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 FDEA201208102935Skin · corrodedCABIN SKIN HAS CORROSION AROUND DOME NUTS BS 1500-1520 S-1L TO S-2L DUE TO INCORRECT REPAIR DOUBLER INSTALLED. REPAIRED IAW EA757-5361-16-F3887. MAJOR REPAIR.SDR FDEA201208042842Skin · crackedDOOR R1 INTERNAL SKIN LIGHTNING HOLE CUT OUT IS CRACKED AT AFT LOWER AREA. COMPLIED WITH EA F-5210-162548. MAJOR REPAIR.SDR FDEA201208032832Web · corrodedON REMOVAL OF WEB SECTION FROM BS 940-960, FOUND CORRODED ON BOTH ENDS AND PREVIOUSLY REWORKED. REMOVED CORROSION IAW SRM 53-40-13 FIG 101, FOUND OUT OF LIMITS IAW SRM 53-40-13 FIG 101 DETAIL III SECTION A-A. REMOVED WEB IAW SRM 51-40-02. LOCATED, DRILLSDR FDEA201208032834Frame · damagedBS 1661 FRAME S-18R HAS AN ELONGATED FASTENER HOLE COMMON TO THE FRAME FAIL SAFE CHORD AND STRINGER CLIP. COMPLIED WITH F-5310-162418 FUSELAGE- ELONGATED HOLE IN FRAME AND FAILSAFE CHORD AT BS 1661 AND S-18R. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD A RESDR FDEA201208022818Skin · dentedDENT IN FUSELAGE BETWEEN STA 1640 TO 1660 BETWEEN S26 - 27R. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. FABRICATED REPAIR DOUBLER IAW SRM 53-00-01, FIG 201, REPAIR 7. INSTALLED REPAIR DOUBLER IN SRM 53-00-01, FIG 201, REPAIR 7 ANDSDR FDEA201207302761Bearing · crackedL4 DOOR INNER SKIN LIGHTING HOLE EDGE, AT HINGE SHAFT UPPER BEARING CRACKED. COMPLIED WITH EA F-5210-162409. MAJOR REPAIR.SDR FDEA201207272720Beam · corrodedNOSE LANDING GEAR BOX BS 345 UPPER SURFACE BEAM FWD SIDE AT FASTENER ROW HAS CORROSION, DOT 122-011 COMPLIED WITH EA F-3510-162401, REF 8100-9. FUSELAGE NLG WHEEL WELL UPPER PANEL BEAM CORROSION AT BS 345 NEAR LBL19 CAT"A" MAJOR REPAIR. MAJOR REPAIR.SDR FDEA201207262709Seat Track · damagedRT SEAT TRACK SIDE SKIN FASTENER HOLE DOUBLE DRILLED AT BS 1026, RBL 45. COMPLIED WITH EA F-5310-160598. WORK ACCOMPLISHED ON EA 757-5345-16-F3835, REPAIR IS A CAT "A" MAJOR REPAIR.SDR FDEA201207212634Frame · dentedBS 1320 BETWEEN S26-27L, FRAME DENTED. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG.101, REMOVED AND REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1006, CAT."A" MAJOR REPAIR.SDR FDEA201207202624Deck Plate · corrodedAFT DECK PLATE UPPER SURFACE AT BS 1681.8 TO 1720 FROM LBL 58 TO RBL 58 HAS SEVERAL AREAS WITH NICKS, SCRATCHES, AND CORRSION FOUND AFT GALLEY UPPER DECK PLATE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL II AND III. REMOVED DECK PLATE IAW SRM 51-40-02. . INSDR FDEA201207192617Skin · damagedFOUND DAMAGE ON FWD CARGO DOOR CUTOUT LOWER EXTERIOR SKIN AT FS 610 UNDER SCUFF PLATE AREA. ACCOMPLISHED EA F-5330-160592. MAJOR REPAIR.SDR FDEA201207192616Spar · corrodedCORROSION FOUND AT LT AFT WING SPAR WEB SURFACE AT AFT FUEL BOOST PUMP OPENING, LOWER BONDING JUMPER ATTACH POINT. ACCOMPLISHED ON EA F-5710-162420, STEPS 1-5. MAJOR REPAIRSDR FDEA201207192615Spar · corrodedCORROSION FOUND AT LT AFT WING SPAR WEB SUFACE AT AFT FUEL BOOST PUMP OPENING UPPER BONDING JUMPER ATTACH POINT.SDR FDEA201207182601Strap · corrodedFUSELAGE BS 1825 S3-6R INNER STRAP CORRODED. REMOVED CORROSION IAW SRM 51-40-02. CHECKED LIMITS , ORIGINAL MAT .100 MATERIAL LOSS .050, OUT OF LIMITS IAW SRM 53-80-13 ALLOWABLE DAMAGE 1, FIG 904, DETAIL IV. R & R STRAP IAW SRM 51-40-02 AND DWG 148N3138, CASDR FDEA201207112544Frame · corrodedBS 1460, STR 27R CORROSION ON FRAME REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA ORIGINAL MATERIAL .063 MATERIAL REMAINING .040 D=.023. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, ALLOWABLE DAMAGE 2. R & R FRAME STA 1460, S-25R TO S-25L IAW SRMSDR FDEA201207072513Firewall · chafedAPU FIREWALL AFT SIDE RBL 7, 7" UP FROM LOWER FUSELAGE CHAFED REMOVED DAMAGE IAW SRM 51-10-02. REMOVED CHAFE IAW SRM 53-80-08, FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08, FIG 101, DETAIL IV. REPAIRED AREA IAW SRM 53-80-08, REPAIR 2.SDR FDEA201207062505Skin · damagedLT FWD FUSELAGE SKIN BS 750- 780, S24L PERIMETER OF PANEL 191AL MULTIPLE SCRATCHES AND CORRODED.SDR FDEA201207062503Skin · dentedDENT AT STA 694, BETWEEN S-26L TO S-27L EVALUATED DENT A=1.34 Y= .047 A/Y 28.5, DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED AREA AT STA 694 BETWEEN S-26L TO S-27L IAW SRM 53-00-01, REPAIR 16. THIS REPAIR IS CATEGORY "SDR FDEA201207062499Stringer · corrodedS-17L BS 752-900 CORRODED. REMOVED CORRODED STRINGER FROM STA 752-900 LBL 64 IAW SRM 51-40-02. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51, FIG 101. FABRICATED NEW STRINGER IAW 143N5520 AND INSTALLED IAW SRM 51-40-02 DWG 143N5520 SH 4, REV E. MAJOSDR FDEA201207032464Floor Skin · gougedCOCKPIT FLOOR SKIN HAS GOUGES, BS 299, LBL5. REMOVED DAMAGE AND CHECKED LIMITS ORIGINAL MATERIAL .050 AFTER REWORK .020 L=1.5 W=1.5 D=.030 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED FLOOR SKIN IAW SRM 51-40-02. INSTALLED NEW FLOOR SKIN IAW SRM 51-40-02 ANDSDR FDEA201207032474Floor Skin · corrodedCOCKPIT FLOOR SKIN SPLICE HAS CORROSION BS 297, LBL 34.SDR FDEA201207032473Floor Skin · gougedCOCKPIT FLOOR SKIN HAS GOUGES BS 278, LBL 34.SDR FDEA201207032471Floor Skin · corrodedCOCKPIT FLOOR FWD OF F/O YOKE FLOOR SKIN HAS CORROSION.SDR FDEA201207032470Seat Track · corrodedAFTER REMOVAL OF PILOTS SEAT TRACKS FOUND NUMEROUS AREAS OF CORROSION.SDR FDEA201207032469Floor Skin · corrodedCOCKPIT FLOOR SKIN FWD OF CAPTS YOKE HAS CORROSION.SDR FDEA201207032468Floor Skin · corrodedCOCKPIT FLOOR SKIN HAS CORROSION SPOTS STA 278, LBL19-RBL19.SDR FDEA201207032467Floor Skin · corrodedCOCKPIT FLOOR SKIN HAS CORROSION SPOTS STA 288, LBL12-RBL12.SDR FDEA201207032465Floor Skin · corrodedCOCKPIT FLOOR SKIN SPLICE HAS CORROSION BS 297, LBL16.SDR FDEA201207032462Floor Skin · corrodedAFTER REMOVAL OF COPILOTS SEAT TRACKS FOUND NUMEROUS SPOTS OF CORROSION ON FLOOR SKIN. R & R NEW FLOOR SKIN IAW SRM 51-40-02 & DWG 141N5810.SDR FDEA201207032459Frame · damagedAT BS 395 RBL2 UPPER FRAME HAS DOUBLE DRILLED HOLES. REPAIRED.SDR FDEA201206292413Skin · dentedINCOMING DENT AT BS 1390, BETWEEN S-22L TO S-23L. (D-48) EVALUATED DENT-A=1.30, Y=.030, A/Y=43.33. DENT IS LESS THAN 0.50" FROM FRAME FASTENER, AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED AREA AT STA 1390 BETWEEN S-22L TO SSDR FDEA201206282393Floor Skin · corrodedFLIGHT DECK FLOOR STRUCTURE PLATE BS 247-278, LBL 20-27 HAS CORROSION. REMOVED CORROSION IAW SRM-51-10-02, CHECKED LIMITS ORIG. MAT. .050 AFTER REWORK .042 L=15" W=25" D=.008". FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLIGHT DECK FLOOR STRUCTURE PLSDR FDEA201206282392Plate · corrodedFLIGHT DECK FLOOR STRUCTURE PLATE STA 247-278, RBL 20-27 HAS CORROSION. REMOVED CORROSION IAW SRM-51-10-02 CHECKED LIMITS ORIG. MAT. .050 AFTER REWORK .043 L=16" W=4" D=.007 FOUND TO BE OUT OF LIMITS NO ALLOWABLE LIMITS. REMOVED AND REPLACED FLIGHT DECK SDR FDEA201206282396Skin · failedSKIN AT BS 420-430 BETWEEN S-21R- S-23R MISREPAIRED. REPAIRED IAW-SRM-53-00-01 REPAIR 15, FIG 201, REPAIR IS A CAT "B" MAJOR REPAIR.SDR FDEA201206282391Plate · corrodedFLIGHT DECK FLOOR STRUCTURE PLATE AFT SIDE OF YOKE HAS CORROSION ON F/O'S SIDE.SDR FDEA201206282390Plate · corrodedFLIGHT DECK FLOOR STRUCTURE PLATE AFT SIDE OF YOKE HAS CORROSION ON CAPT SIDE.SDR FDEA201206272368Crease Beam · corrodedMAIN DECK CREASE BEAM HAS CORROSION AT FS 680, RT SIDE. CORROSION BLENDED AREA ON I/B CHORD IAW SRM 51-10-02 ORIGINAL MATERIAL .100 AFTER REWORK .030 MATERIAL LOSS .070. CHORD IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51 FIG 101. REMOVED CREASE BEAM SECTISDR FDEA201206252347Skin · damagedAFT CARGO DOOR CUTOUT LOWER EDGE AFT END HAS 2 EA STOP DRILLS IN SKIN AT LIP. ACCOMPLISHED EA F-5330-160572. MAJOR REPAIR.SDR FDEA201206202284Skin · dentedFUSELAGE EXTERNAL SKIN, STA 1627 S26R, DENTED. DENT FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. ACCOMPLISHED EA F-5330-159950. MAJOR REPAIR.SDR FDEA201206202283Frame Splice · corrodedBS 1560, FRAME SPLICE CORRODED BETWEEN STR 24R AND 25R. REMOVED CORROSION AT FRAME SPLICE STA 1560 AT STR. 24 & 25R IAW-SRM-51-10-02. BLENDED AREA ORIG MAT .071, MAT REMAINING .034, NO ALLOWED DAMAGE ON SRM. R & R SPLICE IAW-SRM-51-40-02, FABRICATED SPLICE SDR FDEA201206192260Web · corrodedSTRINGER 17 RT, BS 365-377, WEB LWR SURFACE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIG MAT .040 AFTER REWORK .032 TOTAL MAT LOSS .008 AREA OUT OF LIMIT IAW SRM 53-00-51, FIG 101, DETAIL III. FABRICATED NEW WEB FROM MAT 7075-T6, .040C BATCH NR 1948057SDR FDEA201206182255Frame · damagedFRAME AT STA 377 RBL 2 HAS DOUBLE DRILLED HOLES. HOLES REMOVED DAMAGED FRAME IAW-SRM-51-40-02, INSTALLED NEW FRAME IAW-SRM-51-40-02 AND DWG.141N1320, CATAGORY "A" MAJOR REPAIR.SDR FDEA201206142243Support · corrodedLEFT WING AT WS 165-204 UPPER T/E SKIN & PANEL SUPPORT CORRODED. REPAIRED IAW EA F-5710-159945 STEPS 1-12. MAJOR REPAIR.SDR FDEA201206122223Frame · dentedFRAME DENTED AT BS 1280, STR 26L AFT CARGO BAY. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028, BS 1280 BETWEEN S-25L TO S-25R. MAJOR REPAIR.SDR FDEA201206082162Skin · damagedHIDDEN DAMAGE FOUND AFTER REMOVAL OF R4 DOOR THRESHOLD. EXTERNAL FUSELAGE SKIN AT BS 1640-1681 S17-18R HAS MISDRILLED SCREW HOLES. ACCOMPLISED EA F-5330-162561. REPAIRED IAW EA 757 -5361-16 -F3836. MAJOR REPAIRSDR FDEA201206042081Stringer · corrodedFWD PIT STRINGER 22L IS CORRODED AT DOME NUT AT FS 750. CHECKED LIMITS 100 PERCENT EXFOLIATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL II. REPAIRED DAMAGED AREA IAW SRM 53-00-03, FIG 201, REPAIR 2. MAJOR REPAIR.SDR FDEA201206022058Frame · dentedBS 1240, S26L FRAME DENTED. NOT ALLOWED IAW SRM 53-00-07 FIG 101. REMOVED AND REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1003. MAJOR REPAIR.SDR FDEA201205302016Floorbeam · misinstalledTHE STA 1640, FLOORBEAM IS MISLOCATED. REMOVED MISDRILLED FLOORBEAM IAW SRM 51-40-02. INSTALLED REPLACEMENT FLOORBEAM IAW DWG 146N8711 SH2 REV R. MAJOR REPAIRSDR FDEA201205302013Skin · chafedRT INBD MAIN FLAP UPPER SKIN CHAFED. REPAIR ACCOMPLISHED IAW EA 757-5752-16-F3928, REV A, MAJOR REPAIR.SDR FDEA201205292007Angle · corrodedLT WW SIDEWALL TO KEELBEAM SUPPORT ANGLE, BELOW HYD. PRESSURE TRANSMITTER D2536 HAS CORROSION. REPAIRED IAW EA F-5310-160586 STEPS 1-10 . CAT "A" MAJOR REPAIR.
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