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 MASA200600709Repair · nonePERMANENT REPAIR TO LT SIDE 621 PRESSURE BLK WEB.SDR MALA060070Unknown · vibrationCREW REPORTED AN UNUSUAL VIBRATION IN CRUISE FLIGHT. AFTER DEBRIEFING THE CREW, THE ONSET OF THE VIBRATION WAS DURING STRAIGHT AND LEVEL FLIGHT AND AT 210KTS. THEY WERE NOT IN ICING CONDITIONS, THERE WAS NO TURBULANCE, A/P AND YAW DAMPNERS ENGAGED, CONDITION SDR MASA200600435None · noneASH 7284 ORD - CABIN WAS FILLED WITH SMOKE DURING A (HUFFER) AIRSTART. MAINTENANCE SWAPPED RAMP POWER CART AND AIRSTART CART. RAN ENGINES NO DEFECT NOTED.SDR COMA0660140Unknown · unknownFLIGHT 5250 - DURING CRUISE FLIGHT ENCOUNTERED NOTICEABLE GENTLE OSCILLATION IN AFT CABIN, DEACTIVATED AUTO-PILOT AND YAW DAMPERS OSCILLATION PERSISTED. AIRCRAFT REQUIRED EXCESSIVE TRIM FOR COORDINATED FLIGHT. PERFORMED ISOLATION CHECKS OF PCU'S, NO FLUCTUATSDR KBM2006F00075Control Unit · inoperativeUNIT INOPERATIVE, MEL AC UNTIL 2/20/06. (K)SDR 06FDEA0646Repair · unknownEXTERNAL FLUSH REPAIR APPROX 2.5 X 2.5 INCH RT LWR FUSE STA 302 STRINGER 24R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* REPAIRED PER SRM 53-30-3, 51-30-2 MAJOR REPAIR.SDR 06FDEA0620None · noneUNABLE TO PERFORM EA 1-5740-90695A PT3, WINGS LEADING EDGE SLATS, LT NR 2 SLAT TRACK WEB AND SUPPORT REPAIR DUE TO LONG LEAD TIME OF NEW WEB PN: ARB2981-5. COMPLIED WITH FEDEX EA 1-5740-90695ASDR 06FDEA0592Repair · unknownFOUND REPAIR LOCATED ON NR 2 L/E SLAT. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA (LEFT WING).SDR 06FDEA0591Repair · unknownFOUND REPAIR LOCATED AT STATION 188, FORWARD OF NOSE ACCESS DOOR REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING APPROVED DATA.SDR 06FDEA0590Repair · unknownFOUND REPAIR LOCATED AT STA 660, STR 30. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0589Repair · unknownFOUND REPAIR AT STA 259.5 STR 17L, REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0588Repair · unknownFOUND REPAIR LOCATED AT STA 188, STR 27L. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0587Repair · unknownFOUND REPAIR LOCATED ON MAIN CARGO DOOR LOWER FWD EDGE REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0524Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 2982 - FS 2294, FR38-FR40 FLUSH REPAIR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PERMANENT REPAIR PERFORMED BYSDR 06FDEA0511Repair · misinstalledN00765 EXTERIOR FUSELAGE SKIN STA 725-730 BETWEEN L44R-L45R HAS NON-SRM REPAIRS. REMOVED EXSISTING REPAIRS FS 725-760 L44R-L45R, FABR. EXTERNAL DOUBLERS AND FINGER DOUBLERS AND INSTALLED IAW DC10 SRM 53-20-00 FIG. 6 SHT 3 AND SHT 5 VOL I AND DC10SRM 51-33SDR 06FDEA0494None · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: STA 1159, STR 37-40 RT, EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED, REPAIR IS CONFORM TO SRM 53-40-00 FIG 8; PERFORMD E.A 8-5330- 94669 PART 1 INSPECTION.SDR QXEA200600384None · noneSEA FLIGHT NR 2134 PASSENGER AND FLIGHT ATTENDANT ADVISE THAT THEY SMELL ELECTRICAL BURNING ODOR NEAR ROW 4. MAINTENANCE INSPECTED PASSENGER LIGHT CONNECTIONS PSU'S FOUND NO SIGN OF BURNING OR ANY BURNING ODOR NEAR OR AROUND ROW 4. POSSIBLY COMING FROM DEICESDR USAA060163Repair · unknownFOUND LOWER L/E SURFACE PREVIOUS REPAIR. DOUBLER REPAIR IAW SRM 57-53-01, DEFECT SIZE: 4" BY 4.5".SDR C1HA200681001Unknown · unknownPERFORMED W/S ESCAPE MANUEVER AT MAF (ARRIVAL) WITH FIREWALL POWER ON ALL 3 ENGINES. NO ENGINE LIMITATIONS WERE EXCEEDED. PERFORMED INSPECTION OFF ALL ENGINES INLET AND EXHAUST PER B727 MM 72-00-00. NO DAMAGE FOUND. A/C OK FOR SERVICE.SDR A6WA200640011Unknown · unknownABORTED TAKEOFF DUE TO LOSS OF DIRECTIONAL CONTROL AT LOW SPEED (30 KNOTS) WHEN APPLIED POWER. AC WENT TO THE RT, FULL LT RUDDER HAD NO EFFECT. ENG PERAMETERS NORMAL AND NO THRUST LEVER SPLIT. CREW PERFORMED 2 HIGH SPEED TAXIS, PERFORMED POWER ASSURANCE RUNSDR CA060127004Switch · unserviceable(CAN) FLOAT SWITCH FAILED INTERNALLY CAUSING THE EPA CAN TO DRAIN OVERBOARD ON SHUTDOWN. (TC NR 20060127004)SDR IXXA06SMN061SNone · noneDURING C CHECK, 'FWD LAVATORY DRAIN HOLE PLUG INSTALLATION REQUIRED, STA 270.000 - 280.000, L-22R TO L-23R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 1 (SHEET 1, 3). REMOVED FASTENERS IAW DC8 SRM 51-3-0. CUT OUT AREA, FABRICATED REPAIR DOUBLER, (02EA) ISDR MASA200600195None · noneASH 6486 ELP - CAPTAIN REPORTED THAT THE FWD PBE VSI IS PROTRUDING. MX FOUND PBE TO BE SERVICEABLE PER THE ESSEX PB/E CORP REFERENCE AND PROCEDURES MANUAL.SDR KBM2006F00045Unknown · unknownENGINE OIL PRESSURE AND TORQUE GAUGE FLUCTUATED AND DROPPED TO ZERO, REMOVED AND REPLACED. (K)SDR 06FDEA0294Repair · noneLEFT HORIZONTAL STABILIZER DETACHABLE ELEVATOR LOWER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0293Repair · unknownDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: INSTALLED REPAIR ON LT OUTBOARD ELEVATOR LOWER SKIN AT STA XE 347.948. THE EXISTING REPAIR COMPLY SRM 55-10-00 FIG 1 FOLLOWING FEDEX EO 8-5100-7-5001 PT2.SDR 06FDEA0281Skin · scheduled maintBS 480-680 STR 4L-4R, REPLACEMENT SKIN REQUIRES REMOVAL OF TEAR STRAPS TO ACCOMMODATE STRUCTURE OF MCD CUTOUT FROM STR 3L TO LT EDGE. REPAIRED PER SRM 51-10-2 AND DWG 53FX1380.SDR AT0600010Hose · burnedAFTER APPLYING POWER ON TAKEOFF BOTH PILOTS F/AS SMELLED A BURNING RUBBER ODOR. THE ODOR REDUCED WHEN POWER REDUCED. DECIDED TO RETURN AND LAND. ODOR WAS GONE BY LANDING. FIRST IMPRESSION WAS THAT IT WAS TIRE SMOKE FROM ANOTHER A/C BUT IT PERSISTED IN THE CSDR AWXA200600420Repair · unknownMCN - DURING C19 CHECK DISCOVERED TEMP SKIN REPAIR, AT BS 937.15 TO BS 947.50 AND STR 24L, THAT WOULD BE OUT OF PERMANENT REPAIR LIMITS OF SRM 53-00-01 FIG 201 REPAIR 31. MAINTENANCE PERFORMED INSURANCE CUT IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5SDR 06FDEA0255Repair · unknownDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: STA 1248-1256 RT SIDE, EXISTING REPAIR ON JAMB DOOR STR 27-25. REPAIR MEETS SRM 53-50-00 FIG 19 CRITERIA, BUT MUST BE ADDED 2EA RIVETS IAW SRM 53-50-00 FIG 19 SH 1.SDR 06FDEA0251Repair · unknownRIGHT HORIZONTAL STABILIZER INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0250Repair · unknownRIGHT HORIZONTAL STABILIZER INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0249Repair · unknownLEFT WING INBOARD AILERON AT XIA 306 LOWER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 5 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR USAA060077Repair · unknownFOUND PREVIOUS REPAIR LWR SURFACE O/B T/E. UPDATED SDA, IAW TR 57-42-01, DEFECT SIZE: 6" BY 3".SDR USAA060071Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, OUTER DOOR SKIN. UPDATED SDA AS REQUIRED IAW SRM 52-30-01, DEFECT SIZE: 34" BY 43".SDR QXEA200600083Unknown · unknownPDX - WHILE PARKED AT THE GATE IN PDX WITH EXTERNAL POWER SELECTED ON ALL AIRCRAFT LIGHTING FLICKERED SEVERAL TIMES. THEN THE CABIN WENT DARK. AFTER BEING NOTIFIED BY THE FLIGHT ATTENDANT OF A SMOKE SMELL IN THE CABIN. EXTERNAL POWER WAS SELECTED OFF. MAINSDR 06FDEA0176Repair · unknownLT WING NR 1 SLAT AT STA XORS 97 OUTER SKIN HAS FLUSH REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 43 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0175Repair · unknownLT WING OUTBOARD FLAP LOWER SKIN AT STA XOF 467 FOUND DOUBLER REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 7 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0174Repair · unknownLT WING OUTBOARD FLAP LOWER SKIN AT STA XOF 458 TO XOF 462 FOUND DOUBLER REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0173Repair · unknownLT WING INBOARD FLAP UPPER SKIN AT STA XIFH 293 FOUND REPAIR DOUBLER. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0172Repair · unknownLT WING DROOPED L/E AT STA XORS 299 UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 57-10-00 FIG 55 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 2006FA0000064Case · leakingIVSI WAS RECEIVED FOR REPAIR OF A CASE LEAK EXCEEDING MFG TOLERANCES. (RC-60-VIL1) MFG ACCEPTABLE SEALANT FOR DASHPOT CYL ENDS AND FOR FEED-IN-FLANGE MNTG SCREW HEADS IS RED GLYPTAL. 5-MIN EXPOXY WAS APPLIED TO END CAPS AND FITTING FLANGE. 5-MIN EXPOXY HAS SDR MASA200600028None · pilot errorABORTED TAKEOFF AND RETURNED TO THE GATE BECAUSE THE SPEED CARDS FELL ON THE AURAL WARNING TEST SWITCH CAUSED IT TO GO INTO A TEST MODE. CREW HAD TO WAIT TILL THE TEST TO FINISH BEFORE ATTEMPTING ANOTHER TAKEOFF AND PROCEEDED ON. NO FURTHER DEFECTS NOTED.SDR DHL2006752522Repair · noneFOUND NR 111057; ACCOMPLISH IDENTIFICATION OF EXISTING FUSELAGE SKIN REPAIR AT BS 1155 & BETWEEN STR 29R-30R. ACCOMPLISHED IDENTIFICATION OF EXISTING FUSELAGE SKIN REPAIR AT BS 1155 & BETWEEN STR 29R-30R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 3. VSDR DHL2006752520Repair · noneFOUND NR 111055; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 437 & STR 18R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 437 & STR 18R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 3A. VERIFIEDSDR DHL2006752519Repair · noneFOUND NR 111054; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 410 & STR 24R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 410 & STR 24R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 1. VERIFIED SDR DHL2006752518Repair · noneFOUND NR 111053; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 305 & BETWEEN STR 8L - 11L (L1 DOOR UPPER HINGE CUTOUT). ACCOMPLISHED IDENTIFCATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 305 BETWEEN STR 8L - 11L (L1 DOOR UPSDR DHL2006752517Repair · noneFOUND NR 111052; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 205 & BETWEEN STR 19R-23R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 205 & BETWEEN STR 19R-23R. INSTALLATION PERFORMED IAW B727 SRM 5SDR DHL2006752516Repair · noneFOUND NR 111051; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 465 & STR 16R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 465 & STR 16R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 1. VERIFIED SDR 1488123005Insulation · meltedDESCENDING THRU 20,000FT AFT BAG SMOKE LIGHT CAME ON FOLLOWED BY AMBER FLOOR OVERHEAT. F/A REPORTED SMELL OF SMOKE AND HEAT.
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