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 DXTA200601410Computer · pilot errorDURING TAKE OFF ROLL ENGINE SET PARAMETER DID NOT MATCH TAKE OFF CONDITTION. - OBSERVED TAKE OFF POWER FOR THE DAY, NOTICED TEMPERATURE ROSE SIGNIFICANTLY. RECALCULATED PERFORMANCE USING CURRENT TEMPERATURE AND ENGINE PERFORMED NORMALLY IAW GULFSTREAM G200 AFMSDR 06FDEA1986None · noneEXISTING REPAIR FOUND AT NR 2 ENGINE PYLON RT AND LT SKIN. EXISTING REPAIR AT NR 2 ENGINE PYLON RT AND LT SKIN EVALUATED AND FOUND REPAIR PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 361906-14 EO 1-5100-7-5001 TITLE:"STRUCTURES-REPAIR CASDR DJFA2006248Duct · leakingKLAS - KLAS TRIP ID# 1018611 FOLLOWING DEPARTURE FROM KLAS WHILE CLIMBING THROUGH 4,000 FT THE CREW RECEIVED A REAR BAY OVERHEAT INDICATION. EMERGENCY ACTIONS OF CLOSING THE MAIN AIR VALVES AND OPENING THE FLIGHT DECK AIR VALVES WERE ACCOMPLISHED. THE REARSDR 06FDEA1900Repair · misinstalledCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON RT FLOOR SUPPORT STRUCTURE ABOVE DEPRESSURIZATION VALVE FS 1091, FS 12A. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPRSDR 06FDEA1898Repair · misinstalledCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON LEFT SIDE BULK CARGO COMPARTMENT CROSSBEAM FS 3630-3663, FS 67-68 AND Y73. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APSDR 06FDEA1896None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON RIGHT SIDE BULK CARGO COMPARTMENT CROSSBEAM FS 3514-3567, FR 65-66 AND Y91. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA SDR 06FDEA1892None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON RIGHT SIDE MCD FLOORBEAM FS 1870, FS 34 AND Y56 TO Y79. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. RESDR 06FDEA1890None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON LEFT SIDE MCD SEAT TRACK FS 1923-2029, FS 35-37 AND YD95. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPSDR 06FDEA1883None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT AILERON LOWER SURFACE WS 444-459. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1882None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE RT FLAP VANE LOWER SURFACE INBD OF NUMBER TWO FLAP TRACK. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. SDR 06FDEA1877None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE RT OUTBD FLAP T/E WEDGE UPPER SURFACE OUTBD OF NUMBER THREE FLAP TRACK, WS 913-933. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR . NEW REPAIR ACCOMPLISSDR 06FDEA1872None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT OUTBD FLAP LOWER SURFACE, OUTBD OF NUMBER THREE FLAP TRACK. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DSDR 06FDEA1871None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT INBD FLAP T/E WEDGE LOWER OUTBD SURFACE, WS 337-427. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. RSDR 06FDEA1870None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT INBD FLAP T/E WEDGE UPPER, OUTBD SURFACE, WS 352-385. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. RSDR 06FDEA1869Repair · unknownCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT INBD FLAP T/E WEDGE UPPER SURFACE, WS 118-170. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLSDR 06FDEA1868None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT INBD FLAP T/E WEDGE UPPER SURFACE, WS 103-116. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLASDR 06FDEA1867None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT INBD FLAP T/E WEDGE UPPER AND LOWER SURFACE, WS 40-103. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1865None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE L1 DOOR UPPER AFT CORNER, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1864None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED LT FS 3938-3956, FS 73 AND STR 53-54, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1860None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED LT FS 1067-1091, FS 12-12A, FLUSH REPAIR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1856None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED LT FS 3998-4059, FS 74-75 AND STR 2-5, FLUSH REPAIR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING RSDR 06FDEA1854None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED LT FS 3779-3832, FS 70-71 AND STR 27-28, EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1787Repair · unknownREPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STA 304-328 LONGERON 26L-38L. OPS 1401/ T 8-5330-86848 COMPLIED WITH CARD T-8-5330-83848-FUSELAGE-REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STA.304-328 LONGERON 26L-38L. MAJOR SDR 06FDEA1791Repair · unknownFOUND EXTERNAL DOUBLER AT BS 360-380, STR 24R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED NEW REPAIR PER SRM 53-30-3 FIG 3A.SDR 06FDEA1786None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT LT ELEVATOR INBOARD UPPER SURFACE WAS ACCOMPLISHED IAW SRM 55-20-3 FIG 1 PAGE 1, BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANSSDR 2006F00025Canister · openSMOKING ON SHUT DOWN. OPENED RIGHT SIDE COWLING AND FOUND THE END OF THE EPA/JOHN'S CAN COMPLETELY OPEN. END PLATE FOUND IN BOTTOM OF COWLING. TT PRESUMED TO BE ORIGINAL.SDR 2006F00024Canister · openSMOKING ON SHUT DOWN. OPENED RIGHT SIDE COWLING AND FOUND THE END OF THE EPA CAN COMPLETELY OPEN. END PLATE FOUND IN BOTTOM OF COWLING. TT PRESUMED TO BE ORIGINAL.SDR 06FDEA1722None · nonePREVIOUSLY REPAIR INSTALLED AT STA 710, STR 21L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 2 PAGE 9. BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS.SDR 06FDEA1721None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT LT FWD ENTRY DOOR HINGE CUTOUTS WAS ACCOMPLISHED IAW EA 7-5330-28325, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP SDR 06FDEA1706None · noneFOUND REPAIR LOCATED AT STA 410 STR 15 RT, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSSDR 06FDEA1707None · noneFOUND REPAIR LOCATED AT STA 203 STR 28R REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITSDR 06FDEA1708None · noneFOUND REPAIR LOCATED AT STA 1050 STR 29L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 2, REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 SDR 06FDEA1704Repair · unknownREPAIR REQUIRED AT UNUSED MOUNTING BASE HOLES OF ANTENNA (P/N S65- 5366-890L QTY 04 EACH) AFTER ITS REMOVAL AS PER EA1-2310-94626 STEP 18 REQUIREMENT, SNRM N01696: SKIN REPAIR AT BS 839-879 LONGERON 51L-51R AND INNER DOUBLER AT BS 859-879 LONGERON 51R-52. INSDR 06FDEA1705None · noneFOUND REPAIR LOCATED ON AFT CARGO DOOR REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DETERMINED TO BE IAW SRM 52-00-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLSDR 06FDEA1700None · noneDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: FOR CUSTOMER REQUEST REPLACE HORIZONTAL STABILAZER CONSTANT SECTION UPPER SKIN PANEL 7. REMOVED AND REPLACED PLANK NR 7 IAW S/B 55-16 FOLLOWING INSTRUCTION AS PER PAR 2, PAGE 17-18, OPTION II. SINGLE PANELSDR 06FDEA1695Repair · unknownEXTERNAL DOUBLER AT BS 695, STR 28L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPAIRED EXTERNAL DOUBLER AT BS 695 STR 28L IAW SRM 53-30-3 FIG 3A.SDR 2006UALA00863Unknown · unknownSIDEWALL PANEL LOCATED AT ROW 15F IS HOT TO THE TOUCH (SCALE OF 1-10 IT'S AN 8) JUST BELOW WINDOW AROUND EMERGENCY EXIT OVER WING DOOR. SIDEWALL LOCATED AT SEAT ROW 15F FELT HOT TO THE TOUCH. EXCESSIVE HEAT WAS CAUSED BY THE OVERWING EXIT HATCH THRESHOLD HEATSDR 06FDEA1658None · noneTRUNNION ATTACH FITTING MODIFICATION. COMPLIED WITH EO 7-5710-7-2314D PT5 WINGS MLG TRUNNION ATTACH FITTING.SDR 06FDEA1653Repair · noneFOUND FLUSH REPAIR LOCATED AT RIGHT HORIZONTAL STAB STA XE98 TO XFS 175 UPPER. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED DOUBLER IAW DC10-10 SRM 51-31-01 VOL II, 55-0SDR 06FDEA1623None · noneBUSHING REPAIR ON BRACKET RIGHT WING. PERFORMED INSPECTION ON REPAIR BUSHING FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA1622Repair · unknownLWR FUSELAGE LT HAND SIDE HAS AN EXTERNAL DOUBLER REPAIR IN SKIN BETWEEN STA 1741 AND 1761 LONG 37 TO 39. REMOVED AND REPLACED REPAIR IAW SRM 53-20-00 FIG 6 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01197/I011197 IAW SRM 53-20-00 FIG 6 SHT 3-4 VOL 1SDR EIA2006062Unknown · unknownPRIOR TO TAKEOFF, AIRCREW REPORTS UNKNOWN FLASH OF LIGHT OUTSIDE LEFT SIDE WINDOW. NO ENGINE PARAMETER SHIFT NOTED, LEFT MWTS GEAR THERMALED AT GATE. WAITING FOR IRREGULARITY REPORT AND LOG PAGES FOR FURTHER INFO.SDR 06FDEA1610Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1140 STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-30-3 FIG 5 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHSDR 06FDEA1607Repair · unknownFOUND SINGLE RIVET REPAIR LOCATED AT STA 184 FWD OF NOSE ACCESS DOOR, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA1587None · noneEXISTING REPAIR FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED ABOUT 76 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).SDR 06FDEA1572Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1070, STR 21R IS NOT CONFORMED TO FAA APPROVED DATA, REMOVE EXISTING REPAIR AND FABRICATED REPAIR PARTS IAW SRM 53-30-3 FIG 3, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6SDR 06FDEA1570Valve · leakingAFTER TAKEOFF HEARD LOUD BANG AND PRONOUNCED BURNT RUBBER SMELL IN PERMEATE FLIGHT DECK, SUSPECTED BLOWN TIRE. LOWERED GEAR AND RETURNED FOR LANDING. INSP NOSE GEAR, NOSE TIRES, AND NOSE STEERING, NOSE BRAKES, PACK COMPTS, CANS, FWD AVI COMPT ALL RACKS, CNTSDR 06FDEA1567Repair · misinstalledFUSELAGE SKIN REPAIR AT FS 1140 & STR 19L DOES NOT COMPLY WITH SRM REPAIR. REMOVED AND REPLACED EXISTING REPAIR DOUBLERS IAW SRM 53-30-3 FIG 5.SDR 06FDEA1553Repair · unknownFOUND SKIN EXTERIOR SIDE WITH EXTERNAL LONGITUDIANL REPAIR DOUBLER AT PACK 2 ACCESS DOOR 113AL (REF EO 1-5100-7-5001).SDR 06FDEA1541Repair · noneAFT CAC BULKHEAD STA 1159 FOUND DOUBLER AT X-83 AND DOUBLER AT X-84. PERFORMED GVI ON BULKHEAD CAC FOUND IN COMPLIANCE WITH CRITERIA BY EO #8-5100-7-5001 P1, INITIAL INSPECTION PERFORMED IAW EA NR 8-5330-95700.
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