JASC 5350
Service difficulty reports · 6,123
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 SWAA2021111723078Panel · corrodedPANEL 145AL GROUND WIRE SCREW EDGES (DOOR SIDE) SHOW SURFACE CORROSION. REMOVED PANEL 145AL IAW SRM 51-40-02-0G-0. REMOVED CORROSION AT PANEL 145AL GROUND WIRE SCREW EDGES IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM PART 4 51-00-00SDR SWAA2021110122965Access Panel · crackedCRACK ACCESS PANEL 195CL BODY FAIRING AT LOWER FUSELAGE ; 2021-435902 / [23] REPAIRED ACCESS PANEL 195CL BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW.; [24] TASK COMPLETEDSDR SWAA2021092823019Panel · elongatedPANEL#194E HAS WORKING COUNTERSINKS AND ELONGATED HOLES. ; PANEL#194E HAS NUMEROUS WORKING COUNTERSINKS AND ELONGATED HOLES. / [01] REMOVED AND REPLACED PER AMM 53-51-21.SDR SWAA2021092823020Panel · elongatedPANEL#193D HAS NUMEROUS WORKING COUNTERSINKS AND ELONGATED HOLES. ; / [01] REMOVED AND REPLACED PANEL PER AMM 53-51-21.SDR SWAA2021110122359Web · crackedCRACK WING TO BODY FAIRING, BS 540, S22 - 24R. REPLACED I.A.W B737-700 SRM 51-40-02.SDR DALA2021101206259None · noneSHIP 3307 A FACESHEET PUNCTURE WITH PARTIAL CORE DAMAGE COMMON TO WING-TO-BODY FAIRING PANEL 191AB. MTC REPORTED AN AREA OF DELAMINATION SURROUNDING THE PUNCTURE. THE 'W' DISTANCE TO THE SANDWICH EDGE IS NOT MAINTAINED. CORRECTIVE ACTION: REFERENCE ER/A 594358SDR SWAA2021100422215Fairing · delaminatedFUSELAGE FAIRING PANEL 193AR HAS A DENT AND AREA DELAMINATED ; / [01] REMOVED DAMAGED PLIES AT PANEL 193AR AS PER B737-700 SRM 51-70-04 GENERAL ; PARAGRAPH 4.B. NO WATER FOUND; [02] PREPARED DAMAGED AREA FOR REPAIRAS PER B737-700 SRM 51-70-04-2R-1; [03] LATE ESDR SWAA2021100422214Panel · delaminatedPANEL 191AR DELAMINATED AT 4 SCREWS ATTACHMENTS POINT AREA ; / [01] REMOVED PANEL#191AR FOR ACCESS TO REPAIR AT R/H FORWARD WING TO BODY FAIRING PANEL PER B737-700 AMM 53-51-21-000-803.; [02] MEASUREMENTS; [03] CLEANED AREA AND PREPARED AREA FOR REPAIR ON DAMASDR DALA2021092305732None · noneSHIP 3250 CRACK SUPPORT WEB BELLY FAIRING LOCATED FR 47 AT LEVEL STR 40L TO STR 41L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 593858-14 PRI REV.0 AND ER/A 593858-14 REV. ORIGINAL. (1957714)SDR SWAA2021110121402Access Panel · crackedCRACK ACCESS PANEL 194E WING TO BODY FAIRING AROUND HOLES AT LOWER FUSELAGE ; 2021-435714 / [31] REPAIRED ACCESS PANEL 194E WING TO BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. SEE INDIVIDUAL SIGN OFFS BELOW.; [32] STEP 31 ENTRY BSDR SWAA2021110121403Access Panel · crackedCRACK ACCESS PANEL 193D WING TO BODY FAIRING AROUND HOLES AT LOWER FUSELAGE ; 2021-435715 / [28] REPAIRED ACCESS PANEL 193D WING TO BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. SEE INDIVIDUAL SIGN OFFS BELOW; [29] STEP 28 ENTRY BYSDR DALA2021092305739None · none(LOG 1955123) DURING INSPECTION FOUND WING TO BODY PANEL 194D HAS OVERSIZED FASTENER HOLE. REPAIRED OVERSIZED FASTENER HOLE ON WING TO BODY PANEL 194D IAW B737 SRM 51-70-05-2R.SDR DALA2021092305738None · none(LOG 1955113) DURING INSPECTION FOUND WING TO BODY PANEL 194DL HAS CRACKED FASTENER HOLES. WING TO BODY PANEL 194DL CRACKED FASTENER HOLES REPAIRED IAW B737 SRM 53-60-70-2R-1 TABLE 202 AND IAW B737 SRM 51-70-05-2R-8.SDR DALA2021092305737None · none(LOG 1955098) DURING INSPECTION FOUND WING TO BODY PANEL 194D HAS DAMAGE ALONG THE AFT EDGE BAND. REPAIRED DAMAGE ALONG THE AFT EDGE BAND ON WING TO BODY PANEL 194D IAW B737 SRM 51-70-05-2R.SDR SWAA2021092320146Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021092320148Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021092321045Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021092321047Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR DALA2021092005630None · none(LOG 1953294) DURING INSPECTION FOUND FAIRING SUPPORT STRUCTURE AT STA 727+2.7 BL0 TO LBL 55 HAS DAMAGE. REMOVED AND REPLACED FAIRING SUPPORT STRUCTURE AT STA 727+2.7 BL0 TO LBL 55 IAW B737 SRM 53-60-71-1A-1, SRM 51-40-02-0G0, SRM 51-40-05-0G0, AND B737 AMM 53SDR SWAA2021101419980Panel · elongatedKEEL BEAM ACCESS PANEL 194E HAS NUMEROUS FASTENER HOLES ELONGATED AND ENLARGED. ; / [01] REMOVED DAMAGE AT ELONGATED HOLES PER SRM 51-70-05-2R-8.; [02] C/W DAMAGE REMOVAL INSPECTION PER SRM 51-70-05-2R-8.; [03] DUPLICATE WRITE UP FAULT WILL BE REPAIRED ON FAULSDR SWAA2021101420878Panel · elongatedKEEL BEAM ACCESS PANEL 194E HAS NUMEROUS FASTENER HOLES ELONGATED AND ENLARGED. ; / [01] REMOVED DAMAGE AT ELONGATED HOLES PER SRM 51-70-05-2R-8.; [02] C/W DAMAGE REMOVAL INSPECTION PER SRM 51-70-05-2R-8.; [03] DUPLICATE WRITE UP FAULT WILL BE REPAIRED ON FAULSDR SWAA2021101420883Panel · elongatedKEEL BEAM ACCESS PANEL 193B FASTENER HOLES ENLARGED. ; / [01] REMOVED AND REPLACED PANEL 193B PER SRM 51-40-02; [02] C/W INSPECTIONSDR IPXA2021100574614Frame · damagedINSPECTION TYPE:3CFWD TAIL CONE R/H FWD UPPER FRAME IS DAMAGED.REPAIRED DAMAGED FRAMED AT THE FWD TAIL CONE IAW MD-11 SRM 53-80-07 REPAIR 1. (MINOR)SDR SWAA2021100420962Panel · deterioratedPANEL 193AR HAS A DISBOND ON INNER SURFACE 19' FROM IB EDGE; 7' FROM FWD EDGE ; / DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.A(6)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 PER SRM 53-40-70-2R-1 PARA 4.B(1) - 4.D(1)SDR SWAA2021100420961Panel · crackedPANEL 191D HAS SEVERAL CRACKED/PULLED THROUGH FASTENER HOLES ON PANEL EDGEBAND ; / FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-70-1A-1 PAR 4.B (6).<BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 AS DIRECTED PER SRM 53-30-70-2R-1 PAR 4SDR IPXA2021093074440Frame · damagedINSPECTION TYPE:C3FWD TAIL CONE L/H FWD FRAME IS DAMAGED AT THE UPPER GUIDE PIN.REPAIRED DAMAGED FWD TAIL CONE L/H FWD FRAME AT UPPER GUIDE PIN IAW SRM 53-80-07 REPAIR 1. (MINOR)SDR IPXA2021093074438Frame · damagedINSPECTION TYPE:C3FWD TAIL CONE L/H FWD FRAME IS DAMAGED AT CTR GUIDE PIN.REPAIRED DAMAGED FWD TAIL CONE L/H FWD FRAME AT CTR GUIDE PIN IAW SRM 53-80-07 PEPAIR 1. (MINOR)SDR CALA2021091501586Seal · leakingLOUD BANGING NOISE RIGHT SIDE OF A/C ROW 31 ON CLIMBOUT. DTV SEAL FAILED THE BULBSEAL ORDERED COULD NOT BE INSTALLED DUE TO REMOVAL OF ECRA BY ENGINEERING FOR IT, SO CALLED LIVE TV AND THEY GAVE ME AN UPDATED FOR FAIRING WITH SEAL ALREADY INSTALLED P/N 73SK210SDR IPXA2021093074434Tail Cone · damagedINSPECTION TYPE:3CTAIL CONE R/H UPPER INTERNAL PRODUCTION DOUBLER HAS WEAR/CHAFE DAMAGE.REPAIRED DAMAGED TAIL CONE R/H UPPER INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-B. (MINOR)SDR DALA2021091505503Radome · damagedRADOME REPAIR PER ERA 588183-14. RADOME SKIN/CORE REPAIRED PER ERA 588183-14. REPETITIVE INSPECTION PER ERA 588183-14 SECTION II REQUIRED EVERY 850 HRS UNTIL ACCOMPLISHMENT OF PERMANENT REPAIR PER SECTION III AT 8500 HRS. ASSOCIATED ER/A 14-588183 ADDED. (LP# SDR DALA2021091005362Support · damaged(LOG 1942941) DURING INSPECTION FOUND FAIRING SUPPORT STRUCTURE AT STA 727+2.7 FROM STRINGER 27L TO STRINGER 27R HAS FRETTING DAMAGE ON LOWER SURFACE. COMPLIED WITH ER/A 593900-14AD.SDR DALA2021091005361Support · damaged(LOG 1942934) DURING INSPECTION FOUND FAIRING SUPPORT STRUCTURE AT STA 727+2.7 STRINGER 27R HAS DAMAGE TO REPAIRED FASTENER HOLE. COMPLIED WITH ER/A 593900-14AD.SDR SWAA2021091315938Fairing · damagedWING TO BODY FAIRING PANEL 193B FASTENER HOLES ENLARGED AT LOCATIONS 1 - 36 AND 38 / [01] C/W REMOVED AND REPLACED PANEL 193B REF SRM 51-40-02; [02] REMOVED AND REPLACED PNL 193B REF SRM 51-40-02; [03] C/WSDR SWAA2021101115449Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 193D FOR WING TO BODY FAIRING. EVALUATED AND FOUND WITHIN LIMITS IAW SRM 53-40-70-2R-1, REPAIR 1, PARAGRAPH 2.B(1)(B). INSTALLED FILLER PLIES ON REPAIR AREA IAW SRM 51-70-05-2R-8 PAR 4D TO F. DRILLED AND COUNTERSUNK FASTENER SDR YENA2021091700579Skin · dentedDURING HEAVY MAINTENANCE, DENT ON TAIL CONE SKIN BTW FR 100 +72 / FR 100 +76 AND STRGR 01R-02R; (REF TECHOPSMX WO# 1654 NR# 00184) TAIL CONE SKIN BTW FR 100 +72 TO FR100 +76 AND STGR 01R - 02R WAS REPAIRED PER EMB190 53-31-01/REPAIR 51P(SKIN CUTOUT DOUBLER RESDR DALA2021090705271Panel · damaged(LOG 1938785) DURING INSPECTION FOUND LOWER FUSELAGE PANEL 193D,16EA AFT FASTENER HOLES DAMAGED. REPAIRED 16EA FASTENER HOLES ON LOWER FUSELAGE PANEL 193D IAW SRM 53-40-70-2R AND B737 SRM 51-70-04-2R REPAIR 9.SDR DALA2021090705270Panel · chafed(LOG 1935288) DURING INSPECTION FOUND FUSALAGE PANEL 193D CHAFING ON AFT EDGE 3 PLACES. REPAIRED CHAFING ON AFT EDGE IAW B737 SRM 53-40-70-2R AND B737 SRM 51-70-05-2R ON FUSELAGE PANEL 193D ASSOCIATED AA 5352-01035.SDR DALA2021090705269Panel · gouged(LOG 1935310) DURING INSPECTION FOUND FUSELAGE PANEL 193D GOUGED 3 PLACES L/H O/B SIDE. REPAIRED GOUGES ON L/H O/B SIDE ON FUSELAGE PANEL 193D IAW B737 SRM 53-40-70-2R AND B737 SRM 51-70-05-2R ASSOCIATED AA 5352-01035.SDR DALA2021090705225Tail Cone · out of adjustMULTIPLE WIRTEUPS FOR TAIL CONE CAM RIGGING. RAM 1. PLEASE REMOVE TAIL CONE AND INSPECT ALL ATTACH FITTINGS CABLES BRACKETS AND CAMS PER AMDS WORK CARD 5352-4013. 00-0000-3-0001. ADJUSTED TAILCONE RELEASE CAM REF B717 AMM 53-52-03. (LP #1935731)SDR DALA2021090305223Cam · cockedTHE TAILCONE RELEASE CAM IS CLOCKED WRONG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0115:5352-4002/002 00349: ADJUSED TAILCONE RELEASE CAM REF B717 AMM 53-52-03. (LP #19344SDR DALA2021090305221Conduit · dentedTHE CONDUIT FOR TAILCONE RELEASE CABLE IS DENTED, RT SIDE LOWER AREA (MARKED). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0265:5300-2004/007 00082: REPLACED CONDUIT AND TAILCSDR SWAA2021092713982Panel · crackedSUPPLEMENTAL INFORMATION: PANEL 194BL FWD LOWER FASTENER HOLE IS PULLED THROUGH AND CRACKED ; / [01] IDENTIFIED PANEL 194BL IAW SRM 53-60-70-0I-1 TABLE 2 FIGURE 2 ITEM 10. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PARASDR SWAA2021090313321Panel · puncturedFAIRING PANEL 193B PANEL SCREW HOLES ELONGATED AND INNER SURFACE PUNCTURED ; / [01] R&R CENTER WING TO BODY PANEL 193B PER AMM 53-51-21.SDR DALA2021083105135Cam · out of positionTHE TAILCONE RELEASE CAM IS CLOCKED WRONG AND OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 001-0115:5352-4002/001 00303: ADJUSTED TAILCONE RELEASE MECHANISM CAM REF SDR DALA2021083005129Fairing · damaged(LOG 1927749) DURING CCK AT QRO, WHILE PERFORMING EM 5352-01035-02 INSPECTIONS TO THE LOWER AFT WING TO BODY FAIRING PANEL 194E AND SUPPORT STRUCTURE, ELONGATED HOLES (QTY 7) WERE FOUND COMMON TO THE NUT HOLES ON THE STA 727+2.7 & 727C SUPPORT FRAMES. MAINTENASDR SWAA2021100412686Panel · crackedPANEL 191AL INNER SURFACE; FWD LOWER CORNER IS CRACKED AT CORE ; / [01] IDENTIFIED PANEL 191AL IAW SRM 53-30-70-0I-1.FIG 2; ITEM [1]. FOUND DAMAGE AT 3' FROM FWD EDGE; 2'FROM LOWER EDGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1.PARA 4.A.(1). REQUIRESSDR FDEA202108272119Attach Bracket · crackedEXTERIOR FUSELAGE NOSE RADOME HOLD OPEN ROD STOWAGE PIN ATTACH BRACKET IS DEFORMED ON THE LEFT FWD BULKHEADS WALL (ZONE 111) REMOVED DAMAGED BRACKET , INSTALLED SERVICEABLE BRACKET IAW DWG 141N7835 AND B757 SRM 51-40- 02-0GSDR UIEA2021082701883Support · crackedFUS - LH BODY FAIRING 191KL SUPPORT AT STA 1241 UPR AND LWR EDGE CRACKED.(<P>FX-STA 1003-1253.5 LH UNDERWING O/B FAIRING INTERCOSTL P/N: 65B11234-39 CRACK AREA REPAIRED IAW RI NO: RI-53-00-14821 REV A.</P>)SDR UIEA2021082701890Support · damagedLHW O/B NO. 2 FAIRING I/B SUPPORT LONGERON FOUND DAMAGED.(<P>LHW O/B NO. 2 FAIRING I/B SUPPORT LONGERON P/N 65B15595-3 CRACK AREA REPAIRED IAW RI-57-00-14820 REV A.</P>)SDR ASMF202110015Radome · damagedDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL DAMAGES ON NOSE RADOME. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING SEVERAL DAMAGES OUT OF LIMITS ON NOSE RADOME OF LOSS OF MATERIAL COMPOUND IN 2 AREAS OF 3.00" DIAMETER; SO THE NOSE RADOME ASSY WAS REPL
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