEP AT STATION 240; ALL OF THSDR AWXA200701107Skin · delaminatedMCN - MAJOR REPAIR - C-11 CHECK - NR 5988823 AND 5988924, RUDDER TRAILING EDGE HAS AREA OF DELAMINATION, RUDDER STATION 228.850, RUDDER STATION 233.852. REPAIRED RUDDER TRAILING EDGE, RUDDER STATION 228.850 - RUDDER STATION 233.852 IAW USAIRWAYS EA 120229.SDR IXXA07SMN203SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER EXT SKIN WITH CORROSION AT STA ZR -253.000 RT SIDE.SDR IXXA07SMN202SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER EXT SKIN WITH CORROSION AT STA ZR -162.000 RT SIDE.SDR 2007FA0000869Skin · crackedFOUND 3 INCH CRACK AFT OF RUDDER BALANCE WEIGHT IN COMPOSIT SKIN FWD OF UPPER ATTACH POINT. AIRCRAFT WAS BASED OUT OF A HEAT RELATED AREA. (K)SDR UPS07850192Skin · corrodedINSPECTION TYPE:C2 LEFT SIDE OF RUDDER SKIN ZR 251 HAS CORROSION. REMOVED SKIN PANEL ON LEFT SIDE OF RUDDER STA ZR 251 IAW SRM 51-1-21. FABRICATED AND INSTALLED LEFT RUDDER SKIN PANEL AT STA ZR 251 IAW SRM 51-3-2, SRM 51-1-9A, AND DWG 5655077.SDR UPS07850178Skin · canningINSPECTION TYPE:C2 RIGHT SIDE OF RUDDER SKIN ZR 271 HAS OIL CANNING. REMOVED SKIN PANEL ON RT/SIDE OF RUDDER AT ZR 271 IAW SRM 51-1-21. FABRICATED AND INSTALLED RUDDER SKIN PANEL ON RT/SIDE OF RUDDER STA ZR 271 IAW SRM 51-1-21, AND DWG 56555077.SDR AWXA200700972Skin · crackedMCN - MAJOR REPAIR - C-20 CHECK - NR 5981803, RUDDER LEADING EDGE SKIN CRACKED, LEFT SIDE, RUDDER STATION 4.5. REPAIRED RUDDER LEADING EDGE SKIN, LEFT SIDE, RUDDER STATION 4.5. IAW USAIRWAYS 120134.SDR IXXA07SMN189SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RUDDER RIGHT SIDE OUTER SKIN FROM STATION ZR 293.938, TO ZV 315.000 AND ZV 330.250. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL CLEANED, TREATED AND PRIMSDR HNAA0700123Skin · corrodedSIX BLIND FASTENERS FOUND CORRODED ON RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO LOWER ACTUATOR FITTING. RIGHT SIDE OF SKIN OF FORE RUDDER NEXT TO ACTUATOR FITTING 6 BLIND FASTENERS REPLACED IAW RD8-55-024.SDR CALA0700328Skin · delaminatedTHE RUDDER TRAILING EDGE SKIN WAS FOUND DELAMINATED OVER AN AREA OF APPROXIMATELY 0.50 INCH BY 1.9 INCH AT RUDDER STA 175. THE DELAMINATION WENT THROUGH THE ENTIRE THICKNESS OF THE LT RUDDER PANEL AND APPROXIMATELY 20% OF THE THICKNESS OF THE RT RUDDER PANEL.SDR UPS07849831Skin · canningINSPECTION TYPE:C3 LEFT RUDDER SKIN OIL CANNING AT STA ZR 185. REPAIRED LEFT RUDDER SKIN AT STA ZR 185 IAW SAA EA 008-2720-01-A0856 DAC DWG 5655077 REV-S, AND FAA FORM 8100-9.SDR MZZA0700007Skin · corrodedINSPECTION FOUND UPPER RUDDER T/E CORRODED AT LOWER STATIC WICK ALONG BASE PLATE LOWER FORWARD EDGE, RUD STA 278-283. THE RUDDER WAS REPAIRED IAW ECRA 5540-01234 AND ECRA 5540-01232. A RUDDER BALANCE PROCEDURE WAS PERFORMED IAW SRM 51-60-07.SDR SWAA071788Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RUDDER T/E LOWER AFT SURFACE DELAMINATED. REPAIRED RUDDER PER SRM.SDR DHL2007806520Skin · crackedLT RUDDER EXT SKIN DENTED AT STA ZR 188.781 AND CRACKED 1" AT STA ZR 198.844 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING (PLATING AND BONDED DOUBLESDR DHL2007786506Skin · dentedFOUND TWO DENTS ON UPPER RUDDER LT T/E SKIN AT LOWER HINGE BS 1540. NO DENTS ALLOWED. FOUND OUT OF LIMITS IAW B727 SRM 55-40-1 FIG, 61. REMOVED LT T/E SKIN AT UPPER RUDDER BS 1540 IAW B727 SRM 51-30-2. FABBED LT T/E SKIN AT RUDDER BS 1540 MATERIAL USED 202SDR N865F753008Skin · corrodedRUDDER ZR 168.656 LT EXTERNAL SKIN WITH CORROSION CPCP 6820 0551.SDR AMW070223021Skin · dented(2) DENTS IN RUDDER; (1) ON THE LT SIDE AND (1) ON THE RT LOWER END CAP. REPAIRED IAW 1900-27-00-0001.SDR SIMA200705701Skin · chafedRUDDER 1 LEADING EDGE FOUND TO BE CHAFED ON LOWER LEFT SIDE. CUT OUT DAMAGE. FABRICATED REPAIR FILLER AND DOUBLER. INSTALLED REPAIR PIECES AND RESTORED SURFACE FINISH IAW EMB IC2007-145/00812. RETURNED AIRCRAFT TO SERVICE.SDR UPS07849223Skin · dentedINSPECTION TYPE:C3 RUDDER RT SIDE LEADING EDGE STA ZR 140 SKIN HAS DENT. FOUND DENT OUT OF LIMITS AT RUDDER STA ZR 140 IAW SRM 55-02-00-0 FIG 001. REMOVED AND REPLACED SKIN AT RUDDER BAY NR 2 STA ZR 140 IAW SRM 51-3-0, 51-1-21, AND SRM 55-06-01-0. NO WEIGHTSDR CA070118001Skin · cracked(CAN) WHILE DOING 100 HR INSPECTION ON AIRCRAFT, MECHANIC NOTICED THAT THERE WAS A CRACK BY THE LIGHTING HOLE BELOW THE TOP HINGE ATTACH BRACKET. NEW SKIN ORDERED AND WHEN RECEIVED NOTICED THAT MFG HAS REMOVED THIS LIGHTING HOLE. REST OF AIRCRAFT OF THIS TYPESDR DJFA2007006Skin · crackedDURING A SCHEDULED MAINTENANCE, DISCOVERED A CRACK ON THE RUDDER LEADING EDGE SKIN AND ONE RIB AT A FASTENER HOLE. UPON FURTHER INVESTIGATION MAINTENANCE FOUND THAT SEVERAL OF THE FASTENER HOLES ON (3) RIBS WERE ELONGATED. THE CRACKS ON THE RIB ORIGINATED INSDR CALA0700037Skin · damagedINSPECTION FOUND THE RIGHT SIDE OF RUDDER SKIN TRAILING EDGE DAMAGED BY LIGHTNING STRIKE NEAR THE TOP BETWEEN THE TWO STATIC WICKS. REPAIRED RUDDER SKIN IAW ECRA 5540-01229.SDR 2007UALA00075Skin · damagedLEFT SIDE OF THE RUDDER EXTERNAL SURFACE HAS EXPOSED COMPOSITE FIBER STRANDS AT 2 EACH EXISTING REPAIRS BETWEEN NR 4 HINGE AND COUNTER WEIGHT HORN. MAJOR REPAIR: REPAIRED RUDDER IN SHOP PER SM 95-55-40-01JD AND GNMM 6-0-2-23.SDR N921R50502Skin · dentedRUDDER ZR 138 LEFT SKIN AFT SECTION WITH DENT. REMOVED LT SKIN SECTION IAW DPS 3.67-27. FABRICATED NEW SKIN IAW DPS 3.69-4. TREATED AND PRIMED AREA AND NEW SKIN IAW DC8 SRM 51-1-8. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21.SDR QXEA200603316Skin · damagedC3 - RUDDER RIGHT SIDE HAS WEAR MARKS ALONG LEADING EDGE, RS 40.0 - 150.0. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-42-001.SDR DHL2006780134Skin · crackedVERTICAL STAB, LWR RUDDER HAS DENT CLUSTER NEAR L/E AFT OF RUDDER HINGELINE, FIN STA 110.4. NDT INSP REVEALED CRACKS IN DENTS. REMOVED AND FABRICATED NEW DOUBLER REPAIR FROM 301 1/2 HARD CRES, .025" BY 23" BY 12", PO NR 9003982, PER B727 SRM 55-40-3 FIG 1. SDR DLM88070443Skin Panel · dentedRUDDER LEADING EDGE RT PANEL REPAIR AT STA ZR=108 - DENT OUT OF LIMITS. PERMANENT REPAIR INSTALLED IAW SRM 51-70-1A.SDR IXXA06SMN422SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND THE RUDDER SKIN CRACKED AT STATION 2R 219.000 LEFT SIDE. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. BONDED NEW SKIN AND INTERNAL DOUBLER WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. APPLIED SEALANSDR ASAA0691130Skin · puncturedRUDDER HAS PUNCTURE ON LOWER LT SIDE. REPARIED IAW SRM 51 70 05.SDR AWXA200601847Skin · delaminatedMAJOR REPAIR - BC-4 CHECK -NR 5950024, DELAMINATION FOUND ON RUDDER RT SIDE PANEL, ABOVE BR 7 NEXT TO FASTENER ROW (FASTENER NR 31), DELAMINATED AREA APROX 81/4 X 5.0 INCHES. REPAIRED RUDDER RT SIDE PANEL ABOVE BR 7 IAW A319 SRM 55-41-00 PAR 9Q(9).
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