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 06FDEA2485Repair · unknownEXISTING REPAIR FOUND AT VERTICAL STABILIZER NR 4 BANJO FITTING LT.SDR QXEA200601759Unknown · unknownPDX FLT NR 2040, ON ENGINE START OF NR 2 ENG AND AFTER SELECTING NR 2 BLEED ON, F/A AND FLT DECK CREW NOTICED SMOKE IN CABIN AND COCKPIT. ABORTED THE START ASSUMING EXHAUST MAY HAVE ENTERED WITH TAIL WIND AND GAVE SECOND START ATTEMPT. LEFT THE NR 2 BLEED OFSDR BAQ2006F00001Bearing Race · crackedBEARING INNER RACE CRACKED. NOTED UPON DISASSEMBLY. (K)SDR 2006FA0000640Carrier Assy · crackedCARRIER PN 3500693-1 FOUND CRACKED DURING PENERANT INSPECTION OF PART. PART WAS BEING INSPECTED FOR OVERHAUL REPAIR, CRACK IS BEYOND REPAIR LIMITS.SDR DXTA200601478Unknown · unknownLOUD CLUNKING NOISE HEARD AND FELT ON COCKPIT FLOOR DURING CRUISE FLIGHT. OCCURRED ON SEVERAL OCCASIONS DURING CRUISE FLIGHT 400, NO GEAR INDICATION NOTED.SDR ASMF200607003Scuff Plate · ground damageDURING TRANSIT CHECK, AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR PROMOTING A DENT OF 3 INCHES LONG, 1 INCH WIDE AND .2500 INCH DEPTH IN THE SCUFF PLATE OF THE ACCESS BULK CARGO, SO IT WAS REPAIRED IAW SRM 51-10-01. DURING OVERNIGHT CHECK SCUFF PLATE WAS REMOVED TOSDR 06FDEA2434Unknown · unknownREPAIR DOUBLER STA 620 FWD LOWER CORNER MAIN CARGO DOOR CUT-OUT MARKED NR 73. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. COMPLIED WITH FEDEX EA 8-5330-100785, FUSELAGE, MAIN CARGO DOOR OSDR HALA0600468Structure · ground damagePER BOARDING AGENT, JET BRIDGE CONTACTED BOTTOM OF MED. LOWER FWD OF DOORS EDGE DAMAGE 1/8 DEEP BY 10" LONG. OK TO CONTINUE PER M105FILE NR 486050. XCRIBED TO DPM P14542367SDR MASA200601712Unknown · unknownASH 6022 FAT - STAB CHANNEL 1 DISCONNECT IN FLIGHT. MX PERFORMED A SELF TEST AND FOUND NO FAULTS. OPS CHECK NORMAL.SDR SIMA200617901None · noneFLIGHT CREW REPORTED SEVERE TURBULENCE ON FLIGHT FROM RST. FLIGHT LANDED AT ORD WITHOUT INCIDENT. COMPLIED WITH SEVERE TURBULENCE INSPECTION IAW AE WC 05=200-03, NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE. (M)SDR VNAA0606014None · noneCREW REPORTED A BIRD STRIKE ON RT LEADING EDGE. AREA WAS INSPECTED AND CLEANED. NO DAMAGE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA0606013Structure · undamagedCREW REPORTED A BIRD STRIKE ABOVE RT WINDSHIELD. AREA WAS INSPECTED AND CLEANED. NO DAMAGE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA0606011Structure · undamagedCREW REPORTED ON APPROACH TO CLT POSSIBLE BIRD STRIKE IN LT NOSE AREA. MAINTENANCE INSPECTED AIRCRAFT AND NO DAMAGE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE.SDR MASA200601677None · noneASH 7230 IAD - SMOKE AND SMELL OF FUMES IN CABIN. MX INVESTIGATED AND FOUND IT NOT TO BE SMOKE, BUT VAPOR CAUSED FROM CONDENSATION FROM NR 2 PACK. THE A/C SYSTEM OP'S CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.SDR 06FDEA2388Doubler · unknownREPAIR DOUBLER STA 870 LONG 28R-30R, MARKED NR 8. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED AND FOUND TO BE ACCEPTABLE IAW EA 8-5330-102789. FUSELAGE SKIN HAS EXISTINGSDR 06FDEA2374Doubler · unknownFOUND REPAIR DOUBLER LOCATED AT STA 1139 L48R -L48R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED, FABBED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL I FIG 6. MASDR 06FDEA2373Doubler · unknownREPAIR DOUBLER NR 3 A/C PACK DOOR UPPER EDGE. MARKED NR 7 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED FAA APPROVED DATA. REMOVED, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC10 SRM 52-10-00 VOL I FIG 2. MAJOR RESDR NSVA200600080Unknown · unknownT/O ROLL AUTOCOARSEN ON CWP CAME ON. TRIED TO RESET AND CAME ON AGAIN. PERFORMED AUTOCOARSEN COMPUTER TEST AND ADJUSTMENT, OPS CHECK GOOD.SDR HNAA0600054Unknown · unknownELECTRICAL SMELL IN CABIN. FOUND SIDEWALL LIGHT 8AC INOP. PERFORMED HIDDEN DAMAGE INSPECTION, NO DISCREPANCIES NOTED.SDR NSVA200600076Unknown · unknownLT ENGINE ITT REACHED 942 DEGREES FOR ABOUT 5 SECONDS. PERFORMED CAPPED AND UNCAPPED RUNS. DELTA FOUND TO BE 4.92, OPS CHECK OK.SDR 06FDEA2313Unknown · unknownLEFT WING FIXED L/E LOWER SIDE, STA XOS 545 AT SLAT TRACK NR 8 CUTOUT, FOUND AN EXTERNAL REPAIR DOUBLER (5.5 X 3.5 INCHES). REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIG 6 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER N01207 AND IAW SRM 57-10-00 FIG 6 VOSDR 06FDEA2312Unknown · unknownFOUND REPAIR DOUBLER CENTER FUSELAGE R3 DOOR JAMB AT STA 1250.750 AND STA 1256.750 BETWEEN LONGERON S26/27. REPLACED REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F177246-4 DOUBLER AND IAW SRM 53-50-00 FIG 19 DETAIL -3.SDR 06FDEA2311Unknown · unknownR1 DOOR EXISTING FLUSH REPAIR ON EXTERNAL SKIN. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 12 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELERF177260-4 DOUBLER F177260-2 FILLER AND IAW SRM 52-10-00 FIG 12A. VOL1SDR 06FDEA2310Unknown · unknownLT WING FIXED L/E LOWER SIDE, AT STA XOS 490, AT SLAT TRACK NR 7 CUT OUT, FOUND AN EXTERNAL DOUBLER (9" BY 6"). AFTER ASSESSMENT OF THE REPAIRED WAS DETERMINED THIS REPAIR COMPLIED WITH THE REQUIREMENTS OF SRW, REMOVED AND REPLACED REPAIR IAW SRM 57-10-00 FIGSDR 06FDEA2308Unknown · unknownMAIN CABIN FOUND FRAME REPAIR AT STA 1741 BETWEEN LONGERONS 9 LT AND 14 LT. REPLACED FASTENERS IAW SRM 53-30-00 FIG 05 VOL 1.SDR 06FDEA2307Skin · unknownREMOVE AND REPLACE REPAIR IAW SRM 57-10-00 FIG 68. FABBRICATED PART IAW DETAIL PART TRAVELER N01231 AND SRM 57-10-00 FIG 68. REMOVE AND REPLACE REPAIR IAW SRM 57-10-00 FIG 68. FABBRICATED PART IAW DETAIL PART TRAVELER N01231 AND SRM 57-10-00 FIG 68.SDR CA060612006Unknown · unknownON FINAL APPROACH, APPROX 300 FT AGL, PILOT HEARD LOW ROTOR HORN ACTIVATE AND ENG LOOSE PWR. A SUCCESSFUL AUTOROTATION WAS COMPLETED WITH NO FURTHER INCIDENT. AFTER LANDING, ENG WAS STILL RUNNING AND ONCE COLLECTIVE WAS LOWERED, ENG RETURNED TO FULL PWR. PILSDR XGN2006F00076Pump · inoperativeTHIS PUMP WAS INSTALLED NEW WITH ZERO TIME ON IT. IT HAS A 2000 TBO. IT LASTED 92.9 HRS. THE PUMP FAILED INTERNALLY. THE DRIVE GEAR WHEN TURNED BY HAND LOCKS UP INSIDE THE PUMP. (K)SDR 2006UALA01123Pin · installedSLIDE SAFETY PIN WAS PREVIOUSLY INSTALLED AND NOT REMOVED BEFORE FLT. SAFETY PIN WAS ROUTINELY INSTALLED PRIOR TO RII INSPECTION OF SLIDE RAFT FOR DOOR 1R. THE SAFETY PIN WAS NOT REMOVED AS PER UA OPERATING PROCEDURE BEFORE FLIGHT. REQUIRES FURTHER TRAININSDR 06FDEA2178Unknown · unknownPAINT STRIPED HOLE CLEANED IAW SRM 51-21-01 VOL 2 NDI PERFORMED (SEE JPF) FINDING RECORDED SEE ATTACHED SHEET, STRUCTURAL REPAIR EA NR 8-5710-96067. PERFORMED FABRICATED PART IAW DETAIL PARTS TRAVELER N I012300/N02300 AND DWG ARC0448 SRM 57-31-01 VOL 3 EA NR SDR 06FDEA2145None · noneEXISTING REPAIR FOUND ON NR 2 AIRCON BAY DOOR UPPER EXTERIOR SKIN. REMOVED AND NEW SKIN INSTALLED AS PER SRM 51-35-01 VOL II AND DRAWING ACA3822, NEW SKIN PANEL FABRICATED P/N: FX ACA3822-7 PER DRAWING ACA3822. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.SDR 06FDEA2130None · noneEXTERNAL DOUBLER ON RT FUSELAGE AFT CARGO COMPARTMENT DOOR, AFT LOWER CORNER BS 980 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED AFT CARGO DOOR IAW MM 52-35-011-4.SDR 06FDEA2081None · noneFOUND PREVIOUSLY REPAIR INSTALLED FROM STA 970-990, STR 29R WAS DETERMINED TO BE ACCOMPLISHED PER BOEING SB 727-53-0179, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENESDR 06FDEA2080None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 950D, STR 18R WAS DETERMINED TO BE ACCOMPLISHED IAW FEDEX EA 5310-57265, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKSDR 06FDEA2079None · noneFOUND PREVIOUSLY REPAIR INSTALLED BETWEEN STA 950-950C, STR 29L WAS DETERMINED TO BE ACCOMPLISHED IAW FEDEX EA 5380-55160, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GESDR 06FDEA2078None · noneFOUND PREVIOUSLY REPAIR DOUBLER/TRIPLER INSTALLED AT STA 1090 FWD LOWER SIDE OF AFT CARGO DOOR CUT OUT WAS DETERMINED TO BE ACCOMPLISHED IAW EA 7-5330-55172 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS,SDR 06FDEA2077None · noneFOUND PREVIOUSLY REPAIR LOCATED AT STA 178, FWD SIDE OF BULKHEAD, LT BOTTOM WAS DETERMINED TO BE ACCOMPLISHED PER SRM 53-10-9, FIG 3, BASED ON AN EXTERNAL EVALUATION, CONSIST OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS,SDR 06FDEA2076None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 196.5, STR 24R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG. 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS AND GENERAL WSDR 06FDEA02052Unknown · unknownSNRM N00511: RHW TOPSIDE FIXED LE BETWEEN NR 1 AND NR 2 SLAT FOUND EXISTING REPAIR. SNRM N00511: RHW TOP SIDE FIXED LE BETWEEN NR 1 AND NR 2 SLAT REPAIR IAW SRM 57-10- 00 FIG 24 VOL I. THIS REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR 06FDEA02051Unknown · unknownSNRM N00505: LHW TOPSIDE FIXED LE APPROX XORS 163.800 BETWEEN NR 1 AND NR 2 LE SLAT FOUND EXISTING REPAIR. SNRM N00505: LHW TOP SIDE FIXED LEADING EDGE APPROX. XORS 163.8 BETWEEN NR 1 AND NR 2 SLAT. REPAIR IAW SRM 57-10-00 FIG. 24 VOL.I. REPAIR CLASSIFIED MASDR 06FDEA02049Unknown · unknownSNRM N00173: EXISTING REPAIR DOUBLER FOUND AT CENTER CARGO DOOR JAMB AFT CUTOUT (ER/A273320-14) SNRM N00173: CENTER CARGO DOOR JAMB AFT CUTOUT SKIN REPAIRED IAW SRM 53-50- 00 FIG 16 VOL I. CLASIFIED MAJOR REPAIR IAW GMM 6-2-100.SDR 06FDEA2053None · noneEXT MOD DOUBLER/RPR JUST FWD OF NR 10 RPR LOCATION SHEET AT 6 O`CLOCK STA 1581. ACCOMPLISHED EA# 8-5330-95694.SDR 06FDEA2052None · noneRT WING TOPSIDE FIXED LE BETWEEN NR 1 AND NR 2 SLAT FOUND EXISTING REPAIR.SDR 06FDEA2051None · noneLT WING TOPSIDE FIXED LE APPROX XORS 163.800 BETWEEN NR 1 AND NR 2 LE SLAT FOUND EXISTING REPAIR.SDR 06FDEA2050None · noneEXISTING REPAIR DOUBLER FOUND AT AFT CARGO STA 1841 BULKHEAD WEB.SDR 06FDEA2049None · noneEXISTING REPAIR DOUBLER FOUND AT CENTER CARGO DOOR JAMB AFT CUT-OUT.SDR 06FDEA2048None · noneEXISTING REPAIR DOUBLER FOUND AT LT HORIZONTAL STABILIZER L/E SKIN AT XFS 103.2.SDR 06FDEA2047None · noneEXISTING REPAIR FOUND AT LT INBD FLAP INBD SEGMENT AT XIFH157.5. EXISTING REPAIR AT LH INBD FLAP SEGMENT AT X1FN157.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER DELTA ENGINEERING REPAIR/ AUTHORIZATION 361348- 14. E1-5100-7-5001, TITLE " REPAIR SDR 06FDEA2027None · noneRIGHT FUSELAGE STA 535 TOP AFT CORNER NR 3 PACK A/C COMPARTMENT FOUND EXISTING DOUBLER REPAIR. INSTALLED NEW ROW FASTENERS IAW SRM 51-33-01 VOL 2 AND 53-50-00 FIG 3 VOL 1.SDR 06FDEA2018None · noneRIGHT FUSELAGE STA 535 TOP AFT CORNER NR 3 PACK A/C COMPARTMENT FOUND EXISTING DOUBLER REPAIR. INSTALLED NEW FASTENERS IAW SRM 51-33-01 VOL 2 & 53-50-00 FIG 3 VOL 1.
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