JASC 5100
Service difficulty reports · 4,235
Reports filed under 5100 · Standard Practices/Structures, 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 = '5100' 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 = '5100' 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 FDEA202409201665Repair · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH CTR FLAP NOSE SKIN BTW RIB 23~24 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14SDR YENA2024092401296Doubler · unknownDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / WASTE ACCESS DOUBLER / CORROSION TEMPORARY REPAIR; REFERENCES: /1/ AIRBUS REO-500-53-61-1378_-- /2/ AVIANOR NRC A49107-1009. DESCRIPTION: DURING CURRENT C1 CHECK (08/2024) ON N3085J (MSN: 55132) AT YMX, AVIANSDR CALA2024092000666Drain Line · unknownREF LOG 9270379 FOR NON HAZARDOUS FWD GALLEY CLEANUP REF ECRA 2011-01000 WITHIN 7 DAYS, ACCOMPLISH EC/RA 2011-01000, GALLEY SPILL, SECTION 2.B., IN-DEPTH CLEANUP, IN APPROXIMATE AREA FROM BODY STATION STA 6570 TO STA 7087 BETWEEN STRINGERS 23 TO 28 OKAY TO CASDR DALA2024092109279Switch · malfunctionedSHIP 3521 -ATB- DUE TO LOSS OF AFDX SWITCH CAUSING FIVE PAGES OF DISPATCH MESSAGES. CORRECTIVE ACTION: RESET AFDX SWITCH AND CLEARED FAULTS. REPLACED AFDX SWITCH AS PRECAUTION. (LP 5261684)SDR QMLA2024092020121Sealant · damagedFUEL SMELL IN CABIN BY MED CREW, INSPECTED FOR FUEL LEAKS, NONE FOUND. REAPPLIED SEALANT TO PREVENT FUEL VENT FROM ENTERING CABIN. THIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE.SDR DALA2024092009268Slat Track · no discrepancyLH SLAT TRACK NBR 3 LOWER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP BD500-A-J51-01-20- 01AAA-353A-A. NO DEFECTS NOTED. (LP# 0565088)SDR IPXA2024092758398Drain · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR IPXA2024092758498Drain · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR IPXA2024091858498None · no discrepancy**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)SDR IPXA2024091858398None · no discrepancy**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)SDR REXA2024100400837Bracket · unknownWHILE INCORPORATING SB 670SH-53-043 REV C, R/H VOLUMETRIC FUSE BRACKET P/N: SH698-75355-1 FOUND TO NOT WORK WITH EXISTING A/C FASTENER HOLES (LOW ED). COMPLIED WITH MHIRJ EO SH698-75355 SNIEO S10 ALL STEPS 1-5. STEP #3 IS NOT REQUIRED DUE TO THE PART BEING FASDR IPXA2024091841773Unknown · noiseDURING CLIMB THROUGH 10,000 EXPERIENCED A VERY LOUD NOISE AND VIBRATION WITH A TEMPORARY BURNING SMELL THAT LASTED APPROX TWO MINUTES. SUSPECT NOSE WHEEL ROTATION. EMERGENCY DECLARED, PERFORMED GVI OF AIRFRAME, NOSE WHEEL AND WHEEL WELL, FLIGHT BRAKE BAND. TISDR DALA2024091709117Skin · no discrepancySHIP 670 FUSELAGE SKIN / EXISTING REPAIR BETWEEN STA 1340 STA 1360 AND S-1 S-2R. ER/A 501040-14AD REV C. CORRECTIVE ACTION: REF ERA 501040-14. (0559857)SDR SWAA2024101040226Paint · wornON TOP OF THE LEFT HAND WING; THE PAINTED ESCAPE MARKINGS HAVE WEAR.<[01] REFINISHED WING EXIT PATHWAY PER AMM 11-24-04.;[02] INSPECTED WORK PERFORMEDSDR CALA2024091700649None · noneBIRD STRIKE LOWER LEFT NOSE BIRD STRIKE. INSPECTED BIRD STRIKE PER AMM TASK 05-51-18-210-801. BIRD STRIKE WAS NOT ON THE NOSE RADOME BUT ON THE LH SIDE UNDER CAPTAINS SLIDING WINDOW. NO BIRD REMAINS FOUND IN ENGINE #1 OR ANY PART OF A/C. NO DENTS OR NOTICABLE SDR REXA2024100400836Fitting · noneWHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL 05/2022 FOUND FITTINGS AT STR12A LH AND RH SIDES PN CC670-33562-001SB AND CC670-33563-001SB CAN NOT BE INSTALLED IAW SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING FASTENER PITCH ON THE AIRCRAFT. REPAIRED SDR FDEA202409111291Doubler · no discrepancyAGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER STATION XOS 663 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER STATION XOS 663 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-02-2R RESDR UIEA2024091000890Unknown · unknownDEVIATION - FOUND DURING PERFORMING NWW MODIFICATION CHORD (P/N = 65B07942U76) CONTOUR CAN'T MATCH.(<P>1. PERFORM EI NO: T2024A53M-1852 SEQUENCE A REV= 0 2. PERFORM EI NO: T2024A53M-1852 REV= 1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR FDEA202409101268Frame · no discrepancyAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT STATION 5-73, LONGERON 12 RIGHT (FRAME) EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT STATION 5-73 LONGERON 12 RIGHT HAND SIDE (FRAME) EVALUATED AND FOUND REPAIRED IAW SRM 53-00-07- 2R REPAIR SDR SIMA202409107001Unknown · no discrepancyLOUD POP FROM UNDERNEATH FLIGHT DECK SUSPECT IT CAME FROM BAG IN CARGO COMPARTMENT EMERGENCY DECLARED. PERFORMED GVI OF CARGO COMPARTMENT AND WALK AROUND IAW 05-50-00 AMM NO DEFECTS NOTED AT THIS TIMESDR IPXA2024090631666Drain · no discrepancy*SUPPLEMENTAL SDR* ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO 8217. COMPLETED SDR.SDR IPXA2024090531666Drain · no discrepancy*SDR FILED OPEN* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.SDR AALA202411198977Fitting · noneAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING PER EA 357766, THE RIGHT HAND CONTINUITY FITTING NEEDS TO BE REPLACED. BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 357766.SDR CALA2024090302370None · noneBIRD STRIKE. INSPECTION REQUIRED PER AMM. BIRD STRIKE ABOVE CAPT L1 WINDOW. CAPT STATED FLEW THROUGH RAIN AND MOST WASHED OFF. APPROX 1SQ INCH OF BIRD REMAINS REMAINED AFTER A/C BLOCKED INTO GATE PERFORMED BIRD STRIKE INSPECTION IAW 05-51-18-210-801 WITH NO DASDR SIMA20240831001Unknown · damagedAIRCRAFT REQUIRES A MAJOR REPAIR AIRWORTHINESS RELEASE IAW GPM 12-05 PER ERS EJ 57MR 1620 & ERS-EJ-53MR-5044. (MAJOR REPAIR). C/W MAJOR REPAIR AIRWORTHINESS RELEASE IAW GPM 12-05 PER ERS EJ 57MR 1620 & ERS-EJ-53MR-5044SDR IPXA2024090671665Drain · no discrepancyFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO 82173. COMPLETED.SDR FDEA202408311224Elevator · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV LWR SKIN AT ER10 PLUS 22", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 SDR FDEA202408311223Elevator · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV LWR SKIN AT ER5, T/E-6" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.70SDR FDEA202408311222Elevator · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER13 PLUS 38", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 SDR FDEA202408311221Elevator · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER13 PLUS 31", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR FDEA202408311220Elevator · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER13-3.5", T/E-10" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 SDR FDEA202408311219Elevator · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER10 PLUS 11", T/E-5.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMESDR FDEA202408311218Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEV UPR SKIN AT ER7 PLUS 16", T/E-14.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR IPXA2024083171665None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.SDR UIEA2024082800852Screw · missingZONE 100, LOWER HALF FUSELAGE, MID E/E, MISSING SCREW AND WASHER ON SMOKE DETECTOR.(<P>ZONE 100, LOWER HALF FUSELAGE, MID E/E, ON SMOKE DETECTOR. ZONE 100, LOWER HALF FUSELAGE, MID E/E, SCREW AND WASHER WERE INSTALLED CORRECTLY IAW AMM 26-16-01-400-801-001 REVSDR 2024FA0000675Bearing Race · unserviceableOVERRUNNING CLUTCH INNER RACE PN-369F5455-1 FAILED MD HELICOPTER CSP-COM5 CH 63-10-15 TABLE 502 NDT TESTING.SDR 2024F00245Glide Slope · no discrepancyDURING ILS APP DUAL CMD A/P DISCONNECTS AND FO`S F/D DISAPEARS AT GLIDESLOPE CAPTURE. NOTE: PERFORMED ILS OPERATIONAL TEST IAW TASK 34-31-00-710-801. FOUND NORMAL A/C OK FOR SERVICE.SDR DALA2024082908566None · noneSHIP 3330 NEED TO COMPLY WITH ERA 611252-14. CORRECTIVE ACTION: COMPLIED WITH ERA 611252-14. (0527030)SDR IPXA2024082752510Drain · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR TIMA20240823010None · noneDEPARTED VFR FROM GPI, CLIMBED TO 14000 VFR. SAW WEATHER ON GPS, DEVIATED LEFT/NORTH OF COURSE TO STAY AWAY FROM THUNDERSTORM AND LIGHTNING. ENTERED IMC AROUND 14500 AND ENCOUNTERED UPDRAFTS GREATER THAN 2800FPM, MOD RIME ICE, HAIL, CLOUD TO CLOUD LIGHTNING. SDR AALA202408223461Unknown · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AFTER TAKEOFF SNA TOWER INFORMED US OF LIQUID LEAKING FROM RIGHTSIDE OF AIRCRAFT. ALL COCKPIT INDICATIONS WERE NORMAL. FUEL LEAK QRH PROCEDURE APPLIED, NO FUEL LEAK NOTED; AIRCRAFT DIVERTED TO AND LANDEDSDR IPXA2024082938616None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDRSDR AALA202408235177None · noneAIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN - AN EXTERNAL SKIN DOUBLER IS PRESENT AT BS 500 LOCATED BETWEEN STR 2L AND STR 3L. THIS MAJOR REPAIR IS NOT RECORDED ON THE HSDA REPORT AND NEEDS TO BE DOCUMENTED PER GPM 17.31.1. REPAIRED IN ACCORDANCE. PER SRM 53-0SDR KCSA2024081922Structure · ground damageAIRCRAFT ROLLED FORWARD AFTER ENGINE START STRIKING VAN CAUSING DAMAGE AIRCRAFT RIGHT. AIRCRAFT DAMAGE INSPECTED, REPAIRED, AND LEAK CHECKED IAW E-52 #11533, DWG 52302402-1, 53302408-1 REV OR AND AMM 21-31-00 B747-400 REFERENCE M44 JOB CONTINUATION FORM FOR ADSDR IPXA2024081938616Drain · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPENSDR SIMA20240818001Unknown · unknownATC DECLARED EMERGENCY FOR SUSPECTED BLOWN TIRE. THE FLIGHT CREW THOUGHT THEY MAY HAVE BLOWN A TIRE DEPARTING CRP. BUT AFTER LANDING IN DFW AND AT THE GATE THE FLIGHT CREW PERFORMED THEIR POST FLIGHT WALK AROUND AND FOUND NO EVIDENCE OF A BLOWN TIRE AND OPTEDSDR JJBA20240819014Unknown · noiseLOUD GRINDING SOUND AT 1000 FEET. SOUNDED LIKE STRUCTURAL FAILURE, WENT AWAY AFTER 5 SECONDS. ALL SYSTEMS CHECKED AND FLIGHT CONTROLS FELT NORMAL, THEN AT 27000 FEET IT HAPPENED AGAIN. FLOOR VIBRATED AND CONTROLS. WENT AWAY AFTER 5 SECONDS. PERFORMED GVI ON RUSDR YENA2024082001129Unknown · unknownDURING HEAVY MAINTENANCE: FLIGHT CONTROLS - ELEVATOR AILERON COMPUTER SYSTEM (ELAC) - INSTALL SOFTWARE STANDARD L104 ON ELAC B WITH DATA LOADING CAPABILITY ON CEO, SUPPORTING SAFETY BEYOND STANDARD FUNCTIONS; REFERENCES /1/ AIRBUS SB A320-27-1305 /2/ AIRBUS RISDR DALA2024101490280Skin · cracked-AD- PD: FASTENER HOLE CRACKS CA: **LIMITED RELEASE** REPAIRED PER BOEING DWG 59360610 REV AC & ER/A 620349-14AD SECTION 1, REV ORIGINAL **NOTE: ER/A 620349-14AD, REV ORIGINAL.SDR IPXA2024082088154Panel · crackedPANEL 613AB CRACKED AT NUTPLATE HOLE INSTALLED (2EA) DOUBLERS FOR THE STR Z600-PANEL 613AB IAW A300-600 SRM 53-15-63A AND SRM 51-40-21.
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