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.

SDR FDEA201502240588Valve · unknownIAW MOCC REQUEST NEED TO R & R DEPRESSURIZATION VLV 93 HM. PART ON ORDER. R & R DEPRESSURIZATION VLV 93 HM IAW 21-31-15-04-01.Feb 24, 2015 · N430FE · Airbus A310203SDR DALA2015022601686Unknown · unknownUPON BLOCK IN DOOR 4R WILL NOT DISARM. FAULT COULD NOT BE DUPLICATED. CYCLED ARM/DISARM LEVER.Feb 24, 2015 · N711ZX · Boeing 757231SDR DALA2015022501630None · noneREMOVED OTBD RT SEAT TRACK FROM STA 589 TO STA 746 TO FACILITATE OVERWING FRAME REPLACEMENT DUE TO AD MANDATED OVERWING FRAME INSPECTION FINDINGS.Feb 24, 2015 · N894AT · Boeing 717200SDR DALA2015022401723None · noneDURING INSPECTION, CONFIRM AT EVALUATION FOR POSSIBLE FCS REPAIR. ON EXTERNAL SKIN LT PAX DOOR LOCATION BETWEEN XP 662 AND XP 297 AND BETWEEN BEAM 7 AND BEAM 6. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN L1 PAX DOOR LOCATED BETWEEN XP 662 AND XP 297 AND BETWFeb 23, 2015 · N327NW · Airbus A320211SDR DALA2015022301796Structure · damaged2 EACH HOLES DAMAGED ON INSIDE OF 1809 FWD CORD, COMMON TO THE SKIN ON LT SIDE BELOW LOWER DAMAGE.Feb 22, 2015 · N125DL · Boeing 767332SDR UHLA2015022200118None · noneTHE CREW REPORTED THAT THEY SUSPECTED A FUEL LEAK IN THE RT WING TANK DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RT WING SURFACES AND PERFORMED OPS CHECKS OF THE FUEL SYSTEM WITH NO LEAKS OR DEFECTS NOTEDFeb 22, 2015 · N266SK · Emb EMB145LRSDR DALA2015022301594None · noneMAINTENANCE COMPLIED WITH VA 90134MA, REV A FOR ASSOCIATED AA 2520-01919.Feb 21, 2015 · N377DA · Boeing 737832SDR DALA2015022301591None · noneMAINTENANCE COMPLIED WITH VA REV IR FOR AA 2340-01075.Feb 21, 2015 · N377DA · Boeing 737832SDR DALA2015022301590None · noneMAINTENANCE COMPLIED WITH VA 90146 FOR ASSOCIATED AA 2500-01777.Feb 21, 2015 · N377DA · Boeing 737832SDR DALA2015022301588None · noneMAINTENANCE COMPLIED WITH VA 90138MA, REV IR ASSOCIATED AA 2520-01937.Feb 21, 2015 · N377DA · Boeing 737832SDR DALA2015022301587None · noneMAINTENANCE COMPLIED WITH VA90132 MA, REV A FOR ASSOCIATED AA 2330-01337.Feb 21, 2015 · N377DA · Boeing 737832SDR DALA2015022301592None · noneMAINTENANCE COMPLIED WITH VA 90132MA, REV B FOR ASSOCIATED AA 2330-01337.Feb 20, 2015 · N377DA · Boeing 737832SDR SWIA201540796Skin · gougedRT LOWER FORWARD CORE COWL INBD AFT AREA OF ACOC PANEL LANDING IS GOUGED. C-CHECK, FABRICATED AND INSTALLED REPAIR PATCH FOR FWD CORE COWL INBD AFT AREA OF ACOC PANEL IAW REO.Feb 19, 2015 · N603SK · Cndair CL6002C10SDR DALA2015022601652Structure · handler errorJETWAY DAMAGED, FUSELAGE AFT OF L1 DOOR. COMPLIED WITH EAR 533293-14, SECTION I AND ER 533293-14, SECTION II.Feb 19, 2015 · N926DH · Doug MD9030SDR DALA2015022301589None · noneMAINTENANCE COMPLIED WITH VA 90135MA, REV IR ASSOCIATED AA 2520-01938.Feb 18, 2015 · N377DA · Boeing 737832SDR SWIA201540788Panel · crackedPANEL 222FLW CRACKED, MARKED. C-CHECK REPAIRED PANEL IAW EA AND COMPLIED WITH ST. WORK DONE IAW EA.Feb 13, 2015 · N963SW · Cndair CL6002B19SDR FDEA201502120520None · noneINCOMING REPAIR, STATION 1580 FRAME BETWEEN STRINGER 25L - 26L. DOES NOT COMPLY WITH CURRENT SRM.Feb 12, 2015 · N771FD · Boeing 757222SDR DALA2015032402341None · noneER/A 478209-14AD, REV B, FUSELAGE SKIN, STA 1675-1688 AND STR 18L-20L, DENT AND GOUGE REPAIR, SUPPLEMENTAL INSPECTIONS. CLEARED AREA FOR LFEC ERA 478209-14 C/W LFEC INSPECTION IAW ERA 478209-14, REV B SECTION II NO CRACKS FOUND. RESTORED AREA TO ORIGINAL CONFeb 10, 2015 · N616DL · Boeing 757232SDR FDEA201502070469None · noneEXISTING REPAIR WING, LT SIDE THERE IS A REPAIR AT LT INBD MAIN FLAP LE SKIN, MF STATION 267 - 300. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A3 PT 1 ATTACHMENT B, NO HISTORY.Feb 7, 2015 · N773FD · Boeing 757222SDR FDEA201502070516None · noneEXISTING REPAIR, FUSELAGE EXTERIOR SKIN. THERE IS A REPAIR AT STATION 1462 - 1480, STRINGER 29L - 29R. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A2 PT 1 ATTACHMENT B, NO HISTORY.Feb 7, 2015 · N773FD · Boeing 757222SDR FDEA201502070518None · noneEXISTING REPAIR DOOR. THERE IS A REPAIR AT AFT CARGO DOOR, 16 INCHES FROM FWD & 14 INCHES FROM LOWER EDGE, STATION 1391 - 1400, STRINGER 24R - 26R. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-70A2 PT1 ATTACHMENT B, HISTORY 23.Feb 7, 2015 · N773FD · Boeing 757222SDR FDEA201502050453Bottle · handler errorRAMP BLEW SLIDE BOTTLE.Feb 5, 2015 · N320FE · Doug MD1030FSDR SWIA201540638None · noneTHE ACFT WAS BEING TOWED WHEN IT WENT OVER AN AREA OF ICE AND JACK-KNIFED. THE TUG STRUCK THE FUSELAGE CAUSING DAMAGE. GROUND TRANSFER, FO: 01/27/2015 CLOSED. FOUND PUNCTURE DAMAGE TO THE FWD FUSELAGE SKIN ON RT SIDE OF THE ACFT AT FS 379-FS 437 AND STR 16-Jan 27, 2015 · N784SK · Cndair CL6002C10SDR FDEA201412184146None · noneEXISTING REPAIR, FUSELAGE EXTERIOR SKIN, THERE IS A LIGHTNING STRIKE REPAIR AT STATION 349, STRINGER 22R. EXISTING LIGHTNING STRIKE REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PT 1.Dec 18, 2014 · N773FD · Boeing 757222SDR SWIA201440482Panel · erodedPANEL 344CB HAS ERODED L/E. REPAIRED L/E PANEL 344CB IAW REO.Dec 16, 2014 · N944SW · Cndair CL6002B19SDR SWIA201440479Panel · out of tolerance326AL FAILS VISOR PANEL GAP CHECK. COMPLIED WITH REO. GAPS CHECKED GOOD IAW AMM.Dec 15, 2014 · N944SW · Cndair CL6002B19SDR CA141218023Clamp · deteriorated(CAN) PREMATURE FAILURE OF CUSHION CLAMPS M85052, CLAMP MATERIAL DETERIORATES, WHICH CAN RESULT IN CHAFING & DAMAGE TO HYDRAULIC LINES, ULTIMATELY LEADING TO FAILURE OF THE HYDRAULIC SYSTEM. CUSHION OF CLAMPS ARE DARK BLUE & PURPLE. BLUE CUSHION ON THESE CLADec 11, 2014 · Cndair CL604SDR CA141218022Clamp · deteriorated(CAN) PREMATURE FAILURE OF CUSHION CLAMPS M8505. CLAMP MATERIAL DETERIORATES, WHICH CAN RESULT IN CHAFING & DAMAGE TO HYD LINES, ULTIMATELY LEADING TO FAILURE OF THE HYDRAULIC SYSTEM. APPROXIMATELY 300 CLAMPS USED PER AIRCRAFT ON CL-300/-350 ONLY. CUSHION OFDec 11, 2014 · Bombdr BD1001A10SDR CA141203001Bearing · damaged(CAN) DURING THE C-CHECK OF THE WATER SYSTEM COMPONENTS, THE TECHNICIAN FOUND A BEARING ON WHICH A COMPLETE SET OF ROLLERS WERE MISSING. AFTER INVESTIGATION, WE FOUND THAT THE BEARING HAS BEEN MANUFACTURED WITHOUT THE ROLLERS. NO LOOSE PARTS WERE FOUND AROUND Dec 3, 2014 · Cndair CL2156B11215SDR SWIA201440419Panel · failedVISOR PANEL 326BR FAILED GAP CHECK. REPAIRED IAW REO.Nov 25, 2014 · N907SW · Cndair CL6002B19SDR SWIA201440418Panel · failedVISOR PANEL 326AR FAILED GAP CHECK. REPAIRED IAW REO.Nov 25, 2014 · N907SW · Cndair CL6002B19SDR SWIA201440417Panel · out of toleranceVISOR PANEL 326AL FAILED GAP CHECK. RECONTOURED VISOR PANEL 326AL, REF REO.Nov 25, 2014 · N907SW · Cndair CL6002B19SDR SWIA201440311Panel · failedPANEL 221ELW HAS MULTIPLE ELONGATED HOLES. C-CHECK, REPAIRED ELONGATED HOLES IN PANEL NR 221 ELW, REPAIRED IAW EA.Nov 23, 2014 · N748SK · Cndair CL6002C10SDR SWIA201440310Panel · failedPANEL 221CLC HAS OBLONGED HOLE. C-CHECK, REPAIRED OBLONG HOLE ON PANEL 221CLC IAW EA.Nov 22, 2014 · N748SK · Cndair CL6002C10SDR GQRR2014FA0000707Blanket · missingHEAT BLANKET MISSING.Nov 13, 2014 · Bolkms BK117C2SDR SWIA201440179Panel · chafedPANEL 584AT CHAFED. C-CHECK, BLENDED THE PANEL TO A SMOOTH CONTOUR. REPAIR WITHIN LIMITS IAW EA.Nov 9, 2014 · N916SW · Cndair CL6002B19SDR SWIA201440064Structure · corrodedCORROSION AROUND NUTPLATE HOLE UNDER PANEL 141BL. C-CHECK, REPAIRED IAW REO.Nov 8, 2014 · N821AS · Cndair CL6002B19SDR SWIA201440044Panel · crackedPANEL 221CLC HAS CRACKS AROUND SCREW HOLE. REPAIRED CRACKS AROUND SCREW HOLE ON PANEL IAW EA.Nov 7, 2014 · N984CA · Cndair CL6002B19SDR SWIA201439991Panel · crackedPANEL 321 CT CRACKED. C-CHECK, REPAIRED CRACK IN PANEL 321CT IAW EA.Nov 4, 2014 · N611SK · Cndair CL6002C10SDR SWIA201440093Panel · delaminatedPANEL 333AL IS DELAMINATED. REPAIRED DELAMINATION IN PANEL IAW EA.Nov 3, 2014 · N707SK · Cndair CL6002C10SDR ASOA2014111211634Pin · corrodedLT AND RT LATCH IN INTERCOSTALS ARE CORRODED BETWEEN FS 349 AND FS 364. REMOVED LT AND RT LATCH PIN INTERCOSTALS IAW SRM 51-42-06 AND 51-42-21. INSTALLED LT LATCH PIN INTERCOSTAL 601R31049-9 AND RT LATCH PIN INTERCOSTAL 601R31049-10 IAW SRM 51-42-06, 51-42-2Oct 25, 2014 · N907EV · Cndair CL6002B19SDR SWIA201439851Panel · failedRIGHT LOWER VISOR PANEL 326BR FAILED GAP CHECK. CONTOURED BY HAND THE AFFECTED VISOR PANEL 326BR. PART IS NOT BUCKLED OR CREASED IAW REO.Oct 17, 2014 · N866AS · Cndair CL6002B19SDR WRNA201410160024Unknown · unknownTHE CREW REPORTED THAT DURING TAKEOFF ROLL AT APPROXIMATELY 90KTS, THE MASTER WARNING LIGHT ILLUMINATED MOMENTARILY. AND THE AUTO BRAKES REACTED UNEVEN PULLING THE ACFT TO THE LT WITH A JERKING MOTION. CORRECTED THE SITUATION WITH MOVEMENT OF THE RUDDER AND Oct 13, 2014 · N953AR · Doug MD11FSDR SWIA201439598Unknown · damagedPANEL 321CT COMPOSITE TORN. C-CHECK, REPAIRED PANEL 321 CT USING 7781 GLASS CLOTH P/O T28377 WITH EA9396, P/O T25520.Sep 29, 2014 · N609SK · Cndair CL6002C10SDR SWIA201439552Panel · chafedPANEL 699CB CHAFED. C-CHECK, BLENDED CHAFED AREA ON PANEL 699CB IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439551Panel · chafedPANEL 699BB CHAFED. C-CHECK, BLENDED CHAFED AREA ON PANEL 699BB IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439550Panel · chafedPANEL 699AB, CHAFED. C-CHECK, BLENDED CHAFED AREA ON PANEL 699AB IAW REO.Sep 27, 2014 · N864AS · Cndair CL6002B19SDR SWIA201439461Frame · bentPANEL 172BR GROUND AIR CONDITIONING FRAME IS SLIGHTLY BENT. C-CHECK, REPAIRED GROUND AIR DOOR LANDING PLATE IAW EA.Sep 22, 2014 · N468CA · Cndair CL6002B19SDR SWIA201439283Warning Message · illuminatedFLIGHT RETURNED TO FIELD DUE TO AN UNCOMMANDED SPEED LOSS. INTERROGATED MDC AND FOUND FAULTS LOGGED AT THIS TIME.Sep 12, 2014 · N912EV · Cndair CL6002B19SDR CA140818018Actuator · failed(CAN) AFT CAP OF SCOOP ACTUATOR FAILED DURING FUNCTION TEST BY PILOT ON GROUND RT SCOOP.Aug 8, 2014 · Airtrc AT802A
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