JASC 5100
Service difficulty reports · 4,244
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 VNAA202301160002Beam · not reportedFUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR COMPLY WITH SB 670BA53040C. COMPLIED WITH SB 670BA-53-040 FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS2SDR VNAA202301160001Beam · not reportedCENTER FUSELAGE, BS 669.40 - 855.40, REPLACEMENT OF THE BEAMS AT LBL 36 AND RBL 36; AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH THE BEAMS INSTALLED AT BL 0; LBL 9, LBL 18, LBL 27, RBL 9, COMPLY WITH SB 670BA-53-036D. PERFORMED CENTER FUSELAGE, SDR DALA2023071405720Unknown · unknownSHIP 3248 NEED TO ACCOMPLISH ERA 605147-14AD SECTION I (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA 605147-14AD SECTION 1. (2583816)SDR DALA2023011700362Unknown · noneDOOR 1R DISARM PIN WILL NOT FIT IN HOLE AND STAY IN PLACE. PERFORMED OPERATIONAL TEST OF ARMED/DISARMED CONTROL HANDLE MECHANISM IAW AMM A330-300 TASK 52-12, NO MAL FUNCTIONS FOUND. (9841946)SDR FDEA202301140094None · noneAGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITHSDR YENA2023011800055None · noneDURING HEAVY MAINTENANCE: ACCOMPLISH SB A320-53-1158. ACCOMPLISHED REPAIR IN ACCORDANCE WITH SB A320-53-1158 AND EA 53-0652-22 REV 0. AND PART 1 THRU 4 AND RDAF 80263435/045/2022#A,SDR SWAA2023011791781Slide · noneFWD ENTRY DOOR SLIDE PRESSURE IS IN THE RED. INDICATOR NEEDLE IS NOT COMPLETELY OUT OF THE GREEN GO BAND PER AMM 25-66-01 FWD ENTRY DOOR SLIDE IS SERVICEABLE.SDR DALA2023011700316Skin · noneEVIDENCE OF REWORK EXTERNAL SKIN STATIC PORT LOCATED BETWEEN FR23 TO FR24 LH SIDE LOWER FUSELAGE. REWORKED AREA PER A320 SRM 53-11-11. OK FOR SERVICE.SDR DALA2023011600305None · noneDURING TAKEOFF ROLL AT 110 KNOTS, ATC COMANANDED CREW ABORT TAKEOFF DUE TO CONFILICTING TRAFFIC. T/S IAW AMM CHP 05-51-07-210-801. NO DEFECTS ON ALL TIRE ASSY AND BRAKES ASSY. INSPECTED T/R FOR DEFECTS NO DEFECTS NOTED. C/W TIRE PRESSURES CHECKS, ALL WITHIN LSDR DALA2023011700359None · noneSUPPLEMENTAL INFORMATION SHIP 3302 AIRPORT AUTHORITY REPORTED AIRCRAFT LANDED SHORT AND DAMAGED RUNWAY LIGHT. CORRECTIVE ACTION: PERFORMED DETAILED VISUAL INSPECTION, FOUND RH MLG BRAKE ROD, CABLE ASSY BROKEN. REPLACED BRAKE ROD RESTRAINT CABLE. (6602784)SDR SWAA2023011791911None · none<SDR DALA2023011300295None · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN 48 INCHES FWD OF DOOR L2 1 FOOT BLOW ENGINE SCAN LIGHT AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED DETAIL VISUAL INSPECTION OF THE INSTALLED DOUBLER LOC.EXTERNAL FUSELAGE SKIN 48 INCHES FWD OF DOOSDR DALA2023011300268None · noneSHIP 3229 NEED TO COMPLY WITH ERA 600256-14 REV A. (2579957) CORRECTIVE ACTION: COMPLIED WITH. (2579957)SDR DALA2023011300266None · noneSHIP 3229 NEED TO COMPLY WITH ERA 600256-14 REV A (CRACK) CORRECTIVE ACTION: COMPLIED WITH. (2579947)SDR FDEA2023011320081None · noneAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDESDR FDEA2023011320080None · noneAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDESDR SCNA20230113040None · noneFUEL SMELL NOTED IN PAX CABIN AS CREW ENTERED AIRCRAFT : RESOLUTION: GASOLINE SMELL WAS NOTED PRE TAXI. AUTO FUEL SMELL WAS ATTRIBUTED TO GAS POWERED HEAT CART PREVIOUSLY ATTACHED TO A/C.SDR DALA2023011300261None · none2L DOOR SLIDE LIGHT WILL NOT EXTINGUISH. NO DEFECTS NOTED, CYCLED ARMING MECHANISM. OPS CHECK NORMAL. OK FOR SVC. (9224380)SDR UIEA2023011100014None · noneDURING DEPARTURE IN CLIMB OUT, ACFT ENTERED AREA OF SEVERE TURBULENCE & W/S, ACFT INDICATED O/S OF 285, SPEED TAPE WITH NO ASSOCIATED OVERSPEED WARNINGS IAW 05-51-04, DATA FROM OUR ENGINEERING TEAM SHOWS AIRCRAFT DID NOT SHOW "G" LOADS OF SEVERE TURBULENCE. NOSDR IPXA2023012490218None · noneINSPECTION TYPE:SEG2, MAJOR REPAIR, EXISTING REPAIR WAS FOUND AT BS 1460 STRINGER 25L TO 27. LINSPECTED REPAIR IAW EO B757-531027182-C. ORIG SUBMISSION DATE: 1/24/2023SDR DALA2023011300289None · none(LOG 9370105) BORROWED EMERGENCY EXIT BATTERY PACK FROM UNITED. INSTALLED IN OVERHEAD PANEL AT L1 DOOR.SDR 2023FA0000023None · noneUNDERSTANDING OF THE 1ST GENERATION FUEL SELECTOR FOR PIPER AIRCRAFT. SEE SB 840A, SAIB CE-14-22, SB 1309A, PIPER SB 355, SA-075. PILOTS ARE INADVERTENTLY SELECTING THE OFF POSITION DUE TO CONFUSION / MISUNDERSTANDING OF THE FUEL SELECTOR POINTER.SDR ABXA2023032942Skin · corrodedDURING C22 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND CORROSION DAMAGE ON THE RH WING LOWER SKIN PANEL NO. 3 APPROX., INBOARD OF WS 176.69 BETWEEN STR 11 AND STR 12. THE CORROSION DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA WITH MINIMUM REMAINING SDR DALA2023012200463None · noneWHILE ACCOMPLISHING WORK SECTIONS 2330-01337-42 AND -43, IT WAS NOTED THAT CHANGES ARE REQUIRED TO WORK INSTRUCTIONS. VA 99841 CAPTURES THESE CHANGES. ACCOMPLISH VA 99841 REV C IN CONJUNCTION WITH WORK SECTIONS 2330-01337-42 AND -43.SDR 2023FA0000019None · noneGULFSTREAM GVII-G600 INCLUDES GULFSTREAM STC ST04324AT-D THAT INCLUDES AN ELECTRICALLY OPERATED 'FORWARD CABIN POCKET DOOR'. THE GULFSTREAM PASSENGER BRIEFING CARD DOES NOT ADDRESS THE LOCATION OR INSTRUCTIONS FOR PASSENGER OPENING/EXISTING THROUGH THIS DOOR SDR YENA2023011300041None · noneFLT#1073, JFK-BNA. 'AIRCRAFT ENCOUNTERED MOD TO SEVERE TURB. AFT GALLEY CART FELL OVER; PERFORMED SEVERE TURBULENCE CHECK IAW AMM 05-50-28-210-801-A. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.'SDR UIEA2023010800005Bolt · mechanic error#1 ENG IDG QUAD RING BOLT IS SAFETY WIRED BACKWARDS. REMOVED & REPLACED #1 ENG IDG QUAD RING BOLT SAFETY WIRED IAW BOEING 767-300 REF AMM 24-11-01.SDR DALA2023010900120None · noneL1 DOOR SLIDE INDICATOR LIGHT INOP OR DAMAGED. COULD NOT DUPLICATE FAULT ON GND. NO 90 DAY HISTORY. OK FOR SVC.SDR DALA2023011200239None · noneAMOC, ERA 604474-14AD. REPAIR AT EXTERNAL FUSELAGE SKIN, FR25-26 AND STRG43-44 REQUIRES AMOC FOR AD 2020-20-05. REVISE/UPDATE ERA 604474-14AD WITH AMOC TO AD 2020-20-05 RESULTS PRIOR TO 12,638 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 14-604474 ADDED FOR AC 3015. (SDR DALA2023011200238None · noneDTE, ERA 604474-14AD, REPAIR AT EXTERNAL FUSELAGE SKIN, FR25-26 AND STRG43-44 REQUIRES DTE PRIOR TO 12/30/2023.REVISE/UPDATE ERA 604474-14AD WITH DTE RESULTS PRIOR TO 12/30/ 2023. ASSOCIATED ER/A 14-604474 ADDED FOR AC 3015. (LP# 2570671)SDR DALA2023010900109None · noneSHIP 3230 AFTER FRAME 10 REPAIR COMPLETED ON LOG PAGE: 2530550 ENGINEERING REDESIGNATED REPAIR AS TIME LIMITED (BIRD DAMAGE) CORRECTIVE ACTION: COMPLIED WITH ERA 604384-14 REV. ORIG SECTION IIISDR DALA2023010900108None · noneSHIP 3230 AFTER FRAME 9 REPAIR COMPLETED ON LOG PAGE: 2530575 ENGINEERING REDESIGNATED REPAIR AS TIME LIMITED. CORRECTIVE ACTION: COMPLIED WITH ERA 604384-14 REV. ORIG SECTION II. (2570767)SDR DALA2023010900107None · noneDAMAGE FOUND DURING GVI IN PILOT REPORT OF BIRD STRIKE. DAMAGE LOCATED ON R/H OF A/C ABOVE AND AFT OF FIRST OFFICERS WINDOW FWD OF FRAME 12. CORRECTIVE ACTION: COMPLIED WITH PRI 603956-14 REV 2. (2570664)SDR DALA2023010600101Structure · pilot errorDURING WALKAROUND, MAINTENANCE DISCOVERED TAIL STRIKE DAMAGE TO THE FUSELAGE BELLY SKIN AND THE AFT GALLEY DRAIN MAST. THERE IS DAMAGE TO MULTIPLE FUSELAGE SKIN PANELS FROM BS 1714 - 1744, BETWEEN STRINGERS 29L AND 29R. ERA 604938-14.SDR 2023FA0000002None · noneDURING MAINTENENCE INSPECTION FOUND EXISTING BLEND OUTS AND CORROSION ON FUSELAGE SKIN BETWEEN STA 196 AND STA 2220 BELOW WINDOW L3, CLOSE TO PITOT STATIC.SDR 2023F00022None · pilot errorPILOT RETURNED TO AIRPORT AFTER LOSS OF AC POWER DUE TO INADVERTENTLY BUMPING THE INVERTER SWITCH TO THE OFF POSITION. MAINTENANCE CHECKED THE INVERTER SWITCH AND INVERTERS AND NO FAULT WAS FOUND. IT IS RECOMMENDED THAT THE 3 POSITION TOGGLE SWITCH BE REPLSDR DALA2023010500076None · noneSHIP 670 REF ERA 596391-14 REPETITIVE INSPECTIONS NEEDED ON REPAIRED INTERCOSTALS. CORRECTIVE ACTION: REF ERA 596391-14. (2567298)SDR DALA2023010500075None · noneSHIP 5645 COMPLY WITH ERA 604846-14AD REV ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH ERA 604846-14AD REV ORIGINAL. (2567111)SDR DALA2023010400063None · noneR3 DOOR KNUCKLE KNOCKER DOES NOT SPRING BACK IN WHEN DOOR IS DISARMED FA PURSER IN BY HAND, IT STAYS IN. OPS NORMAL NO PROBLEM FOUND.SDR FDEA202301040024Unknown · smokeCREW REPORTS MEM TOWER CONTACTED FLT 0700 OTBD AT800' DURING CLIMBOUT OF POSSIBLE SMOKE COMING FROM THE FUSELAGE TAIL AREA. AMM 05-50-00-02 PERFORMED GVI OF ENTIRE AIRCRAFT WITH ATTENTION TO TAIL AREA. NO VISIBLE SIGNS OF LEAKS OR SOOT. NO ABNORMAL FLIGHT SDR QMLA2023010420001None · noneINSTALLED HOVERLIGHT. USING WIRING DIAGRAM HD 135-05-8011, NOT COMPLIANT WITH AC 43.13-1B SECTION 4 PARA 11-48, DETERMINATION OF CIRCUIT BREAKER RATINGS. 25 AMP CALLED FOR IN WIRING DIAGRAM, 30 AMP CURRENT DRAW POSSIBLE.SDR CALA2023010400019None · noneROBBED AFT LEFT EMERGENCY LIGHT POWER SUPPLY BATTERY REF AMM 33-51-06-960-806. C/B''S PULLED AND TAGGED. ROBBED PARTS TAG SECURED ON CANNON PLUG AT AFT GALLY AREA. REPLACED BATTERY PACK FOR POWER SUPPLY IN AFT GALLEY IAW AMM 33-51-06-960-805. OPS CHECK GOOD.PASDR DALA2023010400052None · noneA/C DEPARTED ICE COVERED TAXIWAY. INSPECTED AIRCRAFT. NO DAMAGE FOUND.SDR DALA2023010600096Skin · handler errorBAG CART HIT A/C ON LEFT SIDE STA 500D S-21L. DAMAGE BETWEEN STA 500C TO 500E ALONG S-21L. PERFORMED REPAIR PER PRI 604740-14 REV 0,1,2. TASK OF PRI 604740-14 REV 0,1,2.SDR DALA2023010400059None · noneESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS FOR L1 DOOR SLIDE ENGAGE LIGHT INOPERATIVE. REINSTALLED GIRT BAR IAW AMM 52-11. . PERFORMED GIRT BAR SYS TEST IAW AMM 52-11. TEST PASSED.SDR DALA2023010400058None · noneOBSTRUCTION OF VIA SAT SHEAR TIES ON FS 1260 FRAME. REF ERA 604846-14. (2564591)SDR DALA2023010300028Access Panel · crackedAFTER REMOVAL OF ACCESS PANEL 532DZ, A CRACK WAS FOUND. THE ACCESS PANEL WAS REPAIRED IAW ERA 604797-14 REV ORIG, AND ERA 604797-14 PRI REV 1.SDR CALA2023010200011Skin · handler errorDURING JETBRIDGE CONNECTION TO THE AIRCRAFT THE JETBRIGDE CONTACTED THE AIRCRAFT FUSELAGE FWD OF D2L . INSPECTED DENT REF SRM 53-00-01 SHEET 3 PARA B,F,I,J.. DENT IS OUT OF LIMITS BUT MEETS ALL CRITERIA LISTED IN PARAGRAPH "I". APPROVED FOR DIP PER THIS SRM WISDR IPXA2023041177371Unknown · crackedL/H HORIZ STAB UPPER CHORD CRACKED AT AFT END ACCOMPLISHED R/R OF CHORD AS PER SRM 51-40-02SDR 2023F00078None · defectiveECAM WARNING ENG 1 BOWED ROTOR DISPLAYED DURING FLIGHT PH 02, APU INOPERATIVO
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