N964FD
Service difficulty reports · 184
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 = 'N964FD' AND registry_match = 'registration' 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 = 'N964FD' AND registry_match = 'registration' 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 FDEA2018100542783Deck Plate · corrodedCORROSION ON DECK PLATE STA 1682 RBL 40 - RBL 46. REMOVED CORROSION DECK PLATE STA 1682, RBL 40 - RBL 46 IAW SRM 51-10-02-OG, ORIG MAT = .071" REM MAT =.049", MAT LOSS = .022" FOUND OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAIL III. FABRICATED AND INSTALLSDR FDEA2018100542782Deck Plate · corrodedCORROSION ON DECK PLATE STA 1682 RBL 25 REMOVED CORROSION ON DECK PLATE STA 1682, RBL 25 IAW SRM 51-10-02-OG, ORIG. MAT .071", REM MAT .053", MAT LOSS .018" FOUND OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DETAIL III. FABRICATED AND INSTALLED REPAIR IAW SRM 53-SDR FDEA201810042785Deck Plate · corrodedCORROSION ON DECK PLATE STA 1682 LBL 8 - LBL 13. REMOVED CORROSION IAW SRM 51-10-02-OG, ORIG MAT = .071" REM MAT OG, ORIG MAT = .071" REM MAT =.060", MAT LOSS = .011", FOUND OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAIL III. FABRICATED AND INSTALLED REPAISDR FDEA201810042781Deck Plate · corrodedCORROSION ON DECK PLATE STA 1682 RBL 9 - RBL 16. REMOVED CORROSION IAW SRM 51-10-02-OG, ORIG MAT = .071" REM MAT =.053" & .056", MAT LOSS = .018" & .015", FOUND OUT OF LIMITS IAW SRM 53 OG, ORIG MAT = .071" REM MAT =.053" & .056", MAT LOSS = .018" & .015", FOUSDR FDEA201810042780Seat Track · corrodedCOCKPIT FWD WET AREA STA 358 LBL 7 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION ON SEAT TRACK, STA 345 TO 377, LBL 7 IAW SRM 51-10-02-OG. EVALUATED DAMAGED SEAT TRACK, ORIG MAT=.080", REM MAT=.030", MAT LOSS=.050",L=6.0"XW=1.0", FOUND OUT LIMITS IAW SRM 53-00SDR FDEA201810042779Seat Track · corrodedFWD WET AREA, BS 358 RBL 14, SEAT TRACK HAS PITTING CORROSION. REMOVED CORROSION ON SEAT TRACK, STA 345 TO 377, RBL 14 IAW SRM 51-10-02-OG. EVALUATED DAMAGED SEAT TRACK, ORIG MAT=.080",REM MAT=.020", MAT LOSS=.060",L=3 LOSS=.060",L=3.0"XW=1.0", FOUND OUT LIMISDR FDEA201809292744Door Frame · gougedFWD E&E BAY DOOR FRAME AT BS 231.25 BL0 GOUGED. BLENDED GOUGE IAW SRM 51-10-02. AFTER FURTHER EVALUATION FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIGURE 101 DETAIL II. CUT OUT AND REMOVED DAMAGED AREA IAW SRM 53-00-07-2R REPAIR 7. FABRICATED AND INSDR FDEA201801160101Collar · brokenCREW FOUND THE L1 DOOR LOCK BROKEN OFF. REMOVED AND REPLACED L1 DOOR LOCK COLLAR IAW AMM 52-11-08-8. LOCK OPS CHECKED GOOD IAW AMM 52-11-00.SDR FDEA201610143627Seal Depressor · damagedC2 DOOR EXT LWR EDGE HAS NUMEROUS AREAS OF DAMAGE. R&R C2 DOOR EXT LWR EDGE, SEAL DEPRESSOR IAW SRM 51-40-02 & DWG 146N6603 REV A. ACCOMPLISHED PRESSURIZATION CHECK IAW AMM 05-51-24-2.SDR FDEA201610143626Seal Depressor · gougedC1 DOOR AFT EDGE DAMAGED 2 PLACES. REMOVED AND REPLACED C1 DOOR LOWER SECTION DEPRESSOR IAW DWG 143N6603 REV B. PRESSURIZATION CHECK REQ PER AMM 05-51-24-2.SDR FDEA201610133607Angle · corrodedC1 DOOR CENTER ANGLE LOWER BEAM BS 588.93 HAS CORROSION. REMOVED AND REPLACED C1 DOOR CENTER ANGLE LOWER BEAM BS 588.93 IAW DWG 143N6603 REV AT AND REV E.SDR FDEA201610103529Beam · gougedMAIN CABIN STUB FRAME AT STA 600 LOWER AFT FLANGE HAS 2 OPEN EXISTING HOLES WITH SHORT PITCH AND RADIUS LOCATION AND 2 EXISTING FASTENER HOLES WITH LIGHT GOUGES IN RADIUS APPROX LBL 51. R&R MAIN CABIN STUB BEAM, FRAME STA 600 LT IAW DWG 657N4311 REV -. MAJORSDR FDEA201610053466Fitting · crackedMCD CUT OUT LOWER SILL ATTACH STUB FRAME AT STA 580 LT HAS A CRACK IN THE UPPER AFT RADIUS. REMOVED AND REPLACED MAIN CABIN STUB BEAM, FRAME STA 580 LT IAW DWG 657N4311 REV - . MAJOR REPAIR.SDR FDEA201610033444Door Frame · crackedR2 DOOR FWD FRAME UPPER HINGE CUTOUT CRACKED. REPAIRED IAW EA F-5210-TO328868 P1. MAJOR REPAIR.SDR FDEA201606162022Skin · crackedFOUND FUSELAGE SKIN BULGED AT INBD AFT CORNER OF LAV SERVICE DOOR FRAME WITH SKIN CRACKS. COMPLIED WITH EA F-5330-TO326081, PARTS 1 AND 2 THIS A MAJOR REPAIR.SDR FDEA201601120129Light · not seatedCOCKPIT EMER LIGHT INOPERATIVE. RESEATED BULB & OPERATIONS CHECKED NORMAL IAW MM 33-51-09-3. ACFT OK FOR SERVICE.SDR FDEA201510213293Mechanism · obstructedR1 DOOR FAILED TO ARM PRIOR TO DEPARTURE. FOUND DEBRIS IN FLOOR AREA WHERE GIRT BAR ARMS DOOR. REMOVED DEBRIS & CHECKED ARM & DISARM MECHANISM IAW AMM 25-66-10-2, OK FOR SERVICE AT THIS TIME.SDR FDEA201506131777Arm · obstructedR1 DOOR WILL NOT OPEN COMPLETELY. FOUND DEBRIS ON UPPER HINGE FLAPPER HINGE ARM ABOVE COCKING BELL CRANK. CLEANED, DOOR OPENS & CLOSES NORMAL INSIDE & OUTSIDE DOOR HANDLES. DOOR CHECKS NORMAL IAW AMM 52-11-01-6.SDR FDEA201506111763Hinge · dirtyR1 DOOR WILL NOT OPEN COMPLETELY. FOUND DEBRIS ON UPPER HINGE FLAPPER HINGE ARM ABOVE COCKING BELLCRANK. CLEANED, DOOR OPENS AND CLOSES NORMALLY INSIDE AND OUTSIDE DOOR HANDLES. DOOR CHECKED NORMAL. IAW AMM 52-11-01-6SDR FDEA201505161522Screw · corrodedDURING R & R OF THE RT ESCAPE SLIDE FOUND ONE OF 2 SCREWS ON THE BAR CENTERING PLATE CORRODED & UNUSABLE. INSTALLED NEW SCREW AS REQUIRED IAW AMM 20-11-00-2 TORQUE VALUE. ACFT OK FOR CONTINUED SERVICE.SDR FDEA201502210570Collar · brokenRIGHT LT CREW ENTRY DOOR HAS HOLD OPEN LOCK COLLAR BROKEN. R & R BROKEN HOLD OPEN LOCK COLLAR IAW AMM 52-11-08-8.SDR FDEA201412194153Slide · failedAIRCRAFT SLIDE FELL OUT OF DOOR WHEN OPENED BY RAMP AGENT. FOUND DOOR ARMED & DOOR EMER ASSIST BOTTLE EMPTY & BLOWN. R & R L1 DOOR SLIDE & DOOR POWER RESERVOIR.SDR FDEA201410253383Skin · dentedLOWER FUSELAGE SKIN DENTED AT BS 521 JUST BELOW STRINGER 26L. REPAIRED IAW EA F-5330-T0312662 PT 1.SDR FDEA201410253382Skin · gougedLOWER FUSELAGE SKIN HAS A GOUGE AT BS 609 BETWEEN STRINGERS 26 & 27L. REPAIRED IAW EA F-5330-T0312668 PT 1.SDR FDEA201410062973Sliding Window · damagedON POST FLIGHT INSPECTION NOTED FIRST OFFICER`S NR 2 SLIDING WINDOW HAS NUMEROUS BUBBLES IN BETWEEN PANES. R & R NR 2 OPEN ABLE WINDOW FIRST OFFICER`S IAW AMM 56-11-02-4, OK TO CONTINUE.SDR FDEA201306281411Roller · wornL1 DOOR WILL NOT CLOSE CORRECTLY. L1 DOOR APPEARS TO BE OUT OF RIG. WHEN LWR ROLLERS ENGAGE DOORFRAME TRACKS BOTH UPPER ROLLERS WILL NOT ENGAGE THE RACEWAYS IN THE TRACKS. THE UPPER ROLLERS ARE GRINDING AND GOUGING THE CASTINGS TO THE POINT WHERE THE DOOSDR FDEA201305271090Bottle · low pressureON PREFLIGHT, FOUND MAIN ENTRY DOOR SLIDE BOTTLE PRESSURE IN THE RED.SDR FDEA201301030010Sensor · out of adjustLEFT FWD ENTRY DOOR EICAS ALERT AFTER LANDING. DOOR APPEARED CLOSED TO GROUND PERSONNEL. FOUND L-1 DOOR DOOR WARNING SENSOR TO BE OUT OF ADJ IAW AMM 52-71-00-5. ADJ L-1 DOOR WARNING SENSOR IAW AMM 52-71-00-5. CYCLED L1 DOOR NUMEROUS TIMES WITH NO FAULTS SDR FDEA201212214350Bolt · looseL1 DOOR VERY DIFFICULT TO CLOSE FROM INSIDE OF ACFT. TROUBLESHOT USING FIM 52-11, FAULT TREE 807, FOUND GUIDE ARM ATTACHING BOLTS LOOSE ON DOOR SIDE. TIGHTENED BOLTS AND CHECKED ADJUSTMENT. OPS CHECKED GOOD.SDR FDEA201210303778Skin · puncturedRT ELEVATOR UPPER SKIN HAS A PUNCTURE 4 INCHES FROM T/E 21 INCHES FROM INBD END. REPAIRED IAW SRM-51-70-17-4B, FIG 24.SDR FDEA201210253747Frame · damagedFRAME HAS SHORT EDGE MARGIN CONDITION AT STA 680 , S-4L AND S-4R. COMPLIED WITH EA F-5310-162557.SDR FDEA201210243740Structure · damagedLT WING OTBD FLAP ACCESS PANEL 566AL CUT OUT HAS ELONGATED/DOUBLE DRILLED HOLES LOC NR 2 FROM INBD LOWER CORNER AT LT WING OTBD FLAP ACCESS PANEL 566AL CUTOUT A REPAIR WAS ACCOMPLISHED ON MAE NR 47749920001 AND MAE EA 757-5754-16-F3851. REV - DATED AUG 21, 20SDR FDEA201210193697Strap · corrodedAFT CARGO BS 1440-1460 S-27R OUTER CHORD INNER SURFACE HAS CORROSION. ACCOMPLISHED EA F-5310-162531,SDR FDEA201210133608Fitting · gougedRIGHT AFT BODY FAIRING FITTING AT BS 1180 IS GOUGED, WORK ACCOMPLISHED ON EAF-5340-162415 PART 1 A, B, AND C. MAJOR REPAIR.SDR FDEA201210093580Skin · damagedTWO ELONGATED HOLES IN FUSELAGE SKIN RT AFT BODY FAIRING CONTACT AREA BS 1300 BELOW S18R. ACCOMPLISHED EA F-5330-162410. MAJOR REPAIR.SDR FDEA201210083576Skin · dentedSKIN DENTED AT BS 620 AT S-20 R. COMPLIED WITH EA F-5330-159947. MAJOR REPAIR.SDR FDEA201210083577Skin · dentedDENT AT BS 1530 BETWEEN S4 - 5R, ACCOMPLISHED EA F-5330-160599. MAJOR REPAIR.SDR FDEA201210023540Spar · corrodedCORROSION FOUND AT RT AFT WING SPAR WEB SURFACE AT AFT FUEL BOOST PUMP OPENING LOWER BONDING JUMPER ATTACH POINT (MARKED) WINGS-MAIN FRAME -OUTER TANK-REAR SPAR CORRSION IRSS 183.0 RT SIDE (AFT BOOST PUMP) WORK ACCOMPLISHED ON EA F-5710-162542. MAJOR REPAIR.SDR FDEA201210023538Fastener · missingBS 1380 BETWEEN S24 AND 26R, DOOR FRAME MISSING RIVETS, RIVET DRILL IN EDGE OF FRAME UNDER INSIDE OF FRAME ACCOMPLISHED EA F-5310-160589, FUSELAGE-MAIN FRAME-SECT 46-C2 DOOR SURROUND CHORD-DAMAGED HOLES STA 1380 AT S-25R. MAJOR REPAIR.SDR FDEA201210023536Frame · damagedBS 1640, FRAME BETWEEN STRINGERS S25 AND 27R HAS DAMAGE ON TOP OF FRAME. REPAIR ACCOMPLISHED IAW EA 757-5362-16-F3886, REV. CLASSIFIED MAJOR REPAIR.SDR FDEA201209283498Skin · corrodedSKIN AT BS 750-780 S- 24L -BL 0 PERIMETER OF PANEL 191 AL MULTIPLE SCRATCHES AND CORRODED. REPAIRED IAW EA F-5330-162547. MAJOR REPAIR.SDR FDEA201209263456Skin · crackedR1 DOOR INTERNAL SKIN LIGHTNING HOLE CUT-OUT IS CRACKED JUST FWD MID AREA BEHIND TORQUE TUBE. COMPLIED WITH EA F-5210-162411. MAJOR REPAIRSDR FDEA201209043225Crease Beam · crackedOTBD CREASE BEAM AT BS 1641 CRACKED. REPAIRED IAW EA F-5310-162550. MAJOR REPAIR.SDR FDEA201208253166Skin · dentedDENT AT BS 418, BETWEEN S-15L TO S-16L, FOUND OUT OF LIMITS IAW-SRM-53-00-01, FIG 101, DET III. REPAIRED DENT IAW-SRM-53-00-01, FIG 201, R16, PG 201, MAJOR REPAIR. INSTALLED REPAIR DOUBLER IAW SRM-51-40-02.SDR FDEA201208253165Structure · corrodedAFT FUSELAGE LAV SERVICE PANEL. HOUSING (BOX) HAS CORROSION BET BS 1681- 1701. REMOVED CORRODED ON DOUBLER AND TWO CLIPS PER SRM-51-10-02, REMOVED .040 ON DOUBLER AND TWO CLIPS MAT AD 0.50 AREA ON DOUBLER IS 5" X 4" AND CLIPS 1" X 1" FOUND TO BE OUT OF LIMISDR FDEA201208233143Skin · dentedDENT IN FUSELAGE STA 400, STR 5L EVAL DENT, DENT MEASURE 7' X 3.0 X .007 DEPTH, A/Y=100 DENT IS LESS THAN 0.5 FROM STRINGER FASTENERS, OUT OF LIMITS IAW SRM-53-00-01, FIG 101, DETAIL III, REPAIR DENT STA 400, STR 5L IAW SRM-53-00-01, FIG 201 REPAIR 16. INSTASDR FDEA201208213095Skin · dentedEXTERNAL FUSELAGE SKIN STA 1400-1420 BETWEEN S-25L TO S-26L DENTED. FOUND OUT OF LIMITS IAW SRM-53-00-01, FIG 101, DET III, REPAIRED DAMAGE IAW SRM-53-00-01, FIG 201 REPAIR NR 16, PG 201-206. CATEGORY"B", MAJOR REPAIR.SDR FDEA201208173062Skin · dentedRT FUSELAGE SKIN DENTED BETWEEN BS 278 TO 288, S16-17R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIR DENT IAW SRM 53-00-01, FIG 201. REPAIR 7, CATEGORY B REPAIR.SDR FDEA201208112956Skin · bentL4 DOOR LOWER FWD L/E OF DOOR SKIN BENT. FOUND OUT OF LIMITS IAW SRM 52-10-01 FIG 101 DETAIL VI. REPAIRED L4 DOOR LWR L.E. IAW SRM 52-10-01 FIG 210 REPAIR 7 CAT "B" MAJOR REPAIRSDR FDEA201208112955Structure · bentR4 DOOR LWR FWD EDGE BENT 6" ALONG EDGE. FOUND OUT OF LIMITS IAW SRM 52-10-01 FIG 101 DETAIL VIII. REPAIRED BEND IN FWD L..E. OF R4 DOOR IAW SRM 52-10-01 FIG 201 REPAIR 7 THIS IS A MAJOR CLASS "B" REPAIR.
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