N999FD
Service difficulty reports · 109
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 = 'N999FD' 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 = 'N999FD' 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 FDEA201110124445Fire Warning · false activationMAIN CARGO FIRE EICAS ALERT ALONG WITH MASTER WARNING ALERTS ILLUMINATED AFTER TAKEOFF CLIMBING THROUGH 2,500 FT. ALERT LASTED APPROX 5 SECONDS. OVERHEAD MAIN CARGO FIRE DETECTION PANEL ILLUMINATED MID, AFT AND CARGO ISLATION LIGHTS. ALL ALERTS EXTINGUISHESDR FDEA201109224071Fire Warning · false activationON A G/A, FIRE WARNING LT, EICAS MAIN CARGO FIRE LIGHT CAME ON FOR LESS THAN 15 SECONDS, LANDED, NO SIGNS OF FIRE. PERFORMED BITE TEST IAW FIM 26-16-30-101, NO FAULTS DETECTED. ACFT OK FOR SERVICE.SDR FDEA201109224066Bracket · unsecureDOOR IR (RT SIDE) KNUCKLE RAPPER DOES NOT STOW WHEN DOOR IS DE-ARMED (INTERMITTENT). SECURED RETRACTABLE DOOR STOP BRACKET REF MM 52-11-20-5. CKS GOOD.SDR FDEA201108303576Plate · looseDOOR ARM/DISARM COVER PLATE LOOSE. REPAIRED AREA USING SRM 51-70-09.SDR FDEA201108023061Slide · low pressureON PRE-DISPATCH CHECK FOUND L-1 DOOR ESCAPE SLIDE PRESSURE TO BE APPROX 3 NEEDLE WIDTHS BELOW GREEN BAND. REMOVED AND REPLACED L1 ESCAPE SLIDE REF 25-66-01-4. AIRCRAFT OK FOR SERVICE.SDR FDEA201105271996Skin · misrepairedFLUSH REPAIR LOCATED AT BS 1400, BETWEEN S 21L AND S 22L DOES NOT MEET SRM REQUIREMENTS AND WAS REWORKED IAW E.A. F-5330-146509.SDR FDEA201105241970Crease Beam · damagedSTA 1630, CREASE BEAM INNER CHORD HAS A DOUBLE DRILLED HOLE AT NUT PLATE ATTACH HOLE AND .1875 FASTNER HOLE. INCOMING CONDITION. DUE TO DISCREPANCY EFFECTING THE PTF MOD A REPAIR WAS PERFORMED AT STA 1630, RBL 64.40 ON MAE EA 757-5361-16-F3161 AND MAE W/C SDR FDEA201105231932Skin · misrepairedFLT CREW COMP LT SIDE AT BS 263 REPAIR SEVERAL RIVITS WITH BAD BUCKTAILS, AS MARKED. REMOVED DOUBLER IAW SRM 51-40-02. COMPLIED WITH EA F-5330-146517. FUSELAGE EXISTION SKIN REPAIR REPLACEMENT AT STA 263 AND WL 220 LT SIDE. MAJOR REPAIR.SDR FDEA201105201912Skin · misrepairedREPAIR MISINSTALLED, REPLACEMENT REMOVED AND REPLACED EXISTING REPAIR AT STA 1690-1710 BETWEEN S-17L TO S-19L IAW EA F-5330-146522 . MAJOR REPAIR.SDR FDEA201105201914Stringer · gougedSTRINGER 18L AT 1688 HAS A GOUGE IN THE UPPER SURFACE. REMOVED AND REINSTALLED VENT DUCT IAW SRM 51-40-02. REMOVED DAMAGED STRINGER IAW SRM 51-40-02. FABRICATED NEW STRINGER ON MAE TRAVELER T11/882745. INSTALLED NEW STRINGER IAW SRM 51-40-02. FABRICATED NSDR FDEA201105181870Skin · chafedNR 4 L/E SLAT HAS CHAFING ALONG THE TOP OF THE SLAT FROM INBD TO OTBD SIDE. REPAIRED NR 4 SLAT IAW SRM 51-70-10, PN 114N4005-177G, SN A1-0249. REPAIR IS ON THE INBD END AND IS 24" L X 7" W. EA F-5750-146530 GENERATED FOR TRACKING PURPOSES ONLY. CLASSIFIED MSDR FDEA201104151500Channel · corrodedNR 6 SLAT INBD INNER L CHANNEL HAS CORROSION REMOVED CORROSION ON NR 6 SLAT INBD " L "CHANNEL IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101 DETAIL II. ORIGINAL MATERIAL .080 AFTER REWORK .060 SLAT. R & R ON N00817, MAJOR REPAIR.SDR FDEA201104131469Skin · misrepairedREWORK OF SNRM N00013: REWORK REQUIRED AT STA 740 S-17L TO S-18L. EXTERNAL DOUBLER/TRIPLER REPAIR DUE TO INSTALLATION IN PASSENGER CONFIGURATION REMOVED AND REPLACED EXISTING REPAIR AT STA 740 S-17 TO 18L USING EA-F 5330-1465112 REF SNRM N00013. MAJOR RESDR FDEA201104111442Skin · corrodedNR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 736. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D.028. ORIG MATERIAL .063 AFTER REWORK .035 FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5750-146287. SDR FDEA201104111441Skin · corrodedNR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 809. REMOVED CORROSION ON 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D=.025 ORIG MATERIAL .063 AFTER REWORK .038. FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5740-146287. SDR FDEA201104091415Skin · dentedEXTERNAL FUSELAGE SKIN STA 1640-1660 S-23R TO S-24R HAS DENT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 16. CATEGORY "B" MAJOR REPAIRSDR FDEA201104081409Skin · misrepairedREWORK OF SNRM N00031, REPAIR EVALUATED IAW INCORRECT SRM REPAIR REQUIRES REPLACEMENT PREVIOUSLY INSTALLED EXTERNAL SKIN REPAIR BETWEEN STA 740 TO 760 STRINGERS 6L TO 7L. REWORK ACCOMPLISHED ON EA F-5330-146284. MAJOR REPAIR.SDR FDEA201104051318Skin · dentedFWD CARGO DOOR SKIN AFT UPPER CORNER HAS A DENT. EVALUATED DENT A=.5 Y=.030 A/Y RATIO 16.6. FOUND OUT OF LIMIT IAW SRM 52-30-01 FIG 101 DETAIL VI. CUT OUT DAMAGE IAW SRM 52-30-01 FIG 201 REPAIR 4. FABRICATED REPAIR DOUBLER .071 2024 T3 IAW SRM 52-30-01. LSDR FDEA201103241158Skin · dentedFUSELAGE SKIN DENT STA. 377. 3" ABOVE STR. 14-R . EVALUATED 2EA DENTS AT STA 377 S-14R. DENT NR 1 A=1.0 Y=.020 A/Y RATIO 50. DENT NR 2 A=1.25 Y=.025 A/Y RATIO 50. DENTS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO SHEAR TIE IAW SRM 53-00-01 FIG 101 DETAILSDR FDEA201103241157Strap · corrodedAFT APU STRAP STA 1825 BETWEEN S-3R TO S-6R HAS CORROSION REMOVED CORROSION AT AFT APU STRAP STA. 1825 BLENDED AREA L=14" W= 1.0" D=.054 ORIG. MATERIAL .100 AND MAT. REMAINING .046 FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG.101 DET. 4 PAGE 104 REMOVED AND SDR FDEA201103241156Skin · misrepairedREMOVED EXISTING REPAIR BS 324-340 STR. 22L TO 23L IAW SRM 51-40-02 AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG.201 REPAIR 15 THIS IS A CLASS "B" REPAIR WITH INSPECTION THRESHOLD OF 29,000 F/C AND REPEAT INSPECTION EVERY 6,000 F/C MAJOR REPAIR.SDR FDEA201103231144Crease Beam · corrodedCREASE BEAM WEB AT STA 930 RT SIDE HAS AREA OF CORROSION REMOVED CORROSION ON RT SIDE CREASE BEAM WEB IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13 FIG 101, DETAIL III. ORGINAL MATERIAL .056 AFTER REWORK .047. L=3" X W=3" X D=.009. R & R WEB ISDR FDEA201103181075Strap · corrodedMAIN CABIN STA 1640, STRAP AT S-12R HAS AREA OF CORROSION ACCOMPLISHED EA F-5310-146269. CLASSIFIED AS MAJOR REPAIR.SDR FDEA201103150977Skin · misrepairedREWORK OF SNRM N00016 PREVIOUSLY INSTALLED EXTERNAL DOUBLER REPAIR AT STA 1710- 1718 BETWEEN S-14L TO S-16L REMOVED AND REPLACED REPAIR STA 1710-1718 BETWEEN S-14L TO S-16L IAW SRM 53-00-01 FIG 201 REPAIR 15. CLASSIFIED MAJOR REPAIRSDR FDEA201103150980Skin · corrodedLT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION- SPOTS. REPAIRED NR1 SLAT IAW SRM 51-70-10.SDR FDEA201103150979Skin · corrodedLT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION- SPOTS. REPAIRED NR 1 SLAT IAW SRM 51-70-10.SDR FDEA201103100932Skin · corrodedLT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION SPOTS ENTIRE LENGTH. REPAIRED NR 1 SLAT IAW SRM 51-70-10. MAJOR REPAIR .SDR FDEA201103080912Tear Strap · damagedSTA 365, RBL-70 AFT SCUFFPLATE DOME NUT WAS REMOVED AND DAMAGE. THE TEAR STRAP UNDER DOME NUT BY DRILLING APPROX .100 IN TO THE STRAP THE HOLE IS A NR 0.40. COMPLIED WITH EA F-5310-146528 ON MAE N/R 45633750001.SDR FDEA201103040849Retainer · corrodedHORZ STAB BOX AREA AT BS 1787 APU DOOR CUT OUT FWD RETAINER WITH CORROSION. REMOVED CORROSIONS AT HORZ STA BOX AREA AT B.S. 1787 APU DOOR CUT OUT FWD RETAINER IAW SRM 51-10-02. BLENDED AREA L=24" W=1.075" D=.060" ORIGINAL MAT .100",REMAINING =.040 FOUND OUTSDR FDEA201103040848Support Angle · corrodedAPU INLET DOOR ATTACH STRUCTURE 1787-1825 S-3R HAS CORROSION. REMOVED CORROSION AT APU INLET DOOR ATTACH STRUCTURE 1787-1825 S-3R,IAW SRM 51-10-02. BLENDED AREA L=3" W=1"D=.063" ORIGINAL MAT .063" REMAINING =0. NO SRM FOR ALLOWABLE DAMAGE. R & R ANGLE SUPSDR FDEA201103040847Support Angle · corrodedAPU INLET DOOR ATTACH STRUCTURE 1787-1825 S-6R HAS CORROSION. REMOVED CORROSION AT APU INLET DOOR ATTACH STRUCTURE 1787-1825, BLENDED AREA L=2.025" W=1.075" D=.063" ORIG MAT =.063 REMAINING =0, FOUND OUT OF LIMITS IAW NO SRM FOR ALLOWABLE DAMAGE. R & R ANGSDR FDEA201103020815Web · corrodedMAIN CABIN FLOOR STR. STA .1102 RBL 65 FLOOR WEB HAS AREA OF CORROSION. REMOVED CORROSION MAIN CABIN FLOOR STA 1102 RBL 65 IAW SRM 51-10-02 BLENDED AREA L=2.35" W= 1.10" D= .010 MAT ORIGINAL .063 MAT REMAINING .053 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13SDR FDEA201102240733Skin · misrepairedFLUSH REPAIR LOCATED AT BS 1360 BETWEEN S 21L AND 22L DOES NOT MEET SRM REQUIRMENTS. REMOVED REPAIR IAW SRM 51-40-02. COMPLIED IAW EA F-5330-146277, MAJOR REPAIR.SDR FDEA201102210644Skin · corrodedCORROSION ON FUSELAGE SKIN UNDER THE LT DME ANTENNA.SDR FDEA201102210643Skin · corrodedCORROSION ON FUSELAGE SKIN UNDER THE ATC ANTENNA.SDR FDEA201102110544Skin · damagedRT WING NR10 SLAT, OTBD TO INBD SPOT DELAMINATED FROM INWARD SKIN OUTWARD AND REST OF SKIN HAS NUMEROUS AREAS OF HAIL DAMAGE. REPAIRED NR 10 SLAT DELAMINATION IAW SRM 51-70-10, HAIL DAMAGE REPAIRED IAW SRM 51-70-01. DAMAGE IS LOCATED APPROX 12" FROM O/B EDGESDR FDEA201102110541Skin · corrodedNR 5 SLAT LOWER SKIN T/E INTERNAL L-CHANNEL SEVERAL AREAS THE ENTIRE LENGTH HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.0",W=2.0',D=.015. ORIGINAL MAT .080 MATERIAL REMAINING .065. FOUND OUT OF LIMITS IAW SRM 57-43-02 FIG 101 DET II.SDR FDEA201102110537Floor Panel · corrodedFLOOR PANEL BETWEEN STA 1681 TO 1720 HAS VARIOUS AREAS OF CORROSION ON SKIN FROM RBL 62 - LBL 62. REMOVED CORROSION AT FLOOR PANEL BETWEEN STA 1681-1720 RBL 62-LBL62 IAW SRM 51-10-02. BLENDED 3EA AREAS OUT OF LIMITS IAW SRM 53-60-51, FIG 201, REPAIR 2. ORISDR FDEA201102090515Skin · crackedNR 10 SLAT LOWER INBD SKIN CRACKED AROUND FASTENERS. ACCOMPLISHED EA F-5750-146379. WING -NR10 L/E SLAT NOSE SKIN CRACKS. MAJOR REPAIR.SDR FDEA201102040469Floorbeam · corrodedAFTER REMOVAL OF FLOOR CLIPS, FOUND CORRISION ON BOTTOM FWD SIDE OF FLOORBEAM STA 1681.8, RBL 5 AND LBL 12, WL 208.SDR FDEA201102010444Floorbeam · corrodedMAIN CABIN STA 324, RBL 29 TO RBL 60, WL 208 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF BLENDED AREA L= 3.0" W=2.0" D=.016 STA 324 RBL 28-31 ,L=3.0" W=2.0" D=.020, STA 324 RBL 41-44 ORIG MAT. .125" REMAINING MAT, .109 ATSDR FDEA201101290408Floorbeam · corrodedCORROSION ON FLOORBEAM REPAIR STA.1640 RBL19 AND RBL20 WL208 MAIN CABIN. REMOVED AND REPLACED FLOORBEAM BS 1640 LBL 63 TO RBL 63 IAW SRM 51-40-02 MAJOR REPAIR.SDR FDEA201101280400Frame · crackedMAIN CABIN FRAME AT STA 1520 BETWEEN S-2L TO S-2R HAS MOUNT HOLES OUT OF ROUND. FRAME CRACKED IAW SRM 53-00-07 FIG 101 STEP A ALLOWABLE DAMAGE 2. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 REPAIR NR 3. MAJOR REPAIR.SDR FDEA201101280399Frame · damagedMAIN CABIN FRAME AT STA 1600 BETWEEN S-2L TO S-2R HAS ELONGATED MOUNT HOLES. AFTER EVALUATION FOUND RIVETS HOLES CRACKED AT STA 1600 BETWEEN S-2L TO S-2R IAW SRM 53-00-07, FIG 101. ALLOWABLE DAMAGE 2 SF. REPAIRED SECTION FRAME IAW SRM 53-00-07, FIG 201, REPASDR FDEA201101270391Seat Track · chafedSEAT TRACK HAS CHAFE MARKS INSIDE CROWN SURFACE FROM BS680 TO 780, LBL45. REMOVED CAHFFED MARKS NSIDE CROWN AT SEAT TRACK BS 680-780 LBL-45 SRM 51-10-02 ORIGINAL MAT.230 AFTER REWORK .200 AMOUNT OF MAT REMOVED FOUND TO BE OUT OF LIMITS SRM 53-00-52 FIG 10SDR FDEA201101250346Crease Beam · corrodedINBD CREASE BEAM CORRODED AT BS 755, RBL 62. REMOVED CORROSION AT I/B CREASE BEAM IAW SRM 51-10-02 ORIG. MAT. .071 AFTER REWORK .061 FOUND OUT OF LIMITS IAW SRM 53-30-13 FIG. 101 DET. VIII FABRICATED NEW PER SRM 51-30-01 AND DWG 143N5529 WITH MAT. BAC1515-SDR FDEA201101240342Floorbeam · corrodedMAIN CABIN, STA 365, RBL 2- 60, WL 208, FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .125 MATERIAL REMOVED .017. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL VI. FABRICATED T- CHORD MATERIAL BAC1505-100800 70SDR FDEA201101200310Floorbeam · corrodedMAIN CABIN STA 395, RBL 11, WL 208, FLOORBEAM TOP STRAP (PLATE) HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGNAL MAT THICKNESS .125 AFTER REWORK .108 MAT LOSS .017 AREA OF DAMAGE L(1") X W(1") OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. SDR FDEA201101190291Crease Beam · corrodedLT INBD CREASEBEAM HAS CORROSION BS 660 TO 760. REMOVED CORROSION ON CREASE BEAM IAW SRM 51-10-02 ORIG. MAT. 0.080 AFTER REWORK 0.054 FOUND TO OUT OF LIMITS IAW SRM 53-30-15 FIG. 101 DET. IV. REMOVED AND REPALCED CREASE BEAM IAW SRM 51-40-02 THIS IS" A " MASDR FDEA201101190284Skin · unknownPREVIOUS BLEND OUT AT STA 1352, BETWEEN STR 29R TO 30 ON FUSELAGE SKIN.
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