N926FD

Service difficulty reports · 95

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 = 'N926FD' 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.

SDR FDEA201507242376Skin · gougedLEFT WING INBD FLAP, UPPER SURFACE HAS 1 EACH DEEP GOUGE AT WS 270. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.Jul 24, 2015 · N926FD · Boeing 7572S7 · Trailing Edge FlapsSDR FDEA201507232345Skin · gougedNUMBER 2 ENG AFT PYLON, INBD SIDE HAS A GOUGE. ACCOMPLISHED WORK IAW EA F-5480-T0319007 P 1.Jul 23, 2015 · N926FD · Boeing 7572S7 · Nacelle/Pylon, Plate/SkinSDR FDEA201507222317Skin · bulgedSKIN BULGE AT UPPER LOBE BS 395, BETWEEN STRINGERS 6 - 7R. REMOVED DAMAGED AREA IAW SRM 53-00-01-2R. FABRICATED DOUBLER IAW SRM 53-00-01-2R. INSTALLED THE DOUBLER IAW SRM 53-00-01-2R FIG 201 REPAIR 16.Jul 22, 2015 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201506071718Light · unsecureAFTER BLOCK IN, UNARMED, LIGHT ON EMER LIGHT PANEL FELL OUT. R & R THE UNARMED SWITCH LIGHT ASSEMBLY IAW AMM 33-13-00-2. OPERATIONS CHECKED GOOD. ACFT OK TO CONTINUE.Jun 7, 2015 · N926FD · Boeing 7572S7 · Flight Compartment LightingSDR FDEA201406131428Governor · malfunctionedTHE RT ENGINE SPOOLED UP UNCOMMANDED WITH BOTH THROTTLES AT IDLE. WHEN ON FINAL AT 2000' AGL, 170 KNOTS, WITH LT ENG IN FLIGHT IDLE, THE RT ENGINE WAS APPROXIMATELY 1.33 EPR, 74% N1 590 EGT, N2, N3 & FUEL FLOW ALL CORRESPONDING TO THE RT ENG STABILIZED AT A HJun 13, 2014 · N926FD · Boeing 7572S7 · Fuel Controlling SystemSDR FDEA201307101521Stringer · corrodedCORROSION ON STRINGER 29L BS 1440. CUT OUT DAMAGED STRINGER, FABRICATED AND INSTALLED REPAIR ON STRINGER IAW SRM 53-00-03 FIG. 201 REPAIR 2, 51-40-02, 51-40-03, AND SRM 53-00-00 PAGE 1 GENERAL.Jul 10, 2013 · N926FD · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR FDEA201212114280Bearing · failedL1 DOOR UNABLE TO BE CLOSED FROM THE OUTSIDE, THE EXTERNAL HANDLE WON`T COME OUT TO THE FULLY FLARED (BUTTERFLY) POSITION. REPLACED CAM FOLLOWER BEARINGS IN EXTERIOR HANDLES IAW MM 52-11-13-2, PROCEDURE E, THROUGH (R). TO SUPPORT FITTING NR 16. DOOR HANDec 11, 2012 · N926FD · Boeing 7572S7 · Passenger/Crew DoorsSDR FDEA201209223389Bottle · low pressureL1 DOOR ASSIST BOTTLE LOW. REPLACED L1 EMERGENCY POWER RESEVOIR IAW AMM 52-11-30-4.Sep 22, 2012 · N926FD · Boeing 7572S7 · Passenger/Crew DoorsSDR FDEA201209113294Slide · dislodgedDURING OPENING OF LT MAIN ENTRY DOORWAY, SLIDE BUNDLE FELL FROM STORAGE CONTAINER. REMOVED SLIDE. INSTALLED L1 SLIDE PACK IAW AMM 25-66-01-4.Sep 11, 2012 · N926FD · Boeing 7572S7 · Escape SlideSDR FDEA201201180242Door · missingRT ENGINE IDG SERVICING DOOR MISSING. R AND R DOOR IAW SRM 51-40-02.Jan 18, 2012 · N926FD · Boeing 7572S7 · Nacelle/Pylon, Main FrameSDR FDEA201201070041Girt Bar · out of adjustL1 DOOR WILL NOT DISARM PROPERLY. CANNOT MOVE TO DISARM WITHOUT MOVING HANDLE ALSO. HANDLE DOES NOT POSITIVELY GO INTO DISARM BAND. REMOVED ACCESS COVER FOR DOOR SLIDE. FOUND GRIT BAR NOT GOING LOW ENOUGH TO SLIDE INTO FLOOR FITTINGS MM REF 25-66-01-4; 25-Jan 7, 2012 · N926FD · Boeing 7572S7 · Emergency EquipmentSDR FDEA201109224035Seal · dirtyVERY LOUD SQUEEL (AIR NOISE) ON THE BOTTOM OF THE R2 WINDOW. NOISE STARTED ABOUT 6.0 PSID ON CLIMBOUT AND WAS VERY LOUD AND DISTRACTING. REMOVED SMALL DEBRIS FROM R2 WINDOW FRAME, CLEANED AND INSPECTED R2 WINDOW SEAL. SEAL IS IN VERY GOOD CONDITION. CHECKSep 22, 2011 · N926FD · Boeing 7572S7 · Flight Compartment WindowsSDR FDEA201109133867Skin · puncturedLEFT NR 1 SLAT HAS A PUCTURE AT 55.5 INCHES FROM INBD EDGE AND 6.5 INCHES FROM T/E OF SLAT HOLE IS .5" X .75". REMOVED DAMAGED SKIN AND CORE, FABRICATED CORE PLUG AND DOUBLER, BONDED AND SEALED REPAIRED AREA IAW SRM 51-70-10, REPAIR NR 2 AND EA F-5750-155424Sep 13, 2011 · N926FD · Boeing 7572S7 · Leading Edge DevicesSDR FDEA201106272453Skin · damagedFUSELAGE SKIN DAMAGED DURING INSTALATION ON SURROUND STRUCTURE AT STA 439 BETWEEN S-2L TO S-3L COMPLIED WITH EA F-5330-146550 REF FAA FORM 8110-3. MAJOR REPAIR.Jun 27, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201106142243Bushing · gougedRIGHT PYLON OTBD WING STRUT BUSHING HAS GOUGES. R & R BUSHING IAW SOPM 20-50-03 AND EA F-5720-146285. MAJOR REPAIRJun 14, 2011 · N926FD · Boeing 7572S7 · Nacelle/Pylon, Main FrameSDR FDEA201106012076Skin · damagedLEFT PYLON, LT SIDE SKIN AT P/P STA 204 HAS ELONGATED HOLE. NACELLE/PYLON - SKIN GOUGE ADJACENT TO TOOLING HOLE, COMPLIED WITH/ REPAIR IAW EA F-5450-146516. THIS IS A CAT "A" MAJOR REPAIR.Jun 1, 2011 · N926FD · Boeing 7572S7 · Nacelle/Pylon, Plate/SkinSDR FDEA201105231933Frame · gougedFUSELAGE INTERIOR UPPER DOOR REINFORCEMENT STRAP HAS GOUGE APPROX AT STA 1653 ABOVE R-4 DOOR CUTOUT. ACCOMPLISHED FUSELAGE MAIN FRAME- SECTION 46 - UPPER DOOR SILL STRAP REPAIR, BS 1654, IAW EA F-5310-146288, DATED 04/25/2011. REF FORM 8100-9 DATED 05/19/20May 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201105171858Floorbeam · misrepairedFLOORBEAM REPAIR AT STA. 324, RBL 45 - RBL 60 UPPER TEE REQUIRES REPLACEMENT DUE TO NOT BEING IAW APPROVED DATA. REMOVED UPPER TEE ON FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW TEE. INSTALLED TEE, IAW SRM 51-40-02, AND DWG 141N2932, MAJOR REPAIR.May 17, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR FDEA201105071777Stringer · misrepairedEXISTING STRINGER REPAIRS AT STA 1450-1470, STR 28L REQUIRES REPLACEMENT DUE TO NOT BEING INSTALLED IAW APPROVED DATA. REMOVED AND REPLACED EXISTING STRINGER REPAIRS, BS 1450-1479, S28L, PER SRM 53-00- 03, REPAIR NR 2, DETAIL 1. FABRICATED HAT SECTION, 2EA.,May 7, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Longeron/StringerSDR FDEA201105071776Skin · misrepairedFUSELAGE EXTERNAL SKIN REPAIR AT STA 540-550, STR-27L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. R & R DOUBLER & FILLER STA 540-550 STR -27L IAW SRM 51-40-02 /SRM 53-00-01, FIG 201, TABLE I - III, REPAIR 15, W/ DOUBLER PN 2024-T3-071May 7, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201105051759Skin · misrepairedEXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STA. 740, STR 25R REQUIRES REPLACEMENT DUE TO NOT BEING IN COMPLIANCE WITH APPROVED DATA. REMOVED EXISTING DOUBLER/FILLER, BS 730-750, S-25R. HFEC INSP. SKIN CUTOUT, INITIAL HOLES PER NTM 51-00-19, PT.6 AND NTM 51-00May 5, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201105041751Skin · misrepairedSKIN REPAIR AT STA.740-760, STR 27R TO 28R REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. REMOVED DOUBLER/FILLER AT BS 740-760, S-27R-S-28R, PER SRM 51-40-02. HFEC SKIN CUTOUT, INITIAL HOLES PER NTM 51-00-19, PT.6, AND NTM 51-00-16, PT.6. May 4, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201104251618Channel · mismanufacturedUNABLE TO INSTALL CHANNEL SPLICE, BETWEEN STA 1620 TO STA 1640, RBL 60, WL 208.1, WILL HAVE SHORT EDGE CONDITION AT (1 EA) 0.100 HOLE LOCATION AT BS 1620 - 1640 RBL 60 A CREASE BEAM REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MApr 25, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201104061366Frame · gougedFRAME AT BS 1140, S2L, IS GOUGED. REMOVED DAMAGED SECTION OF FRAME IAW SRM 51-40-02. LOCATED, TRIMMED AND DRILLED FRAME AND SPLICES SRM 53-00-07, P.201/202, FIG 201. TREATED AND PRIMED FRAME AND SPLICES IAW SRM 51-20-01. INSTALLED FRAME REPLACEMENT AND 4 EApr 6, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201103291235Frame · damagedSECTION 46, STA 1640, LBL63.0 BETWEEN WL207-200 UNABLE TO LOCATE 657N3161-11 FITTING DUE TO EXISTING FASTENER HOLES ON THE FRAME, 2 EA ARE NOT POSITIONED AS DEPICTED ON DWG 657N3160, SH 2, REV D -FIGURE "E". AT BS 1640, LBL 63, WL 207, FRAME REPAIR WAS ACCOMMar 29, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201103291234Seat Track · damagedSEAT TRACK INSTL SEC46 UNABLE TO INSTALL 657N3311-1 SPLICE FITTING AT STA 1280 LBL 45.50, EXISTING FASTENER HOLES ON FLOORBEAM WEB ARE NOT POSITIONED ON DWG 657N3311, SH 5 AND SEAT TRACK 657N3318-7 REQ TO TRIM FWD EDGE FLANGE .300 APPROX TO MAINTAIN .10Mar 29, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR FDEA201103231284Beam · crackedVERTICAL STABILIZER LT FIXED T/E BEAM IS CRACKED AT RUD STA 97.354 SDR ENTERED IN ERROR. CONSIDERED MINOR REPAIRMar 23, 2011 · N926FD · Boeing 7572S7 · Vertical StabilizerSDR FDEA201103231680Skin · misrepairedEXISTING FUSELAGE SKIN REPAIR AT STA 274-285, STR 16L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. REMOVED AND REPLACED EXTERNAL FUSELAGE SKIN DOUBLER / REPAIR AT STA 274- 285, STR 16L IAW SRM 53-00-01 FIG 201 REPAIR 15. CAT. "B" REMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201103231587Crease Beam · damagedUNABLE TO INSTALL 657N4308-1 CHANNEL SPLICE, BETWEEN STA.1620 TO STA 1640, LBL60.00 WL208.1; WILL HAVE SHORT EDGE MARGIN CONDITION AT -1 EA.- 0.10" HOLE LOCATION. AT BS 1640, LBL60, WL208 A CREASE BEAM REPAIR WAS ACCOMPLISHED. CLASSIFIED AS A MAJOR.Mar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, StructureSDR FDEA201103231521Sill · misrepairedREPAIR ON DOOR SILL/CREASE BEAM AT STA 1370, WL 208, RBL 62 REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R CREASE BEAM CHORD, FROM BS 1290-1405, RBL 62, PN: 146N8326-2, BATCH NR 2032339, IAW SRM 51-40-02, AND DWG 146N8326. MAJOR REPAIRMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201103231504Frame · damagedFRAME STA 1640, RBL 63, WL 208 HAS INCOMING DAMAGE, 2 EA AREAS ON INBD J ANGLE, 2 EA GOUGES AND THE WEB HAS CUT. FRAME REPAIREDMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201103231283Frame · gougedFRAME STA 1640, RBL63, WL208 HAS 2 EA AREAS OF DAMAGE INBD JANGLE HAS EEA GOUGES AND THE AFT FRAME WEB HAS CUT (INCOMING DAMAGE FOUND AFTER FLOORBEAM REMOVAL) THIS SDR WAS GENERATED IN ERROR. THE ABOVE DISCREPANCY IS CAPTURED ON THE FAA FORM 337, WHICH IS ISSUMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201103231408Skin · misrepairedFUSELAGE SKIN REPAIR 60" AFT OF L2 DOOR, 6" ABOVE FLOORLINE REQUIRES REPLACEMENT, DUE TO NOT COMPLYING TO APPROVED DATA. REMOVED AND REPLACED DOUBLER AT BS 775, S16L-S17L, PER SRM 51-40-02, AND SRM 53-00- 01, REPAIR 16, BATCH 1928869, PER SRM 53-00-01, FIG.2Mar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201103231186Seat Track · gougedSEAT TRACK AT STA 1075-1180, RBL45.50 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS. SEAT TRACK FROM BS 1075-1180, RBL 45.5, OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, P 102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 00019046632 AND INMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103231185Seat Track · gougedSEAT TRACK AT RBL24.75 FROM STA 1075-1180 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS, SEAT TRACK FROM BS 1075-1180, RBL 24.75 OUT OF LIMITS IAW SRM 53-00-52, FIG101, DETAIL 1, P.102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 000194663 AND INSMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103181077Beam · misinstalledUNABLE TO INSTALL 657N3338-36 SPLICE AND 657N338-30 ANGLE CLIP AT STA 1180 RT DUE TO THE INCOMING CONDITION OF THE 144N5214-1 RT INBD CHORD LOCATION TOO FAR INBD. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION , ON MAE MOD W/C 11Mar 18, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201103100930Floor Support · corrodedAFT CARGO STA. 1400 TO STA.1420 AT BL 0 FLOOR SUPPORT WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-53, FIG. 101 DETAIL V, REMOVED AND REPLACED FLOOR SUPPORT WEB IAW SRM 51-40- 02 AND SRM 53-00-53, REPAIR CLASSIFIMar 10, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201103030833Floorbeam · misalignedSTA 700 INCOMING REPAIR AT RBL40 WILL INTERFERE WITH PTF MOD. R & R FLOORBEAM AT STA 700, BETWEEN RBL 70 TO LBL 70". BAC1518-338/18A, BATCH NR 0001922129, IAW SRM 53-30-51, FIG 1, PAG-4 AND SRM 51-40-02, AND REINSTALLED ATTACH PARTS, FROM ITEM 3 THRU 12, IAWMar 3, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR FDEA201102220679Floorbeam · corrodedSTA 377, FLOORBEAM, LBL-60 HAS CORROSION ON LAWER SIDE OF UPPER FLANGE AROUND NUT PLATE HOLES. REMOVED CORROSION AND CHECK LIMITS ORIG MAT. 0.125 AFTER REWORK 0.050. FOUND OUT OF LIMITS IAW SRM 53-00-51 DET III. R & R FLOORBEAM IAW SRM 51-40-02 WITH MAT PFeb 22, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR FDEA201102190631Frame · gougedFRAME AT STA 1280 HAS GOUGES BETWEEN AREAS OF STR 11R-17R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, P103; ORIGINAL MATERIAL IS .071", AFTER REWORK IS .050", LOSS IS .021". R & R FRAME SPLICE AT BS 1282, S12R-S13R, IAW SRM 53-00-07, FIG Feb 19, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201102170595Seat Track · gougedBS 418-440, RBL 24, SEAT TRACK GOUGED. BLENDED AREA IAW SRM 53-00-52, FIG 101, DETAIL 1. CHECKED LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, AND FOUND OUT OF LIMITS; BEFORE: .53", AFTER: .47", LOSS: .060". REMOVED SEAT TRACK IAW SRM 51-40-02, AT BS 418-440, RFeb 17, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102170594Seat Track · gougedBS 418-440, RBL 45, SEAT TRACK GOUGED. BLENDED AREA AND CHECKED LIMITS IAW SRM 53-00-52. ORIGINAL MATERIAL WAS .053", AFTER REWORKIS .047", LOSS WAS .060", FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. REMOVED SEAT TRACK AT BS 418-440, RBL 45, IAWFeb 17, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102120549Frame · gougedMDC FRAME AT STA 1280 HAS GOUGES ON AREAS BETWEEN STR S11L & S17L. REPAIRED IAW EA F-5310-146523, MAJOR REPAIR.Feb 12, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201102110535Floorbeam · corrodedMAIN DECK, BS 365.25 FLOORBEAM, BETWEEN RBL 45 - 58, UNDERNEATH UPPER CHORD, HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION BY BLENDING AREA IAW SRM 51-10-02 AREA OUT OF LIMITS. ORIGINAL MAT .125 AFTER REWORK .077 EXCEEDS MAX ALLOWABLE DAMAGE OF 10 PFeb 11, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR FDEA201101180269Feeder Cable · burnedPOWER FEEDER CABLE, PN: W2800-0006-2/0, AT BS 405, S5L, IS BURNED AND ARCHED. STAND OFF SUPPORT ROD IS BURNED OFF AS WELL. R & R APU POWER FEEDER CABLE IAW SWPM 20-10-21, AND WDM 24-21-41. STANDOFF SUPPORT ROD DISPOSITIONED ON MOD W/C 118450613AZD. OPS CHEJan 18, 2011 · N926FD · Boeing 757222 · Electrical Power System Wiring
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