N806FT

Service difficulty reports not matched to an aircraft · 56

They name N806FT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N806FT' AND registry_match IS NULL
  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 P5CA0200698Gearbox · failedSHORTLY AFTER T/O, #1 ENG. LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO 10psi & WAS STEADY; OIL QTY SHOWED FULL & WAS STEADY. PERFORMED LOSS OF OIL PRESSURE PROCEDURE IAW AFM. COULD NOT RESTORE ENG. OIL PRESSURE OR EXTINGUISH LIGHT, THEREFOREAug 28, 2002 · N806FT · Boeing 747249F · Powerplant SystemSDR P5CA0200686Autopilot Sys · malfunctionedB-AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODE. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM.Jun 30, 2002 · N806FT · Boeing 747249F · Autopilot SystemSDR P5CA0200685Wire · broken"A" AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODES. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM ID #036042 CTR #29299 IAW MEL 02-22-2-1 IN CONSULT W/ MTC & PLACARD INSTALLED. JFK MX FOUND BROKEN WIRE AT PINS 9 & 10 ON CONNECTOR DB193 Jun 30, 2002 · N806FT · Boeing 747249F · Autopilot SystemSDR P5CA0200690Acoustic Panel · damagedAPU EXHAUST ACOUSTIC LINER DAMAGED AT 01:30 O'CLOCK POSITION. APU LINER REMOVED & REPLACED IAW MM 49-81-02.Jun 29, 2002 · N806FT · Boeing 747249F · APU Exhaust SystemSDR P5CA0200689Shroud · crackedCRACKS FOUND ON NR 1 ENG TURBINE COOLING SHROUD AT 8 & 2 O'CLOCK POSITIONS. RT (2 CRACKS) NR 1 IS 5 INCHES LONG & NR 2 IS 2 INCHES LONG. LT (4 CRACKS) NR 1 IS 3 INCHES LONG, NR 2 IS 5 INCHES LONG, NR 3 IS 1.5 INCH LONG & NR 4 IS 1.5 INCH LONG. ALSO BRACKET Jun 29, 2002 · N806FT · Boeing 747249F · Engine Cooling SystemSDR P5CA0200688Panel · crackedCRACK 15" LONG FOUND RH WING UPPER SKIN LE FIXED PANEL AT WS 834 TO WS 862. PANEL SHOWS 15 X 30 IN. SQ AREA DELAMINATED. LEADING EDGE FIXED PANEL AT WS 834 TO WS 862 REMOVED & NEW PANEL INSTALLED IAW SRM 51-10-01, PG 8, SECT 6, PARA A-B-C. ALSO SRM 51-30-02.Jun 29, 2002 · N806FT · Boeing 747249F · Wing, Plate/SkinSDR P5CA0200687Door · crackedA 2 INCH LONG CRACK FOUND ON APU INLET DOOR OUTSIDE LOWER FORWARD CORNER. COMPOSITE REPAIR CARRIED OUT WITH REF TO SRM 51-40-06. AREA PROTECTED WITH REF TO SRM 51-21-01.Jun 27, 2002 · N806FT · Boeing 747249F · APU Cowling/ContainmentSDR P5CA0200651Flap Track · corrodedFOUND LIGHT CORROSION, AREA 600, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 5, 6, 7 & 8 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801.Feb 20, 2002 · N806FT · Boeing 747249F · Trailing Edge FlapsSDR P5CA0200650Flap Track · corrodedLEVEL 1 CORROSION: FOUND LIGHT CORROSION, AREA 500, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 1, 2, 3 & 4 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801.Feb 20, 2002 · N806FT · Boeing 747249F · Trailing Edge FlapsSDR P5CA0200649Bolt · wornWORN LT WING BODY GEAR, AREA 751; SUPPORT ROD BOLT WORN. REMOVED BOLTS/BUSHINGS AND CLEANED UP. REASSEMBLED IAW MM 32-13-00 WITH LUBRICATION AND NEW WASHERS INSTALLED TO CORRECT ITEM. FOUND DOOR TO ROD BEARINGS AND BOLTS NOW WITHIN LIMITS. OK FOR SERVICE.Feb 20, 2002 · N806FT · Boeing 747249F · FastenersSDR P5CA0200629Wire · brokenRT BODY GEAR LEFT REAR (NR 11) ANTI-SKID LIGHT CAME ON AND WOULD NOT RESET. WHEEL ASSY RETORQUED FOR PRECAUTION PER MM 32-45-01. NR 11 BRAKE DEACTIVATED PER MEL. REPAIRED BROKEN WIRES AT TRANSDUCER ELECT CONNECTION PER MM STANDARD PRACTICES. REACTIVATED NRJan 11, 2002 · N806FT · Boeing 747249F · Brake Anti-Skid SectionSDR P5CA0100613Fairing · damagedL/H HORIZONTAL STABILIZER STA 560 OUTBOARD TIP - AFT WEDGE 6" SECTION BROKEN OFF. REMOVED & REPLACED T/E & BOTTOM ACCESS PANELS PER SRM 51-10-01.Nov 18, 2001 · N806FT · Boeing 747249F · Horizontal Stabilizer StructureSDR P5CA0100606Web · crackedNOSE GEAR WHEEL WELL FRAME WEB CRACKED, APPROX. 1/8" LONG, BY INSULATION HOLES FIRST & FOUR FROM FLOOR CHORD ANGLE ON RIGHT SIDE. OPENED HOLES TO 7/16", RE-INSPECTED BY H.F.E.C. - NO INDICATIONS. REPAIRED IAW BOEING SERVICE LETTER PAO-LGB-01-0015514, SB74752Oct 31, 2001 · N806FT · Boeing 747249F · Fuselage Main, StructureSDR P5CA0100569Slide · defectiveRT UPPER DECK SLIDE BLOWN BY MAINTENANCE AND ONLY HALF INFLATED. REPLACED U/D RIGHT SLIDE ASSIST BOTTLE. REMOVED AND REPLACED U/D RIGHT SLIDE FOUND SHEARED CABLE. P/N ON 7A1248-36 S/N ON G476.Jun 12, 2001 · N806FT · Boeing 747249F · Escape SlideSDR P5CA0100466Fire Warning · activatedNR 2 ENG FIRE DET LIGHT AND FAULT LIGHT CAME ON A-LOOP WITH A FIRE WARNING. ENGINE SHUT DOWN AND BOTTLE FIRED. REPLACED NR 2 LFT FIRE BOTTLE. P/N ON 33603903P, S/N M2621Feb 25, 2001 · N806FT · Boeing 747249F · Fire DetectionSDR P5CA0000344Skin · corrodedLEVEL 1 CORROSION FOUND RT WING I/B MID FLAP TOP SKIN PANELS FOUND WITH CORROSION IN SEVERAL PLACES ON THE UPPER T-CHORD. CORRODED TJ-CHORD REPLACED PER SRM 51-40-04 FIG 1.Oct 17, 2000 · N806FT · Boeing 747249F · Trailing Edge FlapsSDR P5CA0000343Frame · crackedCRACK FOUND ON FRAME 320 RHS AT WINDOW POST INTERSECTION, DURING COCKPIT WINDOW INSPECTION. FRAME 320 RHS TEE CHORD REPAIR C/OUT PER SRM 51-40-04.Oct 17, 2000 · N806FT · Boeing 747249F · Fuselage Main, FrameSDR P5CA0000342Frame · crackedCRACK FOUND ON FRAME 320 RHS AT COCKPIT WEB. WEB REPAIR C/OUT PER SRM 51-40-02.Oct 17, 2000 · N806FT · Boeing 747249F · Fuselage Main, FrameSDR P5CA0000341Skin · damagedDAMAGE FOUND ON FUSELAGE SKIN NOT SMOOTH AT BS 1826 TO BS 1837 BETWEEN 542L AND 543L. PAINT REMOVED NDT INSPECTED AND NO CRACKS NOTED, AREA RESTORED PER SRM 51-40-01 AND PAINTED.Oct 17, 2000 · N806FT · Boeing 747249F · Fuselage Main, Plate/SkinSDR P5CA0000340Panel · crackedCRACK FOUND AT BS 1241 CANTED BULKHEAD CLOSEOUT PANELS (LHS 2.5 AT O/B LOWER CORNER, RHS 5.0 AT O/B EDGE FASTENERS). BS 1241 LT & RT CANTED BULKHEAD CLOSEOUT PANELS REPLACED PER SB 747-53-2329.Oct 17, 2000 · N806FT · Boeing 747249F · Fuselage Main, Plate/SkinSDR P5CA0000339Bolt · brokenOUTBOARD T/E AFT FLAP ATTACHMENT FITTING TO MID FLAP MOUNTING BOLTS FOUND SHEARED DURING NISPECTION. ATTACH FITTING MOUNTING BOLTS REPLACED PER MM 27-51-04.Oct 17, 2000 · N806FT · Boeing 747249F · Trailing Edge FlapsSDR P5CA0000338Bolt · brokenNR 2 SEQUENCE CARRIAGE ASSY HOOK BOLT FOUND SHEARED DURING INSPECTION. BOTH HOOK BOLTS REPLACED PER MM 27-51-30.Oct 17, 2000 · N806FT · Boeing 747249F · Wing Miscellaneous StructureSDR P5CA0000337Hook · looseABNORMALITY FOUND ON RT WING NR 7 POSITION SEQUENCE CARRIAGE HOOK ASSY FOUND LOOSE. REPLACE WITH NEW TOGGLE SEQUENCE ASSY P/N 65B17198-10, INSTALLED PER MM 27-51-30.Oct 17, 2000 · N806FT · Boeing 747249F · Wing Miscellaneous StructureSDR P5CA0000345Skin · corrodedLEVEL 1 CORROSION FOUND ON UPPER SURFACE OF UPPER SKIN PANEL OF WING CTR TANK JUST FWD OF BS 140 BETWEEN RBL 2 AND RBL 9. CORROSION BLENDED OUT AND REPAIRED PER PAO-SIN-00-00043F & -00045H. FAA FORM 8110-3 ISSUED.Oct 16, 2000 · N806FT · Boeing 747249F · Fuselage Main, Plate/SkinSDR P5CA0000334Intercostal · crackedCRACK FOUND ON MAIN DECK STA 997 INTERCOSTAL AT RBL 75 FOUND ALONG FASTENER HOLE. MAIN DECK STA 997 INTERCOSTAL REPAIR C/OUT PER SRM 51-40-03.Oct 13, 2000 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA0000333Rod · damagedDAMAGE FOUND L/E SUPPORT ROD ASSY FOR RIB AT WING STA 878.55 FOUND CHAFED THRU. SUPPORT ROD ASSY REPLACED PER SRM 51-30-04.Oct 13, 2000 · N806FT · Boeing 747249F · Leading Edge DevicesSDR P5CA0000332Drain Valve · crackedCRACK FOUND ON 13 OFF DRAIN VALVE ASSY AT BELLY FUSELAGE BS 2160 TO BS 2180. ALL 13 DRAIN VALVE ASSY REPLACED PER MM 51-41-03.Oct 13, 2000 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA0000331Fitting · damagedABNORMALITY FOUND ON RT WING I/B FOREFLAP O/B SEQ CARRIAGE ATTACHMENT FITTING BEARING FOUND MIGRATED. NEW FITTING P/N 65B39025-34 INSTALLED PER MM 27-51-02.Oct 13, 2000 · N806FT · Boeing 747249F · Leading Edge DevicesSDR P5CA0000330Beam · crackedCRACK FOUND ON NOSE WHEEL WELL VERTICAL BEAM WEB AT STA 320 LHS, FOUND 2 CRACKS APPROX .75 & .1875 INCH LENGTH NDT REPORT POLAR/4284/00 REFERS. STA 320 LHS VERT BEAM WEB REPARI C/OUT PER SRM 51-40-02.Oct 13, 2000 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA0000329Structure · corrodedLEVEL 1 CORROSION FOUND ON VERTICAL FIN 4TH BALANCE WEIGHT (COUNTING FROM TOP TO BOTTOM). CORROSION TREATMENT PER CPM PART 1, 20-40-00 P.24 C/OUT WEIGHT REINSTALLED, MM 20-51-01.Oct 13, 2000 · N806FT · Boeing 747249F · Vertical StabilizerSDR 20000919SH015Duct · brokenNR 3 ENGINE FIRE WARNING ON TAKEOFF. BOTTLE DISCHARGED. ENGINE SHUT DOWN. AIRCRAFT RETURNED TO AKL. FOUND BROKEN 8TH STAGE ANTI-ICE DUCT THROTTLE CABLE MELTED AND JUMBLED. WIRE BUNDLES MELTED, ENGINE CHANGED. OPERATOR: POLAR AIR CARGO AKL TO KHG. (X)Aug 26, 2000 · N806FT · Boeing 747249F · Engine Anti-Icing SystemSDR P5CA0000335Panel · crackedCRACK FOUND AT BS 1240 RBL 5.0 CLOSURE PANEL AT CANTED BULKHEAD COMMON TO APU FUEL FEED LINE/SHROUD FOUND CRACKED AROUND FASTENER LOCATION. CLOSURE PANEL REMOVED AND NEW PANEL INSTALLED PER SRM 51-30-02.Jul 24, 2000 · N806FT · Boeing 747249F · Fuselage Main, Plate/SkinSDR P5CA9900633Web · crackedFOUND WEB CRACKED AT BS 434L NR 1 MED. TRIMMED AREA AND FABRICATED PART FOR REPAIR PER SRM 53-10-04 AND 51-30-02.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA9900632Angle · crackedFOUND 1.6 INCH CRACK ON RADIUS OF ANGLE FWD OF BS 434 UNDER STR 26. FABRICATED PARTS AND REPLACED PER SRM 51-30-02.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA9900631Vertical Beam · crackedFOUND INDICATION OF CRACKS AT HOLE ON VERTICAL BEAM AT BS 30L. STOP DRILLED AND FABRICATED REPAIR PER SRM 53-10-04 FIG 94 PG 8 DETAIL 5.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA9900630Bulkhead · crackedCRACKS FOUND ON BS 1000 IN THE RADIUS BETWEEN STR 46 AND 47 LEFT AND RIGHT SIDES. STOP DRILLED, EDDY CURRENT PER SB 530-2316R1 AND SRM 51-10-01 FIG 2.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Main, BulkheadSDR P5CA9900629Bulkhead Flange · crackedFOUND CRACK ON FLANGE OF PRESSURE BULKHEAD AT BS 140 WL 280 BL 10L. TRIMMED DAMAGED AREA AND FABRICATED NEW ANGLE PER SRM 51-40-03 AND 51-10-02.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Main, BulkheadSDR P5CA9900628Clips · crackedFOUND CRACKS ON CLIPS AT NOSE WHEEL WELL VERTICAL BEAM WEB AT BS 340 R. REPLACED CLIPS PER SRM 51-30-02.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA9900627Floorbeam · damagedFOUND SHEARED RIVETS AT BS 400 ON FLOORBEAM LEFT SIDE. REPLACED RIVETS PER SRM 51-30-02.Jun 29, 1999 · N806FT · Boeing 747249F · Fuselage Main, Floor BeamSDR P5CA9900423Skin · damagedDURING CLOSING LOWER FWD CARGO DOOR, AEROGROUND HIGH LOADER HIT DOOR AND CAUSED DAMAGE TO LOWER AFT CORNER. REWORKED LOWER CORNER OF FWD CARGO DOOR PER SRM 51-10-01.Mar 10, 1999 · N806FT · Boeing 747249F · Cargo/Baggage DoorsSDR P5CA9900192Angle · crackedAFT PIT STAT 1726 BL 30L ANGLE FOUND CRACKED JUST BELOW TRACK. REMOVED AND FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-01, 51-10-03 AND 51-30-02.Feb 19, 1999 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA9900191Keel Beam · corrodedLEVEL 1 CORROSION FOUND ON KEEL BEAM AFT END LEFT AND RIGHT SIDE BS 1100 TO 1300. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-01 AND 53-10-02.Feb 15, 1999 · N806FT · Boeing 747249F · Fuselage Main, KeelSDR P5CA9801614Fairing · delaminatedNR 8 FIXED FAIRING TAIL CONE LOWER SKIN FOUND DELAMINATED. SANDED DOWN DELAMINATION AREA AND REPARIED PER SRM 51-40-09.Dec 4, 1998 · N806FT · Boeing 747249F · Aerodynamic FairingsSDR P5CA9801221Panel · crackedRIGHT WING GEAR FLYING DOOR PANEL CRACKED. REPAIRED PANEL IAW 747 SRM 51-40-09.Aug 3, 1998 · N806FT · Boeing 747249F · Landing Gear DoorsSDR P5CA9801216Panel · delaminatedRIGHT WING UPPER SURFACE OF FLYING PANEL HAS A 2X2 AREA OF DELAMINATION AT TITANIUM COFFIN DOUBLER. REMOVED AND REPLACED RIGHT HAND WING FLYING PANEL IAW SRM 57-22-89, 51-30-02 AND POLAR MA A5730-02:01.Aug 3, 1998 · N806FT · Boeing 747249F · Wing, Plate/SkinSDR P5CA9801219Floor · delaminatedLEVEL 1 CORROSION ON FLOOR PANEL UNDER LT UPPER DECK SLIDE CARRIAGE DELAMINATED AND MINOR CORROSION. FOUND MINOR SURFACE CORROSION, REMOVED IAW SRM 51-10-06 AND REPAIRED DELAMINATION IAW SRM 51-40-05.Aug 2, 1998 · N806FT · Boeing 747249F · Fuselage Floor PanelSDR P5CA9801223Support · damagedFWD LOWER CARGO COMPARTMENT STA 860 CENTER GUIDE FLOOR SUPPORT DAMAGED. REMOVED DAMAGED FLOOR SUPPORT AND WEB REINSTALLED PERMANENT REPAIR IAW SRM 51-40-02.Aug 1, 1998 · N806FT · Boeing 747249F · Fuselage Miscellaneous StructureSDR P5CA9801217Skin · corrodedLEVEL 1 CORROSION UNDER THE ATC ANTENNAS. REMOVED CORROSION FROM UNDER A/C ATC ANTENNAS WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01.Aug 1, 1998 · N806FT · Boeing 747249F · Fuselage Main, Plate/SkinSDR P5CA9801220Antenna · corrosionLEVEL 1 CORROSION ON THE NR 1 AND NR 2 ANTENNA BODY. REPLACED NR 1 AND NR 2 ATC ANTENNAS IAW MM 34-53-03.Jul 31, 1998 · N806FT · Boeing 747249F · ATC Transponder SystemSDR P5CA9801218Exhaust Sleeve · delaminatedNR 4 ENGINE EXHAUST SLEEVE INNER SKIN DELAMINATED AT 6 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENG EXHAUST SLEEVE ASSY IAW MM 78-11-02.Jul 31, 1998 · N806FT · Boeing 747249F · Engine Collector/Tailpipe/Nozzle
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