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 FDEA202504180639Skin · damagedFOUND TWO BURN MARK NEAR RUDDER TOP SIDE TE AND PNL 326AT. PERFORM REPAIR OF APEX STRIP BY NEW STRIP SECTION AND CONNECTION PLATES WITH RIVETS AT NEAR RUDDER TOP SIDE TE AND PNL 326AT AREA I.A.W A300-600F SRM 55-41-12-201, PARA.13, PAGE.237~PAGE.239, FIG.2SDR FDEA202504070575Skin · dentedFOUND 3" X 1" DENT ON RUDDER LH SIDE APPROXIMATLY 85.5" FROM THE FUSELAGE AND 23" FROM THE FWD HINGE. REPAIRED DENTED/DELAM (4" X 2") AREA ON L/H SIDE OF RUDDER AT STA 84.250" AND 21.00" FROM THE FORWARD HINGE. IN REF TO B767 SRM 55-40-01-2R FIG 201 SHEET SDR DALA2025040802712Skin · corroded(LOG 0894598) CORROSION ON SKIN OF RUDER TRAILING EDGE STA RUD STA 257 APROX LH SIDE AT RUDDER. SKIN OF RUDER TRAILING EDGE STA RUDSTA 257 APROX LH SIDE AT RUDDER. WAS REPAIRED PER B737-800 SRM 55-40-01-2R PROCEDURE 2 REPAIR 2 AND ( LEVEL CORROSION II ) PER B7SDR HNAA2025042800231Skin · cracked53-2204 RH SKIN PROFILE CRACKED AT RUDDER LWR FITTING. REPAIRED FITTING IAW ETD2025-145-905148 AND EO1-53-25-0132SDR SWIA202509020023Skin · crackedRUDDER LEADING EDGE SKIN, LOWER RT, CRACKED. REMOVED AND INSTALLED NEW RUDDER LEADING EDGE SKIN LOWER RT IAW SRM 51-42-06-001-001 A01 AND DWG CC670-22002 REV -B. COMPLIED WITH TASK 51-900-1002-SKY.SDR REXA2025032100342Drag Angle · cracked"VERTICAL STAB LH FWD DRAG-ANGLE IS CRACKED. FABRICATED, LOCATED AND DRILLED REPAIR PARTS ITEM 1 FWD ANGLE DOUBLER FROM 2024T3 0.090"" P.O.# W72936, ITEM 2 FWD ANGLE FILLER FROM 2024T3 0.090"" P.O# W72936 IAW CRJ900 SRM 55-31-00-201-001-A01 STEP 5.B. (4) THRUSDR CALA2025032103052Skin · contaminatedL/H AFT SIDE OF RUDDER HAS TRAPPED WATER 2 IN FROM TRAILING EDGE , 103 IN FROM BOTTOM, 8X5 IN DIAMETER, NUMEROUS SPOTS IN AREA. " REPAIR PRIOR TO NEXT FLIGHT". GENERATED BY V061632 ON HAECO LCQ NR 9290745/38745. REPAIR WAS PERFORMED IAW A320 SRM 55-41-13-300-0SDR VNAA20250320066Skin · dentedHN00201914 SN: 00471 DISCREPANCY: RUDDER EXTERNAL SKIN IS DENTED CORRECTIVE ACTION: REPAIRED RIGHT SIDE RUDDER SKIN IAW CRJ-700 SRM 55-41-01-201-001-A01.SDR IPXA2025071363969Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON RUDDER R/H SIDE TRAILING EDGE AT APPROXIMATELY RUDDER STATION 255. PERMANENT REPAIR COMPLIED WITH PER EO-93077-REQ3. DEFERRAL REMOVED.SDR DALA2025031702014Rudder · ground damage(LOG 0855976) A/C HIT IN RUDDER BY JAL 787. C/W ERA 624172-14 SECTION 1 PERMANENT REPAIR. R/R RUDDER ASSY, REF LOG 0853320. REPAIRED VERTICAL STAB ASSY IAW ERA 624172-14,624294-14,624280-14,624522-14,624701-14 ALL REV ORIGINAL.SDR DALA2025031702016Rudder · damaged(LOG 0853320) DAMAGED RUDDER BY TAIL STRIKE. REMOVED RUDDER PER AMDS #2721-4912 STEPS 1-3. C/W RUDDER REPLACEMENT IAW AMDS 2721-4912 (R.GROSS 436426) ALL RII ITEMS C/W.SDR JR2R20250307053Diverter · damaged326AL UPPER T/E APPEARS TO HAVE LIGHTNING EXITSDR DALA2025030301643Skin · dentedSHIP 3312 RUDDER RHS LEADING EDGE FOUND DENT FROM BOTTOM 43INCH. CORRECTIVE ACTION: COMPLIED WITH ERA 624354-14. (0837930)SDR FDEA202502200255Skin · chafedRUDDER CAP AFT UPPER LH INTERIOR COMPOSITE DAMAGED . BONDED A (1X1 INCH) SANDING PLY ON THE RUDDER CAP AFT UPPER LH INTERRIOR AREA. IN REF. TO 767 SRM: 55-40-30-2R FIG.201 SHEET:2 AND 767 SRM 51-70-17. RE-APLIED PRIMER IN THE INNER SURFACE IN REF. TO 767 ASDR JJBA20250225042Rivet · looseMIDDLE OF RUDDER I, LH SKIN RIVETS LOOSE ON ANCHOR NUT FOR RUDDER DEFLECTION TOOL INSTALLATION. REPAIR DOUBLER ON LH RUDDER I SKIN BTW RIB ZV2312-ZV2601SDR JJBA202502265041Skin · damagedMIDDLE OF RUDDER II, LH SKIN, RIVETS HOLES ELONGATED ON ANCHOR NUT FOR RUDDER DEFLECTION TOOL INSTALLATION. REPAIR DOUBLER ON LH RUDDER II SKIN BTW RIB ZV2067-ZV2357SDR FDEA202502180244Fairing · damagedRUDDER CAP HAS A LIGHTNING STRIKE LOCATED 12" FROM L/E. REPAIRED AND BLENDED RUDDER CAP, AREA IS WITHIN ALLOWABLE DAMAGE LIMITS PER EVALUATION IN REF. TO B767 SRM 51-70-14-0G, PREPPED, PRIMED AND PAINTED IN REF. TO AMM 51-21-00-7. REFER TO JPF FOR OTHER WSDR SWIA202505300214Skin · dentedDENT ON RH SIDE OF THE RUDDER, LOCATED ROUGHLY 6" FROM THE TOP AND 18" AFT OF THE LEADING EDGE OF THE RUDDER. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-55-41-300 DATED: 2025-02-21 AND REV -- FOR THE PERMANENT DISPOSITION FOR THE DENT TO THE RUDDER SKIN BESDR JJBA20250217027Skin · mechanic error2 MISDRILLED HOLES ON RUDDER II ABOVE ACCESS PANEL 327CL. REMOVED DAMAGE ON RUDDER 2 ABOVE ACCESS PANEL, FABRICATED REPAIR PARTS, LOCATED AND DRILLED HOLES. PREP, PRIMED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER REPAIR PARTS ON RUDDER 2 ABOVE ACCESS PNLSDR CALA2025021100334Skin · damagedDURING REMOVAL OF STATIC DISCHARGER BASE ON THE RUDDER WAS FOUND UNDER THE BASE FOUR HOLES OUT OF STANDARD ON LH SIDE AND ONE RH SIDE THE RUDDER UPPER PANEL SKIN STATIC DISCHARGER WAS REPAIRED AS PER EC/RA: 5540-01602. ITEM OK TO SERVICE. ALL APPLICABLE INSPESDR N6WA2025020505Skin · dentedDENT FOUND ON RH SIDE OF RUDDER BETWEEN RS78.82 - RS72.79. REPAIRED RUDDER IAW CJR SRM 55-41-01 AND GOJET EO C550-55MR -002-0.SDR SWIA202503260204Skin · dentedRUDDER HAS A DENT ON THE LH SIDE ABOVE THE TOP PCU RIB (C-CHECK RO 03/25/2024)COMPLIED WITH 601R-55-41-298 DATED: 2025-02-24 REV -- REPAIR TO RUDDER LHS SKIN BETWEEN STA 95.57 & STA 102.52. COMPLETED THE M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. NDT'S COSDR SWIA20250430115Skin · dentedDENT FOUND ON RUDDER AT UPPER R/H SIDE BELOW TOP MOST RIB (MARKED) (C-CHECK RO 04/30/2025)MEASURED AND EVALUATED DENT ON RUDDER AT RS-140 TO RS-148, DENT FOUND OUT OF LIMITS AND PERFROMED REPAIR IN REF TO MHIRJ REO 601R-55-41-299REV -- 2025-03-11SDR FDEA202501150192Skin · damaged2EA WATER TRAPPED AREAS WERE FOUND AT LH RUDDER T/E SCREW LINE NO.19(30MM*40MM) FASTENER AND RH RUDDER T/E SCREW LINE NO.39(20MM*80MM) FASTENER. ACCOMPLISHED THE COMPOSITE REPAIR AT LH SKIN SCREW LINE #19 AND RH SKIN SCREW LINE #39 OF RUDDER I.A.W A300-600SDR IPXA2025010882763Skin · debondedDISBOND FOUND RUDDER R/H SPAR AND ADJACENT STRUCTURE BETWEEN RUDDER STATION 106 AND STATION 181. (REPAIR). REPAIR DELAMINTION ON RH RUDDER SKIN PANEL AT RUD STA 140.108 I.A.W. UPS EO-92480-REQ1 REV1. CONDITION CHECK IS SATISFACTORY.SDR SWI2025F00218Skin · chafedRUDDER HAS CHAFING ALONG ENTIRE RH LEADING EDGE (MARKED) (C-CHECK RO 2/26/2025) BLENDED AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 690-55-41-064 REV -- DATE 2024-12-26 AND SRM 51-12-00-001-001 A01 REV 38 DATE JUL-25-2020. COMPLIED WITH ALL STEPS OFSDR SWIA2025022841212Skin · chafedRUDDER HAS CHAFING ALONG ENTIRE LH LEADING EDGE (MARKED) (C-CHECK RO 2/26/2025) BLENDED AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 690-55-41-064 REV -- DATE 2024-12-26 AND SRM 51-12-00-001-001 A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SSDR SWIA2025011314Skin · bentRUDDER LEADING EDGE SKIN BENT AT LOWER RH HINGE CUT-OUT (C-CHECK RO 1/13/2025) DURING DRESS-BACK OF BENT SKIN OF THE R/H LWR L/E OF THE RUDDER, THE SKIN CRACKED. REMOVED AND INSTALLED 1EA NEW SKIN (P/N CC670-22035-5) PER CRJ200SRM 51-42-06 AND DWG 601R2SDR FDEA202410281590Skin · damagedFOUND A LIGHTNING STRIKE AT RUDDER TRAILING EDGE ABOUT RUD STA 525.SDR JJBA20250317001Doubler · damagedFOUND DOUBLER ON RUDDER 1 FRON LH SIDE TO BE DAMAGED. REMOVED RUDDER 2. REMOVED RUDDER 1. REMOVED DOUBLER ON RUDDER 1. FABRICATED NEW DOUBLER W/ 2024-T3 0.040". TRANSFERRED HOLES TO NEW DOUBLER. INSTALLED DOUBLER ON RUDDER 1. APPLIED FILLET SEAL TO DOUBLER. INSDR DALA2024101810184Skin · dented(LOG 0614343) DURING DENT EVALUATION, PAINT ON RUDDER SKIN RH SIDE BTW RUD STA 102.2 AND RUD STA 129.7 WAS REMOVED, AND A PREVIOUS REPAIR WAS FOUND IN THE SAME AREA. AREA ON RUDDER SKIN RH SIDE BTW RUD STA 102.2 AND RUD STA 129.7 WAS REPAIRED PER B737-800 S.R.SDR CALA2024101402634Skin · delaminatedRIGHT SIDE OF RUDDER UPPER SKIN HAS PUNCTURE DAMAGE TO COMPOSITE WITH DELAMINATION, MISSING PAINT, AND COMPOSITE EXPOSED. 25 IN FROM RUDDER TIP, 8IN FROM TRAILING EDGE. REPAIRED RUDDER RH SIDE 25IN FROM TOP 8IN FROM TE IAW A320 SRM 5 5-41-14-300-009 CAT A REPSDR FDEA202410111493Skin · dentedRUDDER (RH SIDE) BETWEEN RUD STA 131.108 TO 106.142 WITH DENTS. RUDDER (RH SIDE) BETWEEN RUD STA 131.108 TO 106.142 WAS REPAIRED IAW E.A.#: H-5540- T0380975 RELEASE DATE: OCT 11,2024SDR FDEA202410111492Skin · dentedRUDDER (RH SIDE) BETWEEN RUD STA 240.972 TO 181.032 SEVERAL DENTS. RUDDER (RH SIDE) BETWEEN RUD STA 240.972 TO 181.032 WAS REPAIRED IAW B767 SRM 55-40-01- 2R REP 1 FIG 201 (SHEET 2) PAG 1-2, SRM 51-70-17-0G PAR 4.L(4) AND SRM 51-70-03-0G PAR 5.L FIG 16 REV SDR HNAA2024102801027Skin · cracked55-2261 RUDDER II, LH SKIN CRACKED AT UPPER MID HINGE FITTING ATTACHMENT. REPAIRED IAW ETD 2024-145-026648 AND EO1-55-24-0624SDR SWIA20250226924Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA78985-670-55-41-107 750EV MXCODEID62683-PR - DENT ON THE RIGHT SIDE RUDDER SKIN AT (RHS DWG: CC670-22031, POCKET THICKNESS AT SUBJECT LOCATION 0.25" +/- 0.004",REF) BETWEEN RS 102.520-RS 108.250. DENT MEASURES 0.383" SDR FDEA202409091259Skin · damagedRUDDER, LH SIDE APPROXIMATELY 56" FROM TRAILING EDGE AND 75" FROM THE BOTTOM, SKIN HAS DAMAGE. MARKED WITH RED GREASE PEN AND YELLOW STICKER. REPAIRED, TREATED, AND PAINTED RUDDER SKIN DAMAGE AT L/H SIDE APPROXIMATELY 56" FROM TRAILING EDGE AND 75" FROM THSDR LR7A2024090303485Skin · dentedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RUDDER TRIM TAB TRAILING EDGE SKIN DENTED AT FS1173, VS110-114. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. DRC# 0403. / PSE# 55-10-09, AD 2012-06-09SDR LR7A2024090303477Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RUDDER LEADING EDGE SKIN WITH TEMP STOP DRILL REPAIR AT FS1128, LBL2-5, VSS174L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. DRC# 0314. / PSE# 55-10-09, AD 2012-06-09SDR EE4Y2024090220811Skin · delaminatedDURING INSPECTION AS PER ALLEGIANT WORK CARD 554003-01-1-001 AND REMOVAL OF RUDDER TO COMPLY WITH NON ROUTINE ITEM 3-52 WAS FOUND RH UPPER AND LOWER HOIST POINTS LOOSE AND DAMAGED. PERFORMED PERMANENT REPAIR CAT A AT RUDDER SHELL SKIN PANEL RH AROUND UPPER # 3SDR EE4Y2024090220810Skin · delaminatedDURING INSPECTION AS PER ALLEGIANT WORK CARD 554003-01-1-001, EMPENNAGE RUDDER RH SIDE PANEL WITH DELAMINATION AROUND TRAILING EDGE FASTENER # 12.PERFORMED PERMANENT REPAIR CAT A AT RUDDER SHELL SKIN PANEL RH T/E FASTENER 12 (ZONE W) IAW A320 SRM 55-41-13-283-SDR 2024FA0000579Skin · corrodedBLENDED CORRODED AREA ON THE LH SKIN ON THE RUDDER NEAR THE REPAIRED LEVEL 2 CORROSION FOUND ON LH SIDE OF RUDDER, JUST AFT OF THE RUDDER TRIM ACTUATOR CUTOUT, BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, REMOVING EXISTING DOUBLER, FABRICATINSDR FDEA202407191032Panel · contaminatedRUDDER RH SIDEPANEL STA529 AROUND HINGE #5 AREA FOUND FLUID INGRESS EVIDENCE. COMPLIED WITH EA: 6-5540-T0379793 P1 TEMPORARILY REPAIRED THE FLUID INGRESS RUDDER RH SIDEPANEL HINGE #5 AREA. TITLE: STABILIZERS - RUDDER - RH SHELL WATER INGRESS - EO 6- 5530-ESDR AALA202408213842Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: TRAPPED WATER INDICATION ON SHELL HONEYCOMB CORE CELLS ON VERTICAL STABILIZER. REPAIRED VERTICAL STABILIZER (RUDDER) AROUND HOIST POINT 3 PER SRM 55-41-13-300-029.SDR UIEA2024071100644Skin · erodedLWR RUDDER LH FOUND EROSION(<P>PERFORMED REPAIR AT EROSION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR HNAA2024081300695Skin · dentedE045412 DENT ON RUDDER 2. INSTALLED SERVICABLE DOUBLER AND FILLER FOR REPAIR ON RUDDER 2 IAW EMB 145 ETD2024-145-019254 REV. "B" AND EO1-55-24-0431.SDR FDEA202406250868Skin · corrodedEXISTING REPAIR ON RUDDER LH SKIN BETWEEN RUDDER STA95-STA110 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RUDDER LH SKIN BETWEEN RUDDER STA95-STA110 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA: 6-5541-114926. TITLE: STABILIZERS - RUDDER - SDR AALA202406128116Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RUDDER RIGHT HAND SIDE LOWER TRAILING EDGE SPLIT / DEBONDED 11 INCHES UP FROM THE BOTTOM OF THE RUDDER. REPAIRED RUDDER PER SRM 55-41-19-300-006.SDR HNAA2024070500504Skin · chafedE038379 RUDDER 1 EXTERNAL SKIN CHAFED JUST ABOVE ACCESS PANEL 326EL. PERFORMED DOUBLER REPAIR FOR RUDDER 1 EXTERNAL SKIN JUST ABOVE ACCESS PANEL 326EL IAW ETD2024-145-015198 AND EO1-55-24-0357SDR HNA2024F00001Skin · damaged00105 TOP RH AFT CORNER OF RUDDER 1 DAMAGED. REMOVED DAMAGE IAW EMB 145 51-10-05 STEP #3 DAMAGE DID NOT PENETRATE CLAD LAYER.
Back to JASC 5542