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 DALA2024041504408Skin · damagedSHIP 3248 DISC: RUDDER T/E AND I/B FLAP LOWER SURFACE DAMAGE BY LIGHTNING STRIKE. C/A: ACCOMPLISHED ER/A 617122-14 REV O SECTION I: TIME LIMITED REPAIR. (LP: 5346634)SDR LR7A2024032803409Skin · damagedDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5511, FOUND RUDDER SKIN TRAILING EDGE DAMAGED AT FS1155, BL0, VSS206. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001108528. / PSE# 55-10-09, AD 2012-06-09SDR CALA2024032500850Skin · damaged(B737-27-3-2708) RUDDER T/E L/E SIDE HAS POSSIBLE STATIC DISCHARGE DAMAGE. RUDDER T/E L/H SIDE AT RUD STA 103.35; .5" X 1.0" IAW B737-900ER SRM 55-40-01-2R-1 REPAIR 1 TABLE 20 1 AND 51-70-05-2R-6 REPAIR 6. FINAL REPAIR DIMENSION 4.5 X 2.25 WEIGHT AND BALANCSDR DALA2024032003503Cap · damagedSHIP 3102 LIGHTNING STRIKES ON RUDDER CAP ON TRAILING EGDE. CORRECTIVE ACTION: INSTALLED NEW RUDDER TIP REF A319 AMM 55-41-11. (0252354)SDR ASAA2024022949608Skin · contaminatedTRAPPED WATER INDICATION FOUND: ON R/H SIDE OF RUDDER AT NO. 20 FASTENER LOCATION ADJACENT TO HOIST POINT #3. AREA MARKED IN RED, 6"L X 2.5"W, 5" FWD OF T/E. DOT: B633 GROUNDED - YES. ACCOMPLISHED A PERMANENT REPAIR ON R/H SIDE OF RUDDER AT NO. 20 FASTENER LOSDR IPXA2024032608357Skin · damaged*SUPPLEMENTAL SDR* LIGHTNING STRIKE DAMAGE FOUND BETWEEN GAP OF THE UPPER RUDDER AFT UPPER CORNER AND LOWER AFT TRAILING EDGE VERTICAL STAB SKIN- MARKED WITH TAPE REPAIRED LIGHTNING STRIKE DAMAGE REF EO-89659-REQ 4. THIS REPAIR IS PERMANENT D ITEM IS CLEAR. RESDR IPXA2024030108357Skin · damaged*SDR FILED OPEN* LIGHTNING STRIKE DAMAGE FOUND BETWEEN GAP OF THE UPPER RUDDER AFT UPPER CORNER AND LOWER AFT TRAILING EDGE VERTICAL STAB SKIN- MARKED WITH TAPE SUBMITTED TO ENGINEERING FOR REPAIR.<BR>ITEM REMAINS ON DEFERRAL.SDR DALA2024012901277Skin · dentedSHIP 3155 DENT ON RH STABILIZER LEADING EDGE TIP. CORRECTIVE ACTION: REPAIRED PER SRM 55-14-11-283-001. (5374363)SDR SWIA2024032600121Skin · chafedRUDDER LEADING EDGE SKINS ARE CHAFFED. (C-CHECK RO 3/23/2024) REMOVED DAMAGE AT MULTIPLE LOCATIONS ON L/H AND R/H RUDDER LEADING EDGE SKINS REF CRJ700 SRM 51-12-00-001-001-A01COMPLIED WITH ALL STEPS 1-4 REF REO 670-55-41-134 REV --, DATED 2024-02-09. COMPLSDR EBVR450D122723001Skin · corrodedREPAIRED RUDDER LEADING EDGE CORROSION, IAW RFTS-109106 REV. 0 & SRM 51-40-03. REPAIR THE UPPER FUSELAGE BLENDED AREA LOCATION ABOVE THE ENGINE PYLONS IAW RFTS-108948 REV.0 . REPAIR THE BLENDED AREA ON THE LT FUSELAGE AT APPROXIMATELY BS 501 ON THE TOP SIDE SDR DALA2023121110117Unknown · unknown(LOG 4308620) RUDDER TRAILING EDGE DAMAGE APPROX 4 FEET UP FROM BOTTOM AFT CORNER. REPAIRED PER B737-800 SRM 55-40-01.SDR AALA202312123446Skin · contaminatedAIRCRAFT IN BASE MAINTENANCE: RUDDER LEFT HAND SIDE SKIN PANEL HAS EVIDENCE OF MOISTURE INGRESS AT 12.5 INCHES ABOVE THE #1 HIOST POINT AND 15.5 INCHES FORWARD OF THE RUDDER TRAILING EDGE. REPAIRED RUDDER SKIN PANEL PER SRM 55-41-13-300-024.SDR DALA2023112109571Unknown · unknownCRACK ON REAR SPAR RUDDER ACCESS PANEL 1. SUMMARY OF NRC 00312: REAR SPAR RUDDER ACCESS PANEL 1 WAS REPAIRED PER B717-200 SRM 55-00-00-2R PROCEDURE 2, REPAIR 2, PARAGRAPH A, FIGURE 201. (LP #0074053)SDR HNAA2023112100449Unknown · unknownE003545 RUDDER 2 HAS TWO LIGHTNING STRIKE HOLES AFT OF LOWER CENTER HINGE FITTING. CUT OUT DAMAGE, PERFORMED DOUBLER REPAIR ON RUDDER 2 AT TWO LIGHTNING STRIKE HOLES AFT OF LOWER CENTER HINGE FITTING IAW ETD2023-145-026628 REV A AND EO1-55-23-0371SDR CALA2023102303161Skin · contaminatedRUDDER LH LOWER HOIST POINT #1 HAS POSSIBLE WATER INTRUSION ON LOWER AFT AREA. REPAIRED RUDDER LH SKIN LOWER FWD HOIST POINT #2 LOWER AFT AREA 2.5 IN BY 2IN ZONE O IAW A319 SRM 55-41-13-300-030 CATEGORY ARE PAIR .SDR CALA2023101603079Skin · dented(SUPPORT TASK) RUDDER RH LOWER SIDE HAS A DENT. W/C:69985 REPAIRED RH LOWER SIDE IAW SRM 55-41-13-300-024 PARA 2 STEP 2. W /C:69985 STA:STENGBFM INSPECTIONS ACCOMPLISHED ON ST ENGINEERING NRC#69985 AT STA:STENGBFMSDR JGVR20231005002Unknown · unknownREPAIRED CORRODED AREAS ON THE RUDDER LEADING EDGE NEAR THE BALANCE WEIGHT HARDWARE BY BLENDING AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING AND INSTALLING REPAIR DOUBLERS PER NETJETS REQUEST FOR SDR CALA2023091102757Panel · damagedDURING THERMOGRAPHIC INSPECTION OF THE L/H RUDDER SIDE PANEL, NDT NOTES WATER INGRESS AT THE 12TH FASTENER FROM TOP AT 6.75" FROM THE TRAILING EDGE. INDICATION MEASURES AT 3.5" X 3.0". () LH RUDDER SIDE PNL REPAIRS COMPLETED AS REQUIRED SRM 55-41-13-30 0-025 CSDR CALA2023091102755Panel · damagedDURINGTHERMOGRAPIC INSPECTION OF THE L/H RUDDER SIDE PANEL, NDT NOTES WATER INGRESS AT THE 11TH FASTENER FROM THE TOP AT 6.25" F ROM THE TRAILING EDGE. INDICATION MEASURES AT 4.75 X 3.25" () LH RUDDER SIDE PNL REPAIRS COMPLETED AS REQUIRED- SMR 55-41-13-3 00-0SDR CALA2023091102756Panel · damagedDURING THERMOGRAPHIC IINSPECTION OF THE L/H RUDDER SIDE PANELS, NDT NOTES WATER INGRESS AT THE 4TH FASTENER FROM TOP AT 6.5"FROM THE TRAILING EDGE. INDICATION MEASURES AT 4.0" X 3.25". () LH RUDDER SIDE PNL''S REPAIRED AS REQUIRED IAW SRM''S 55-41-13-300 -025/SDR AALA202308107829Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RUDDER SKIN LOCATED AT RUDDER STA 276.240. REPAIRED SKIN PER SRM 55-40-01-2R-2.SDR SWI2023F00420Unknown · chafedRUDDER LEADING EDGE SHROUD LH SIDE CHAFED. (C-CHECK RO 10/4/2023) BLENDED OUT RUDDER LEADING EDGE SHROUD LH SIDE PER CRJ-700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH REO 670-55-41-124 REV -- DATE 2023-08-16COMPLIED WITH TASK 51-900-1002-SKYSDR IPXA2025062346359Skin · dentedLOWER FORWARD RUDDER DENT .084" DEEP 1.25" W X 1" L APPROX 54" DOWN AND 8" AFT FROM LE ++COMPLETED ALL STEPS OF EO-94072-REQ1. THIS IS A PERMANENT REPAIR. THIS CLOSES DEFERRAL.SDR FDEA202306151043Skin · delaminatedRUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 10" FWD OF THE AFT EDGE REPAIRED R/H EXTERNAL SURFACE OF RUDDER APPROX 8FT UP FROM THE FUSELAGE ,APPROX 10" FWD OF AFT EDGE BY REMOVING DAMAGE , CLEANING AREA , LAYING UP RESDR FDEA202306151042Skin · delaminatedRUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 27" FWD OF THE AFT EDGE REPAIRED RUDDER , R/H EXTERNAL SURFACE , APPROX 8FT UP FROM THE FUSELAGE , APPROX. 27" FWD OF THE AFT EDGE BY REMOVING DAMAGE , CLEANING , LAYING UP SDR DALA2023062605133Unknown · unknownSHIP 0686 PUNCTURE ON CAPTAIN SIDE OF RUDDER APPROXIMATELY 2 FEET FROM TRAILING EDGE AND 1 FOOT FROM BOTTOM OF RUDDER. CORRECTIVE ACTION: ASSOCIATED ER/A 14-609672 ADDED FOR AC 0686 COMPLIED WITH PRI 609672-14, REV.0, REV. 1, REV. 2, REV. 3, ALL STEPS. FINAL ESDR DALA2023072105918Unknown · unknownSHIP 3116 CORROSION RUDDER TOP SURFACE HINGE BEARING 6 ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED HINGE BEARING #6 ON VERTICAL STABILIZER AS PER A320 FAM AMM 55-46-11-000-001-A AND AMM55-46-11-400-001-A. (2803695)SDR A6WA202305128602Rudder · dentedDENT ON LH RUDDER RS 125.44-RS131.17 *******AIRCRAFT REMOVED FROM SERVICE****** REPAIRED DENT ON LH RUDDER AT RS125.44-RS131.17 AND FOUND TO BE ACCEPTABLE PER REO. DENT DIMENSION L = 1.500Ï¿½ X W = 1.150Ï¿½ X D = 0.027Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. SDR HALA2023032800126Unknown · unknownSHIP 383 RUDDER BOTTOM TRAILING EDGE FOUND CRACKED AND CORRODED. 4.0" CRACK FROM BOTTOM OF RUDDER TRAILING EDGE. CORRECTIVE ACTION: RUDDER APEX STRIP REPAIR CARRIED OUT. CARRIED OUT ELECTRICAL RESISTANCE TEST OFTHE TRAILING EDGE. FOUND NIL DEFECT. PAINTING CARSDR AALA202303240589Rudder · delaminatedAIRCRAFT IN BASE MAINTENANCE: RUDDER TRAILING EDGE DELAMINATED. REPLACED RUDDER ASSEMBLY PER TASK CARD 26L32027002.SDR AALA202303157304Rudder · unknownAIRCRAFT IN BASE MAINTENANCE: TRAPPED WATER INDICATION FOUND ON RUDDER SIDE PANEL LEFT HAND HONEYCOMB CORE STRUCTURE BETWEEN RIB 6 AND RIB 7 AND 4.75 INCH FROM RIB 7 AND FASTENER 27 TO 28 AND 2.88 INCH FROM THE TRAILING EDGE. MAINTENANCE REPAIRED RUDDER PER SRSDR CALA2023020600337Not Reported · not reportedR/H RUDDER SIDE PANEL PRODUCED AN INDICATION OF WATER INGRESS AP PROX. 178-186INS. FROM BOTTOM AND 2-6INS. FROM T/E. {A3NB-55-3-6 024} PER HAECO NON ROUTINE 9290079/22079 GENERATED BY V061690 AT HAECO LCQ REPAIRED RUDDER PN D5547100200000B TS-2319 178 TO 186 ISDR VNAA202302021111Not Entered · not enteredRH RUDDER SKIN STA136.90 - STA148.86 DENTED. PERFORMED PERMANENT REPAIR IAW EA 23-C9-55-0029-IR_APPROVED.SDR LR7A2023010403253Skin · damagedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RUDDER SKIN CREASED AT FS1191, LBL8, WL285-360. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000802283.SDR IPXA2022102787560Skin · damagedINSPECTION TYPE:3CNO REPAIR DOUBER HISTORY ON RUDDER ASS AFT UPPER SKIN STA ZV = 487.312 R/H AFT SIDE.REMOVED, REPAIRED EXISTING REPAIR DOUBLER ON AFT UPPER RUDDER AT STA ZV = 487.312 IAW VT-SAA EA 011-5540-01-A9730 REV I/R AND UPS EO C-5540-85056-A AND FAA FOSDR IPXA2022092786654Skin · corrodedINSPECTION TYPE:3CUPPER RUDDER LOWER ROUND ACCESS AREA HAS CORROSION ON LIP AND SKINREMOVED AND REPLACED ASSY UPPER AFT RUDDER PER MD11 AMM 27-20-30SDR 7C7A2022061600021Rudder · dentedDENT ON FORE RUDDER L/H SIDE BETWEEN RIB 19 AND 20. REPAIRED WITH DOUBLER PATCH IAW DHC RD8-55-3763SDR HALA2022052000183None · noneSHIP 381 FOUND FIBREGLASS DAMAGE AT SKIN NEAR RUDDER HINGE #8 (TOP OF RUDDER). CORRECTIVE ACTION: REMOVAL OF RUDDER CARRIED OUT IAW AMM NO 27-21-41. RUDDER SENT TO WORKSHOP FOR REPAIR REPAIR ON RUDDER CARRIED OUT AS PER ER/A 599354-14. REINSTALLED RUDDER. (224SDR HALA2022052000182None · noneSHIP 381 DURING INSPECTION ON RUDDER (P/N: F5547108400000; S/N: TS6235), FOUND DISBOND/DELAMINATION AND FLUID INGRESS IN ZONE P AT T/E SCREW NO. #1, #8, #10, #11 & #14. CORRECTIVE ACTION: REMOVAL OF RUDDER CARRIED OUT IAW AMM NO 27-21-41. RUDDER SENT TO WORKSHSDR SWIA202264892None · noneRUDDER CENTER HINGE FITTINGS BEARINGS HAVE PLAY (UPPER CENTER HINGE & LOWER CENTER HINGE) (C-CHECK RO 3/11/2022) REMOVED NO.2 AND NO.3 RUDDER HINGE ASSY. REF. CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH RIL#1231 RESDR DALA2021122107925None · none(LOG 7833031) DURING INSPECTION FOUND 2 EA SMALL BURN MARKS ON UPPER TRAILING EDGE OF RUDDER. C/C PERMANENT REPAIR PER B 737-800 SRM 55-40-01-2R.SDR 7C7A2021102700035None · noneDENTS ON TRAILING RUDDER R/H SKIN BETWEEN RIBS 4 - 5 & 19 - 20. REPAIRED IAW RD8-55-3680SDR 7C7A2021102200026None · noneDENT BETWEEN RIBS 9 & 10 ON R/H SIDE OF TRAILING RUDDER, REPLACED SKIN DHC-8-100 SRM 55-40-28.SDR 7C7A2021102200025None · noneDENT ON LH SIDE TRAILING RUDDER BETWEEN RIBS 4 & 5 REPLACED SKIN DHC-8-100 SRM 55-40-28.SDR SWIA202163785None · gougedAIRCRAFT RUDDER MIDDLE HINGE FITTING , HINGE LUG AT STATION 92.94 HAS 2 GOUGES , AS MARKED . (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON RUDDER MIDDLE HINGE FITTING AT STA. 92.94 PER REO 670-55-41-093 REV-- DATED 2021-10-14. REFERENCE CONTINUATION CARD FSDR DALA2022091406089None · noneREPEAT INSPECTION PER ER/A 594509-14 REQUIRED EVERY 3000FC AFTER REPAIR INSTALLATION. REPAIR IS APPLIED TO RUDDER SN 55010 INSTALLED. ASSOCIATED ER/A 00-594509 ADDED FOR AC 9503. REDEFERRED LOG TO QC, ESTABLISHED MONITOR INSP. ERA 594509-14 REV A IS NOW CURRENSDR DALA2022091406088None · noneESTABLISHING DTE RESTRICTION FOR ER/A 594509-14. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM THE APPROVAL DATE. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONT SERVICE BEYOND THIS LIMIT. REPAIR IS APPLIED TO RUDDER SN 55010 ISDR CALA2021081601339Skin · puncturedR/H SIDE OF RUDDER HAS THREE EACH PUNCTURES AT APPROXIMATELY SIX TRAILING EDGE SCREWS UP AND FORWARD AS MARKED A3NB-55-3-6024 PE R HAECO LCQ NR 9296161/20161. REPAIRED RH SIDE OF RUDDER 3 EA AREAS AT SIX T/E SCREWS UP AND FWD IAW UAL ECRA 5541-01052 AND REO-LSDR CALA2021080901299Skin · damagedSUPPORT TASK: RUDDER DAMAGED AT TRAILING EDGE BETWEEN STA 190 AN D STA 140 DUE TO CONTACT WITH LIFT. TRANSCRIBED FROM HAECO GSO NRC# 9282712 REPAIRED RUDDER DAMAGE AT TRAILING EDGE BETWEEN STA 190 AND STA 140 DUE TO CONTACT WITH LIFT IAW B757-300 SRM 55-40-01SDR FDEA202108042286Skin · damagedN00074: 1EA WATER TRAPPED AREA(50MM X 50MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.10 FASTENER. ACCOMPLISHED THE WORK : LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1 , SEQ NO:1122 AND SRM 55-41-12-2
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