N928FD
Service difficulty reports · 102
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 = 'N928FD' 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 = 'N928FD' 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 FDEA201103281204Seat Track · damagedSTA 1438 BL 0 SEAT TRACK SPLICE REPAIR WAS ACCOMPLISHED DURING PTF CONVERSION ON MAE EA 757-5365-16-F3127, 8110-3 DATED JAN 30, 2011. THIS N/R GENERATED FOR TIME TRACKING AT STA 1420-1440, BL0 A REPAIR WAS ACCOMPLISHED ON STAM W/C 118350557EZ2R07 AND STAM EASDR FDEA201103231147Skin · crackedL4 DOOR HAS CRACKED SKIN 2 PLACES ON INSIDE OF DOOR. FWD SIDE WL 251, STA 1652. BLENDED OUT DAMAGE ON L4 DOOR FWD SIDE WL 251 STA 1652 IAW SRM 51-10-02. BLEND OUT OF 1ST CRACK. .200X1.5 BLEND OUT OF 2ND CRACK .400X2.5. FOUND TO BE OUT OF LIMITS IAW SRMSDR FDEA201103221127Pressure Panel · misaligned2 EA EXISTING CUT OUTS IN AFT PRESSURE WEB AT STA 1710-1720, RBL 15 AND RBL 35 WILL INTERFER WITH INSTALLATION OF MOD REPAIR OF PRESSURE WEB AT STA 1710-1720 RBL 15 AND 35 WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE NR 45256110SDR FDEA201103181078Skin · corrodedCORRSION ON BOTTOM OF FUSELAGE STA 640, BETWEEN S-28L TO S-30L.SDR FDEA201103181073Frame · gougedAFT CARGO DOOR CUTOUT STA 1380 S-25R TO S27R, FRAME INBD CHORD GOUGED AND BARE METAL AFT CARGO DOOR CUTOUT, STA 1380 S-25R TO S-27R REPAIR COMPLIED WITH EA F-5310-146264. REF FAA FORM 8100-9 DATED MARCH 14, 2011. CLASSIFIED MAJOR REPAIR.SDR FDEA201103150976Skin · dentedEXTERNAL FUSELAGE SKIN STA 1500-1520 BETWEEN S-22R TO S-23R HAS DENT. REPAIRED DENT ON FUSELAGE SKIN STA 1500-1520 BETWEEN S-22R TO S23R IAW SRM 53-00- 01 REPAIR 16 FIG 201. REPAIR INSPECTION REQUIRED IAW SRM 53-00-01 DETAIL II FIG 201 TABLE V. INITIAL INSPSDR FDEA201103070899Skin · misrepairedREPAIR BS 798 BETWEEN STR 15L-16L, INCORRECT SRM USED FOR INSTALLATION, REPAIRED IAW SRM 53-00-01, REPAIR 16 FIG 201 SHEET 1 THROUGH 6, CATEGORY "B" REPAIR RECURRENT INSPECTION IAW 53-00-01 FIG 201, TABLE V. MAJOR REPAIR.SDR FDEA201103070898Skin · failedREWORK OF SRM N00045 REPAIR ASSESSMENT EXT FUSE SKIN REPAIR BS 765 BETWEEN STR 16L-17L C/W ATTACHMENT "B' OF E.O 7-5001-7-5001 PT 1 INCORRECT SRM USED FOR INSTALLATION COMPLIED WITH FED EX EA F-5330-146395. REF FAA FORM 8110-3 DATED MARCH 12,2011. CLASSIFIESDR FDEA201103020824Frame · crackedAFT CARGO TA 1280 26R-25R FRAME HAS A CRACK. COMPLIED WITH E.A. F-5310-146259,8100-9 DATED MARCH 11, 2011- FIRST STAGE APPROVAL DTA 24 MONTHS. MAJOR REPAIRSDR FDEA201102250764Seat Track · damagedWHILE DRILLING P/N 11864182-21 AND -20 BL 0 AT STA 1438.0 SEAT TRACK SPLICES WERE MISDRILLED P/N 146N5178-1 AND 146N5185-U1. REPAIR ACCOMPLISHED IAW EA 757-5365-16-F3127 AND 8110-3 DATED JAN 30, 2011IN STMAE MOD CARD 118350557EZR07 REFERENCE EA F-5310-146387 SDR FDEA201102230700Frame · damagedMAIN CARGO DECK FRAME AT STA 1460 BETWEEN STR 2L TO 3L SEVERAL EXISTING TV MONITOR MOUNT AT HOLES DO NOT HAVE PROPER ED. REMOVED FRAME DAMAGE, FABRICATED NEW PARTS AND INSTALLED IAW SRM 53-00-07, FIG. 201. REPAIR NR 3 CAT "B" REPAIR WITH SUPPLEMENTAL INSSDR FDEA201102110546Skin · misrepairedREWORK OF SNRM N00090, REPAIR INSTALLED IAW INCORRECT SRM REPAIR REQUIRES REPLACEMENT. RT FUSELAGE EXT SKIN DENT AT STA 310 AND STR S23R. REMOVED EXT REPAIR AT STA 310 AND S23R IAW SRM 51-40-02, ACOMPLISHED REPAIR IAW SRM B757-200 SF 53-00-01. REPAIR 15,SDR FDEA201102110536Skin · misrepairedREPAIR INSTALLED IAW INCORRECT SRM. REPAIR REQUIRES REPLACEMENT. RT FUSELAGE EXTERNAL SKIN STA 520 BETWEEN S-24R TOS-25R. R & R REPAIR IAW SRM 53-00-01, REPAIR 15 B757-SF. OUTER ROW OF FASTNERS MUST BE INSPECTED EVERY 25,000 FC, CATEGORY "B" MAJOR REPAIR.SDR FDEA201102080500Stringer · gougedSTA 278-270.5 S-23R HAS A GOUGE. NO ALLOWABLE DAMAGE FOR SPECIAL FREIGHTER EXIST. R & R S-23R AT STA 278-270.5 IAW SRM 51-40-02. FABRICATED STRINGER ON MAE TRAVELER T10/863577. CAT "A" MAJOR REPAIR.SDR FDEA201102040471Frame · misrepairedREWORK OF NR N01483, REWORK REQUIRED ON FRAME, STA 1280 BETWEEN S11R AND S13R DUE TO REPAIR INSTALLED IAW INCORRECT SRM. R & R REPAIR AT STA 1280, BETWEEN S11R AND S13R IAW SRM 53-00-07, FIG 201, DETAIL 1 REPAIR 3. MAJOR REPAIR.SDR FDEA201102040470Frame · misrepairedREWORK OF NR N01479, REWORK REQUIRED ON FRAME STA 1280 AT STRINGER 11L DUE TO REPAIR INSTALLED IAW INCORRECT SRM. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR SRM 53-00-07, FIG 201, DETAIL 1, REPAIR 3.SDR FDEA201101040010Skin · gougedAFT CARGO DOOR, BELOW INTERNAL HANDLE, SKIN GOUGED. ACCOMPLISHED EA F-5230-146219, STEPS 1-8, AFT LOWER CARGO DOOR INNER SKIN GOUGED REPAIR, STA 1400, STR 25R. MAJOR REPAIR.SDR FDEA201012314787Skin · damagedLT WING NR 2 SLAT LOWER SURFACE FSS 635 WEDGE PUNCTURED REPAIRED NR2 SLAT LOWER WEDGE PUNCTURE IAW SRM 51-70-10, REPAIR 2. MAJOR REPAIR.SDR FDEA201012284759Frame · misrepairedSTA 1280, S-11L, FRAME REPAIR IS NOT IAW SRM INCOMING CONDITION. R & R FRAME IAW SRM 51-70-11, FIG 1 AND SRM 51-40-02. DTE REPAIR ASSESSMENT ON WO 00049137, N/R 00078. MAJOR REPAIRSDR FDEA201012284758Skin · dentedRT FUSELAGE EXT SKIN DENTED AT STA 1620 S-18R EVALUATED DENT AT STA 1620 S-18R A=.9 Y=.020 A/Y RATION 45. FOUND OUT OF LIMITS DUE TO PROXIMITY TO STR IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED DAMAGE IAW EA F-5330-146212. MAJOR REPAIR.SDR FDEA201012274754Frame · misrepairedFRAME REPAIR AT BS 1280 BETWEEN ST 11-13R NOT IAW SRM REQUIREMENTS. R & R FRAME IAW SRM 51-70-11 FIG 1 AND SRM 51-40-02. MAJOR REPAIRSDR FDEA201012214730Frame · damagedMAIN CARGO DECK FRAME AT STA 1360 STR S-2R, HAS EXISTING MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER ED'S. REMOVED FRAME FROM STA 1360 S6L TO S6R IAW SRM 51-40-02 RECIEVED THE REPAIR PARTS 1. PORTION OF FRAME TRAVLER T10/860856 2 CHANNEL T10/860858 2 CHANSDR FDEA201012214731Frame · damagedMAIN CARGO DECK FRAME AT STA 1360, STRINGER S-2L HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER ED'S. REMOVED FROME FROM 1360 S6L TO S6R IAW SRM 51-40-02 RECIEVED REPAIR PARTS 1 PORTION OF FRAME T10/860856 2 CHANNEL T10/960858 2 CHANNELS T10/86SDR FDEA201012214732Skin · dentedRT FUSELAGE EXT SKIN DENTED AT STA 231 BETWEEN S-23R TO S-24R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG III. REPAIRED DAMAGE AREA IAW EA F-5330-143238 DATED 12/14/10. FAA FORM 8100-9, DATED JAN 10, 2011, CATEGORY "B" MAJOR REPAIR.SDR FDEA201012154692Floor Support · corrodedCORROSION ON FLOOR MOUNT HOLES STA 1330 TO 1360, RBL62, MAIN CABIN. REMOVED CORROSION CHECK LIMITS ORIG MAT .070",L=2.0", W=0.80",D=.010" FOUND TO BE OUT OF LIMITS.REMOVED I/B CHORD, LOCATED DRILLED AND INSTALLED PART IAW SRM 51-40-02. MAJOR REPAIRSDR FDEA201012144662Crease Beam · corrodedCREASE WEG AT STA 1683, RBL 60 CORRODED ON UPPER SURFACE. CORROSION ON WEB AT STA 1683 RBL 60, BLENDED CORROSION AND CHECKED LIMITS IAW SRM 53-60-13, FIG 101,CORROSION FOUND TO BE OUT OF LIMITS. REMOVED WEB IAW SRM 51-40-02, RECEIVED NEW WEB PN 146N8723-2 ON SDR FDEA201012114635Skin · dentedRT FUSELAGE EXT SKIN DENT AT B STA 310 AND STRINGER S23R INSTALLED REPAIR DOUBLER AT STA 310, S23R DENT WAS OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. DOUBLER WAS FABBED FROM .071 2024-T3 BATCH NR 1941519. FILLER WAS .063 2024-T3, BATCH NR 1905681 SDR FDEA201012104630Floorbeam · corrodedCABIN FLOORBEAM BS 720 TOP SURFACE IS CORRODED ADJACENT TO L-2 DOOR SILL. ACCOMPLISHED STEP 1-7 OF EA -5310-143217 COMPLIANCE WITH FAA FORM 8110-3. MAJOR REPAIR.SDR FDEA201012094625Gate · chafedNR4 RT DOOR LOWER GATE SEAL SUPPORT STRUCTURE BOTH ENDS HAS CHAFED. BLENDED AREAIAW SRM 51-10-02 ,CHECKED LIMITS L=1.5,W=1,D=.060, FOUND TO BE OUT LIMITS IAW SRM 52-10-02 DETAIL V FIG 101. REMOVED DOOR GATE IAW SRM 51-40-02, RECEIVED NEW LOWER GATE P/N 146N6SDR FDEA201012074608Frame · damagedMAIN CARGO DECK FRAME AT STA 418 BETWEEN STRINGER S-1R HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER EDS. REPLACED FRAME AT STA 418 FROM RBL 2.5 TO TO LBL 2.5 IAW EA 757-5312-16-F3027. MAJOR REPAIR.SDR FDEA201012074607Frame · damagedMAIN CARGO DECK FRAME AT STA 1100, STRINGER S-2L HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE EDS. REMOVED AND INSTALLED STRINGER CLIP AT S-2L IAW SRM 51-40-02. CUT OUT FRAME FROM STR 1 TO STR 5L, IAW SRM 53-00-07, FOR SPECIAL FREIGHTER AND REPAIRESDR FDEA201012074606Frame · damagedMAIN CARGO DECK FRAME AT STA 1100, STRINGER S-2R HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER EDS. R & R STRINGER CLIP S2R IAW SRM 51-40-02. CUT OUT FRAME FROM STR 2R TO STR 5R, IAW SRM 53-00-07 FOR SPECIAL FREIGHTER AND REPAIRED IAW SRM 53-SDR FDEA201012044577Skin · dentedRT FUSELAGE EXTERNAL SKIN DENT BS 520 BETWEEN STRINGER 24R-25R. FABRICATED, INSTALLED DOUBLER & FILLER 2024-T3 BATCH 0001928869 .063 &2024-T3 .056 BATCH 0001383027 IAW SRM 53-00-01 REPAIR 2 THRESHOLD INSPECTION OF REPAIR DOULBER TO OCCUR ON OR BEFORE 37,50SDR FDEA201012014533Seat Track · corrodedSEAT TRACK CROWN AT LBL 45 STA1080-1180 HAS SEVERALAREAS OF CORROSION AND GOUGES. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. ORIGINAL MATERIAL .550 MATERIAL REMOVED .050 MATERIAL REMAINING .500 .FOSDR FDEA201012014532Seat Track · corrodedSEAT TRACK CROWN AT RBL 45, STA 1080-1180 HAS SEVERAL AREAS OF CORROSION AND GOUGES FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101, FABRICATED NEW SEAT TRACK P/N BAC 1520-792 IAW SRM 53-40-02, LOCATED AND DRILLED IAW SRM 51-40- 05,SDR FDEA201011304518Cusp Web · corrodedLT SIDE CUSP WEB BETWEEN FR 1140 &FR 1160 HAS CORROSION ON UPPER SURFACE REMOVED CORROSION IAW 51-10-02 SHEAR WEB AND WEB OUT OF LIMITS IAW SRM 53-40-13 FIG-101, DETAIL III. INSTALLED NEW SHEAR WEB AND WEB ON TRAVLERS T10/858934 AND T10/858933. REINSTALLED ASDR FDEA201011304526Seat Track · corrodedSEAT TRACK AT RBL 24 AHS CORROSION ON UPPER SURFACE AT BS 365. REMOVED CORROSION ON SEAT TRACK SUPPORT AFTER BLEND OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL XIK. ORGINAL MAT.080 AFTER REWORK .040 EXCEEDS REMOVE SEAT TRACK SUPPORT IAW SRM 51-40-02. FABRICSDR FDEA201011304523Seat Track · corrodedCORROSION ON SEAT TRACK STA 1640 RT SIDE AT END OF TRACK MAIN CABIN. REMOVED CORROSION ON SEAT TRACK STA 1640 RBL 45. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL VII. ORIG MATERIAL .070 AFTER REWORK .025. R & R SEAT TRACK IAW SRM 51-40-02. SDR FDEA201011294510Seat Track · corrodedSEAT TRACK CORRODED AT STA 440 RBL 24.75 ORIGINAL MATERIAL .070 REMOVED .060 REMAINING MATERIAL .010 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG. 101 DETAIL VII PAGE 104 REMOVED AND REPLACED SEAT TRACK IAW SRM 50- 40-02 PN BAC 1520-792 BATCH 0001904663 FROSDR FDEA201011164396Floorbeam · corrodedAT STA 1681, FLOORBEAM HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE OF FLOOR. REMOVED CORROSION IAW SRM 51-10-01 FOUND FLOOR BEAM OUT OF LIMITS ORIG. MAT 0.150 AFTER BLEND OUT THE WORST SPOT 0.091 IAW SRM 53-00-51 DETAIL VI. REMOVED AND REPLACED FLOORBEASDR FDEA201011164397Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1661, RBL 42, RT SIDE MAIN CABIN. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL II FABRICATED FLOORBEAM 1661 FROM MAT BAC1518-338 BATCH 1915536 LOCATED AND DRILLED IAW SRM 51-40-05. REMOVED AND REPLACED IAW SRM 51-49-0SDR FDEA201011164398Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1640, FROM RBL 62 TO LBL 62, MAIN CABIN. REMOVED CORROSION AT FLOORBEAM, STA 1640 FROM RBL 62 TO LBL 62, MAIN CABIN IAW SRM 53-00. ORIGINAL MATERIAL .130, AFTER REWORK .095, AMOUNT OF MATERIAL REMOVED TO BE IN OUT OF LIMITS IAW SRMSDR FDEA201011124325Crease Beam · corrodedCORROSION ON FLOOR STA 1345, LBL 62, MAIN CABIN. REMOVED CORROSION ON LT SIDE INBD CREASE BEAM CHORD STA 1292-1370 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VIII. ORIG MATERIAL .070 AFTER REWORK .045. R & R CHORD IAW SRM 51-40-02. CLSDR FDEA201011064266Cusp Web · corrodedCUSP WEB BETWEEN FR1600 AND FR1620 HAS CORROSION ON UPPER SURFACE LBL 62. REMOVED CORROSION ON WEB IAW SRM 51-10-02, CHECKED LIMITS L=4",W=3", D=.020",MAT ORIG .040 IAW SRM 53-60-13, DET VI, OUT LIMITS IAW SRM 53-60-13, PG 103, DET III, R &R WEB IAW SRM 51-4SDR FDEA201011054261Frame · gougedFRAME 1280 IS GOUGED JUST BELOW STR S-11L.SDR FDEA201011054260Seat Track · corrodedSEAT TRACK AT RBL 48 HAS CORROSION ON UPPER SURFACE AT BS 365. REMOVED CORROSION ON SEAT TRACK SUPPORT AFTER BLEND OUT OF LIMITS IAW SRM 53- 00-52 FIG 101 DETAIL VII. ORIGINAL MAT .080" AFTER REWORK .48" EXCEEDS. REMOVED SEAT TRACK SUPPORT IAW SRM 51-40-02SDR FDEA201011054259Floorbeam · corrodedBS 365, FLOORBEAM HAS CORROSION ON UPPER SURFACE FROM BL 0.0 TO RBL 65.0. AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. ORIG MAT .125. AFTER REWORK .095 AREA OF DAMAGE L(.5") X W(2"). R & R UPPER T-CHORD IAW SRM 53-00-51. REPAIR NR3 FROM LBLSDR FDEA201011054258Floorbeam · corrodedBS 345 FLOORBEAM HAS CORROSION ON UPPER SURFACE AT RBL 2.0. AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 101. AFTER REWORK .101, AREA OF DAMAGE L(2.5") X W(2"). R & R UPPER T-CHORD IAW SRM 53-00-51, REPAIR 3, FROM RBL 35 LBL 50. BS 345. CATEGORY "A" REPAIR. MAJOSDR FDEA201010284188Crease Beam · corrodedCORROSION STA 1180, LBL 62, W/L 208 CREASE BEAM. REMOVED AND REPLACED NEW CREASE BEAM IAW SRM 51-40-02 AND SRM 51-40-05, FABRICATED ON BATCH 0001879122, MAJOR REPAIR .SDR FDEA201010284190Structure · corrodedCORROSION BETWEEN STA 1040 AND STA 1020 RBL 62 W/L 208 4EA SPOTS MAIN CABIN. REMOVED CORROSION AT INNER CHORD IAW SRM 51-10-02. ORIG. MAT. .070" IAW DWG BAC1515-551 MAT. LOSS D=.030" L=4.200 W=1.00" MAX. MAT. REMOVE ALLOWABLE IS .007", FOUND OUT LIMITS IAW S
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