N312NE, cancelled Jan 28, 2004
Service difficulty reports · 81
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N312NE' AND deregistration_id = 'N312NE-2004-01-28' 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 n_number = 'N312NE' AND deregistration_id = 'N312NE-2004-01-28' 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 EISA20010117Hydraulic System · lowAFTER TAKEOFF WITH GEAR UP AND FLAPS AT 2 DEGREES HYD SYS A QTY DROPPED TO 1.6 GALLONS. SERVICED A-SYSTEM HYDRAULICS, RAN ALL FLT CONTROLS, SYS OPS OK AND A-SYS QTY IND FALL.SDR EISA20010060Skin · delaminatedDURING ROUTINE C-CHECK INSPECTION FOUND DELAMINATION ON PANEL SKIN AT RT WING L/E AFT OF NR 5 KRUEGER FLAP. CLEANED PREPPED AREA BONDED FIBERGLASS OVERLAY, PRIMED AND PAINTED AREA IAW SRM 51-40-9, M/M 51-20-51, 51-20-151.SDR EISA20010058Strap · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON FLOOR STRAP AT BS 1130 AND LBL 24.75 UNDERSIDE. FABRICATED AND INSTALLED FLOOR STRAP, ALODINED AND PRIMED IAW SRM 51-40-2 FIG 1, 51-10-2, 51-30-2.SDR EISA20010057Floorbeam · gougedDURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT MAIN CABIN FLOORBEAM BS 950 AT RBL 7. FABRICATED AND INSTALLED ANGLES, FILLER AND FLOORBEAM T-CAP AT BS 950 RBL 45 TO LBL 45, ALODINED AND PRIMED IAW SRM 53-10-2, 51-10-2, 53-10-8 FIG 8, 51-30-2.SDR EISA20010056Skin · crackedDURING ROUTINE C-CHECK INSPECTION FOUND MAIN CABIN SKIN CRACKED AT BS 1096 STRINGER 1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1096 STR 1, ALODINED AND PRIMED, IAW SRM 53-30-3 FIG 4, 51-10-2, 51-30-2.SDR EISA20010055Web · crackedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING NR 1 SLAT II/B WEB FOR ACTUATOR ATTACH POINT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, ALODINED, AND PRIMED IAW SRM 51-40-3, 51-10-2, 51-30-2, 27-81-11, SPM 20-50-01.SDR EISA20010054Floorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION UNDER NUT PLATE ON FLOOR ANGLE AT BS 1148 12 FT LEFT OF BL 0 UNDER FLOOR SIDE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AT BS 1148 LBL 12, ALODINED AND PRIMED IAW SRM 53-10-8 FIG 8, 51-10-2, 51-10-6,SDR EISA20010053Stringer · gougedDURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT STRINGER 25L BS 400. FABRICATED AND INSTALLED REPAIR DOUBLERS AT BS 400 STR 25L, ALODINED AND PRIMED IAW SRM 53-10-1, 53-10-2, 53-10-3 FIG 2, 51-10-2, 51-30-2.SDR EISA20010052Frame · gougedDURING ROUTINE C-CHECK INSPECTION FOUND GOUGE AT MAIN CABIN FRAME BS 1166 WL 210 LBL 63. FABRICATED AND INSTALLED REPAIR WEB AND FLOOR SUPPORT DOUBLER AND FILLER, AT BS 1166 WL 210 LBL 63, ALODINED AND PRIMED IAW SRM 51-10-2, 51-40-3 FIG 1, 53-10-2.SDR EISA20010051Floorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT BS 620 WL 208 RBL 65 TO RBL 70 FLOORBEAM UPPER CHORD LOWER SECTION. FABRICATED AND INSTALLED REPAIR ANGLE AT BS 620 WL 208 RBL 65 TO RBL 70, ALODINED AND PRIMED REPAIR ANGLE IAW SRM 53-10-8 FIG 3, 51-10-2, SDR EISA20010059Floorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM AT BS 1130 CORRODED AT NUT PLATES FROM RBL 62.5 TO LBL 62.5. FABRICATED AND INSTALLED REPAIR ANGLE AND RADIUS FILLER, ALODINED AND PRIMED REPAIR PARTS IAW SRM 53-10-1 FIG 5, 51-10-6, 53-10-8 FIG 8, 51-10-2, 51SDR EISA20010066Stringer · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT FORWARD CARGO COMPARTMENT, LOWER LOBE, STRINGER 26L EITHER SIDE OF BS 540 FRAME. STOP DRILLED, FABRICATED AND INSTALLED REPAIR ANGLE, ALODINED AND PRIMED IAW SRM 51-10-1, 53-10-3, 51-10-2, 51-30-2.SDR EISA20010065Skin · puncturedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT TRAILING EDGE FLAP HAS PUNCTURE HOLE. FABRICATED REPAIR DOUBLE, SEPTUM AND CONE FILLER, BONDED REPAIRS, ALODINED, SEALED, AND PRIMED AREA IAW SRM 51-40-20 FIG 18, 57-50-2, 51-10-2, M/M 51-20-151.SDR EISA20010064Stringer · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND FORWARD CARGO COMPARTMENT, LOWER LOBE AREA STRINGER 27R BS 560 CORRODED. FABRICATED AND INSTALLED STRINGER SPLICE, ALODINED AND PRIMED IAW SRM 53-10-3 FIG 1, 51-30-2, 51-10-2, M/M 51-20-11.SDR EISA20010063Stringer · crackedDURING ROUTINE C-CHECK INSPECTION FOUND FORWARD CARGO COMPARTMENT, LOWER LOBE AREA STRINGER 25L CRACKED/CORRODED AT ATTACH POINT AT BS 580. FABRICATED AND INSTALLED REPAIR STRINGER SPLICE, ALODINED AND PRIMED STRINGER SPLICE IAW SRM 53-10-3 FIG 1, 53-10-2, 51SDR EISA20010062Skin · gougedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING INBOARD FOREFLAP INBOARD END UPPER AND LOWER SURFACES GOUGED. FABRICATED DOUBLER AND FILLER, BONDED REPAIR FILLER AND DOUBLER, ALODINED AND PRIMED REPAIRS AND PAINTED IAW SRM 51-10-2, 51-40-20 FIG 17, 57-50-2,SDR EISA20010061Frame · misdrilledDURING ROUTINE C-CHECK INSPECTION FOUND DOUBLE DRILLED HOLES AT BS 950A STRINGER 8R TO 9R. FABRICATED AND INSTALLED ANGLE REPAIR, ALODINED AND PRIMED ANGLE REPAIR IAW SRM 53-10-4 FIG 1, 51-10-2, 51-30-2.SDR EISA20010050Spar · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT RIGHT WING CENTER SECTION, REAR SPAR LOWER CHORD AND WEB. FABRICATED AND INSTALLED WEB REPAIR AND SPACERS AT RIGHT WING CENTER SECTION REAR SPAR LOWER CHORD AND WEB, ALODINED AND PRIMED IAW SRM 51-10-2, 51-SDR EISA20010049Hinge · elongatedDURING ROUTINE C-CHECK INSPECTION FOUND MAIN CARGO DOOR HINGE AREA HAS ELONGATED HOLES. REAMED HOLES FABRICATED AND INSTALLED FREEZE PLUG BUSHINGS AND RADIUS FILLER STRAP, ALODINED AND PRIMED IAW SRM 51-10-2, 51-30-2, AND FVCI DRAWING 53-01035-1.SDR EISA20010048Angle · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND Z-ANGLE CORRODED AT BS 570 TO BS 600, RBL 20. FABRICATED AND INSTALLED Z-ANGLE AND WEB REPAIR, ALODINED AND PRIMED IAW SRM 51-40-2 FIG1, 51-40-4, 53-10-2, 51-30-2, 51-10-2, AND M/M 51-20-11.SDR EISA20010047Floorbeam · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM AT BS 1060 LOWER LEG CORRODED. FABRICATED AND INSTALLED 2 REPAIR ANGLES, ALODINED AND PRIMED ANGLE REPAIRS IAW SRM 53-10-8 FIG 2, 51-10-2, 51-30-2.SDR EISA20010046Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CARGO COMPARTMENT RIGHT O/B SEAT TRACK SECTION FROM BS 580 TO BS 620. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 580 TO BS 640 RBL 45. ALODINED AND PRIMED IAW 51-10-2, 53-10-5 FIG 7, 51-10-6, 51SDR EISA20010045Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT I/B SEAT TRACK SECTION FROM BS 741 TO BS 757. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 741 TO BS 757 LBL 24. ALODINED AND PRIMED IAW SRM 51-10-2, 53-10-5 FIG 7, 51SDR EISA20010044Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN LEFT I/B SEAT TRACK SECTION FROM BS 757 TO BS 852 LBL 25. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 757 TO BS 852 LBL 25, ALODINED AND PRIMED IAW SRM 53-10-1, 53-10-5 FIG 7, 51-10-2.SDR EISA20010043Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION FROM BS 440 TO BS 480 LBL 45. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 440 TO BS 480 LBL 45, ALODINED AND PRIMED IAW SRM 53-10-1 FIG 3, 53-10SDR EISA20010042Bulkhead · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT AFT CARGO BULKHEAD BS 1060, WL 208. FABRICATED AND INSTALLED REPAIR FRAME DOUBLER, FILLER, AND REPAIR ANGLE, AT BS 1060 WL 208. ALODINED AND PRIMED IAW SRM 53-10-8 FIG 3, 51-10-2, 51-30-2.SDR EISA20010041Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION FROM BS 757 TO BS 852 LBL 45.5. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 757 TO BS 852 LBL 45.5, ALODINED AND PRIMED IAW SRM 53-10-5 FIG 2, 5SDR EISA20010040Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION ON MAIN CABIN CARGO COMPARTMENT LEFT O/B SEAT TRACK SECTION BS 720C TO 720E LBL 45. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 720C TO BS 720E LBL 45, ALODINED AN DPRIMED IAW SRM 53-10-7 FIG 7, 53-10-5, SDR EISA20020039Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT MAIN CABIN SEAT TRACK SECTION BS 920 TO BS 960 AT 0 BL. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 920 TO BS 960 0 BL, ALODINED AND PRIMED SEAT TRACK IAW SRM 51-10-5 FIG 7 AND FIG 2, 53-10-5, 51-10-6,SDR EISA20010038Seat Track · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT MAIN CABIN SEAT TRACK SECTION BS 910 TO BS 950 LBL 24.75. FABRICATED AND INSTALLED SEAT TRACK SPLICE AT BS 910 TO BS 950 LBL 24.75, ALODINED AND PRIMED SEAT TRACK SPLICE IAW SRM 53-10-5 FIG 7, 51-10-6, 51-1SDR EISA20010037Web · crackedDURING ROUTINE C-CHECK INSPECTION FOUND CRACK AT BS 1195 WL 290 FWD OF ACCESSORY COMPRT LEFT SIDE OF AFT ENTRY DOOR. FABRICATED INSTALLED WEB REPAIR DOUBLER AND CHORD REPAIR ANGLES, ALODINED AND PRIMED IAW SRM 53-10-2, 51-40-2 FIG 2, 51-10-2, M/M 51-20-11 ANDSDR EISA20010036Skin · delaminatedDURING ROUTINE C-CHECK INSP FOUND RIGHT WING NR 11 SPOILER UPPER SURFACE DELAMINATED. CLEANED AND PREPPED AREA, BONDED FIBERGLASS OVERLAYS, PRIMED AND PAINTED AREA IAW SRM 57-40-06, 51-50-6 FIG 1, AND M/M 27-61-1 AND 51-20-151.SDR EISA20010035Trim Tab · damagedDURING ROUTINE C-CHECK INSPECTION FOUND RT ELEVATOR TRIM TAB HAS HOLE WHERE SCREW WAS LOCATED. FABRICATED INSTALLED BUSHING, ALODINED AND PRIMED IAW REO-W00026, SRM 51-30-2, AND M/M 27-30-11.SDR EISA20000199Fuel Line · leakingDURING CLIMBOUT, LOST THRUST ON NR 1 ENGINE. AIR TURNBACK TO (IND). FOUND FUEL LINE LEAKING. REMOVED AND REPLACED FUEL LINE, OPS CHECK GOOD IAW M/M 73-00.SDR EISA200000051Shuttle Valve · inoperativeNR 2 SLAT FAILED TO RETRACT AFTER TAKEOFF. COMPLETED ABNORMAL CHECK.SDR EISA200000050Warning Light · illuminatedAFTER TAKEOFF FROM PDX, NR 2 LEADING EDGE FLAP AMBER LIGHTS BOTH FWD AND AFT PANEL WOULD NOT EXTINGUISH.SDR 2000050Connector · dirtyAFTER TAKEOFF FROM PDX, NR 2 LEADING EDGE FLAP AMBER LIGHTS BOTH FWD AND AFT PANEL WOULD NOT EXTINGUISH. CLEANED CONNECTOR, OPS CHECK GOOD IAW MM 27-81-00.SDR EISA2000045Shutoff Valve · failedAIRCRAFT WILL NOT PRESSURIZE ON THE RIGHT PACK ONLY IN FLIGHT. REPAIRED WIRING TO LEFT PACK VALVE. OPS CHECK GOOD IAW MM 21-00. (M)SDR EISA99217Door · missingB-SYSTEM SERVICE DOOR MISSING. PER MAINTENANCE THERE IS SHEET METAL DAMAGE, TO AIRFRAME, HINGE IS MISSING AND RIVETS PULLED. REPLACED DOOR ASSEMBLEY, DALFORT COMPLETED STRUCTURAL REPAIR PER 727 SRM 51-30-2. (M)SDR EISA99123Bulkhead Web · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 18.2 TO RBL 18.2 (31 PLACES). REMOVED DAMAGED AREAS AND INSTALLED PERMANENT REPAIR PER ENGINEERING AUTHORIZATION (EA) NR 7-5310-77-C1529 ANDSDR 99ZZZM396Bulkhead Web · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 18.2 TO RBL 18.2 (31 PLACES). REMOVED DAMAGED AREAS AND INSTALLED PERMANENT REPAIR PER ENGINEERING AUTHORIZATION (EA) NR 7-5310-77-C1529 ANDSDR EISA99119Shear Tie · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SHEAR TIE BROKEN AT FS 520 19R. REMOVED BROKEN SHEAR TIE, FABRICATED NEW PART PER SAMPLE AND INSTALLED PER SRM 51-30-2 AND 51-10-1. (M)SDR EISA99118Frame · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FUSELAGE FRAME CRACKED AT FS 1166 LEFT AT WL 232.5. REMOVED DAMAGED AREA, FABRICATED REPAIR PER SRM 51-40-4 AND INSTALLED PER 51-40-4 AND 51-30-2. (M)SDR EISA99117Stringer · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND STRINGER 27L CRACKED AT FS 1050. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2 AND 51-30-2. (M)SDR EISA99116Bulkhead Beam · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN SUPPORT BEAM ON REAR BULKHEAD AT FS 1183 RBL 27, WL 262. REMOVED DAMAGED AREA PER SRM 51-40-4. FABRICATED AND INSTALLED FILLERS AND DOUBLERS PER SRM 51-40-4, FIG 1. (M)SDR EISA99115Frame · deformedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FORWARD LOWER CORNER OF FORWARD CARGO DOOR, GOUGED AND DEFORMED AT FS 620. REMOVED DAMAGED CORNER, POSITION DRILLED NEW PART AND INSTALLED PER SRM 51-10-1 AND 51-30-2. (M)SDR EISA99113Seat Track · corrodedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 1 SEAT TRACK AT FS 620. REMOVED SECTION TO TRACK FROM FS 620 TO 66O AND REPLACED WITH NEW SECTION OF TRACK PER SRM 53-10-5. (M)SDR EISA99112Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN LOWER SKIN ON LEFT ELEVATOR. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 55-20-3. (M)SDR EISA99111Skin · corrodedDURING ACCOMPLISHMENT OF C-CHECK WORKCARD, FOUND CORROSION ON LOWER SKIN OF LEFT ELEVATOR, 42 INCH FROM OUTBOARD END. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER PER SRM 55-20-3. (M)SDR EISA99110Seat Track · corrodedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION OF SEAT TRACK AT FS 620 TO 720 LBL 24. REMOVED DAMAGE TRACK SECTION FROM FS 620 TO 720 AND REPLACED WITH NEW SECTION PER SRM 53-10-5. (M)
Back to N312NE, cancelled Jan 28, 2004