N921FT

Service difficulty reports not matched to an aircraft · 253

They name N921FT, 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 = 'N921FT' 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 P5CA0601471Skin · corrodedCORROSION BS 1241 BL 0 TO LBL 11. REPAIRED IAW SRM 51-10-01 PAGE 13, 14.Mar 31, 2006 · N921FT · Boeing 747283B · Fuselage Main, Plate/SkinSDR P5CA0601470Skin · damagedAFT CARGO DOOR CUTOUT HAS 1 INCH HALF CIRCLE BLEND 8 INCHES FROM BOTTOM OF CUTOUT. REPAIRED PER BOEING 8100-9 PER ECRA 921FT-57-747-017, SRM 51-30-02.Mar 31, 2006 · N921FT · Boeing 747283B · Fuselage Main, Plate/SkinSDR P5CA0601469Structure · corrodedRIGHT WING TRAILING EDGE STA 710.0 - 718.0 CORROSION. REPAIRED PER BOEING 8100-9, PER ECRA 921FT-57-747-014.Mar 31, 2006 · N921FT · Boeing 747283B · Wing Main, Frame StructureSDR P5CA0601468Spar · corrodedWS 1010-1038 RT FRONT SPAR WEB CORROSION. REPAIRED PER BOEING 8100-9, PER ECRA 921FT-57-747-013.Mar 31, 2006 · N921FT · Boeing 747283B · Wing SparSDR P5CA0601467Spar · corrodedCORROSION ON LEFT WING LEADING EDGE CAVITY - SPAR WEB - LOWER CHORD LES 1322. REPAIRED PER BOEING 8100-9. REPLACED LEFT WING L/E SPAR WEB LWR CHORD PER ECRA 921-57-747-011.Mar 31, 2006 · N921FT · Boeing 747283B · Wing SparSDR P5CA0601466Bulkhead · corrodedTHE 1241 BULKHEAD CORRODED AT LBL 10 TO RBL 98 (BELOW UPPER CHORD). REPAIRED PER BOEING 8100-9. REMOVED CORROSION AT BS 1241 LBL 10 TO RBL 98. WORK ACCOMPLISHED ON ECRA 921FT-57-474-010 REV NEW.Mar 31, 2006 · N921FT · Boeing 747283B · Fuselage Main, BulkheadSDR P5CA0601465Skin · corrodedEXFOLIATION CORROSION ON LEFT WING LOWER SKIN AT AFT SPAR AREA WS 1376. REPAIRED PER BOEING 8100-9. FABRICATED AND INSTALLED 1-2-3-4 PLATES FILLER PER ECRA 921FT-57-747-004.Mar 31, 2006 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0601464Skin · crackedLEFT WING LOWER SKIN BETWEEN DRY BAY PANELS AT WS 1516 HAS SKIN CRACKED. REPAIRED PER BOEING 8100-9. REPAIRED CRACKED LEFT WING LOWER SKIN PER ECRA 921FT-57-747-001.Mar 31, 2006 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0501419Transmitter · failedON TAKEOFF ROLL, CREW REPORTED NR 3 ENGINE EPR WOULD NOT ADVANCE ABOVE 1.2 EPR, FULL TRAVEL OF THROTTLE HAD NO EFFECT. TAKEOFF ABORTED AT 80 KTS IAS EPR ON NR 3 STAYED AT 1.2 UNTIL ENGINE SHUTDOWN. REPLACED EPR TRANSMITTER, PERFORMED LEAK CHECK AND RAN ENGINDec 15, 2005 · N921FT · Boeing 747283B · Engine Pressure Ratio (EPR)SDR PDCA0501420Transmitter · failedON CLIMB, NR 3 ENGINE EPR STARTED DECREASING AT FL310 EPR IND., ON DESCENT IT READ HIGH (1.24 AT 150 WITH THRUST LEVERS IDLE) (CORRECTIVE ACTION) REPLACED EPR TRANSMITTER IAW MM 77-11-00 AND DEFERRED OPS CHECK IAW DDPG 77-4.Dec 12, 2005 · N921FT · Boeing 747283B · Engine Pressure Ratio (EPR)SDR P5CA0501407Skin · corrodedCORROSION ON RT UPPER SKIN AFT OF REAR SPAR WS 560 TO 575. REMOVED CORROSION & REPAIRED IAW BOEING REPAIR PROCEDURE 1-129539127-5 AND 8100-9.Oct 19, 2005 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0501402Panel · crackedLEFT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02.Sep 22, 2005 · N921FT · Boeing 747283B · SpoilersSDR P5CA0501401Support Beam · crackedLEFT WING TRAILING EDGE SUPPORT BEAM UPPER CHORD CRACKED (APPROX 2 INCHES) AT WS 528.20, WBL 235.20.Sep 22, 2005 · N921FT · Boeing 747283B · Wing Miscellaneous StructureSDR P5CA0501400Fitting · corrodedLEFT WING AT UPPER CHORD OF SPLICE FITTING OF WING REAR SPAR HAS CORROSION BETWEEN WS 553 AND WS 558. CORROSION BLENDED OUT IAW SRM 57-30-01. HFEC & ULTRASONIC INSPECTION OF AREA CONFIRMED REMOVAL OF CORROSION IAW NDT 06-7170 PT 6, 51-00-00 FIG 23, 12. D6-71Sep 22, 2005 · N921FT · Boeing 747283B · Wing, Attach FittingsSDR P5CA0501404Panel · crackedLT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REPLACED NR 3 SPOILER ASSEMBLY IAW AMM 27-61-02.Sep 21, 2005 · N921FT · Boeing 747283B · SpoilersSDR P5CA0501389Switch · out of adjustNR 2 ENGINE REVERSER UNSTOW. ADJUSTED NR 2 REVERSER STOW SWITCH PER MM 78-31-00.Aug 26, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501387Module · failedDURING CRUISE, LEADING EDGE FLAP GROUP 1, 2, 3, 4 LEFT AND 1 RIGHT DISPLAY AMBER, GROUPS 1 & 2 LEFT ALSO DISPLAY GREEN. REPLACED MODULE OPS CHECK OK PER MM 27-88-00.Aug 26, 2005 · N921FT · Boeing 747283B · Trailing Edge Flap Control SystemSDR P5CA0501388Actuator · failedSIDE CARGO DOOR HOOK ACTUATOR FAILED IN ELECTRICAL MODE. DEFERRED PER MEL 52-20.Aug 24, 2005 · N921FT · Boeing 747283B · Cargo/Baggage DoorsSDR P5CA0501383Door · missingON POSTFLIGHT WALKAROUND, FOUND LEFT BODY GEAR O/B SHOCK STRUT DOOR MISSING. REPLACED DOOR PER MM 32-14-06.Jul 24, 2005 · N921FT · Boeing 747283B · Landing Gear DoorsSDR P5CA0501377Clamp · failedCREW REPORTED NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE, MM 36-13-00. OPS AND LEAK CHECK OK MM 71-00-00.Jun 10, 2005 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR P5CA0501362Clamp · failedNR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE. OPS AND LEAK CHECK OK PER MM 36-13-00 AND 71-00-00.Jun 10, 2005 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR P5CA0501335Data Card · failedGPS DATA CARD FAILED. TRANSFERRED TO DMI 34058 PER MEL 34-27-2S.Apr 3, 2005 · N921FT · Boeing 747283B · Global Positioning SystemSDR P5CA0501331Door · missingON POST FLIGHT NR 3 ENGINE REVERSER PANEL MISSING. ACCOMPLISHED INTERIM REPAIR PER SRM 51-00-04 AND SRM 51-40-16, ALSO GMM 3-17-1. TRANSFERRED TO C/O ITEM 921-179.Mar 20, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501325Warning Light · illuminatedNR 2 ENGINE THRUST REVERSER LIGHT CAME ON FLASHING AS ENGINE APPROACHED TAKE OFF EPR. DEFERRED T/R PER MEL NR 78-3-1B.Mar 3, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501324Engine · malfunctionedCREW REPORTED NR 1 ENGINE WOULD NOT MAKE TAKEOFF EPR. INSPECTED NR 1 ENGINE PER MM 71-00-00, OPENED MEL 77-4-1 FOR EPR UNRELIABLE.Feb 22, 2005 · N921FT · Boeing 747283B · Engine (Turbine/Turboprop)SDR P5CA0501310Seat Track · brokenON PREFLIGHT FOUND BOTH SEAT TRACKS BROKEN ON THE F/O'S SEAT (AFT SEAT TRACK). REMOVED & REPLACED BOTH LT & RT AFT SEAT TRACKS PER AMM 25-11-00.Jan 29, 2005 · N921FT · Boeing 747283B · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0501308Thrust Reverser · inoperativeNR 4 ENGINE THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. NR 4 ENGINE THRUST REVERSER DEACTIVATED PER MEL 78-01-2A. REF MM 78-31-00.Jan 21, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501307Pump · leakingDURING CLIMB NR 2 ENGINE OIL QTY DROPPED TO ZERO. AFTER 5 MINUTES OIL PRESSURE 40 PSI AND FLUCTUATING. OIL TEMPERATURE NORMAL. ENGINE SHUTDOWN. REPLACED EDP PER MM 29-141-05. LEAK AND OPS CHECK OK PER MM 29-11-05.Jan 21, 2005 · N921FT · Boeing 747283B · Hydraulic Pump (Electric/Engine), MainSDR P5CA0501306Pump · leakingLOSS OF NR 2 HYDRAULIC SYSTEM. HYDRAULIC QUANTITY WENT FROM 6.5 GALLONS TO ZERO IN LESS THAN 5 SECONDS. FOUND NR 2 ENG EDP CASING CRACKED. REMOVED NR 2 EDP PER MM 29-11-05 AND DEFERRED PER MEL 29-1A.Jan 20, 2005 · N921FT · Boeing 747283B · Hydraulic Pump (Electric/Engine), MainSDR P5CA0501297Pulley · wornON TAXI OUT, FLIGHT CONTROL CHECK REVEALED WHEN CONTROL WHEEL TURNED TO LEFT, NORMAL MOVEMENT OBSERVED. WHEN CONTROL WHEEL TURNED TO RIGHT IT STOPPED AT 10 DEGREES FOR 4-6 SECONDS THEN RETURNS SLOWLY TO NEUTRAL. FOUND CABLE PULLEY IN LT WHEEL WELL WORN. REPDec 29, 2004 · N921FT · Boeing 747283B · Aileron Tab Control SystemSDR P5CA0401296Switch · malfunctionedAT APPROXIMATELY 80 KNOTS TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AT OKO. STAB TRIM WAS AT THE EDGE OF THE GREEN BAN. CAPTAINS TRIM INDICATOR HAS NO CENTER INDEX. MAX THRUST WAS SET PRIOR TO BRAKE RELEASE AT TAKEOFF OKO. RESET GREEN BAND SWITCH PER Dec 29, 2004 · N921FT · Boeing 747283B · Stabilizer Position IndicatingSDR P5CA0401293Hydraulic Line · leakingNR 3 HYD SYS LOST 2 GALS IN THIS FLIGHT FROM UAM-HIK. FOUND LINE LEAKING FROM CASE DRAIN FOR NR 3 EDP. REMOVED EDP DUE TO LEAK. ITEM TRANSFERRED TO DMI 33554 PER MEL 29-1A.Dec 24, 2004 · N921FT · Boeing 747283B · Hydraulic System, MainSDR P5CA0401294Drain Mast · leakingNR 3 ENGINE HYD LEAK AT DRAIN MAST. FOUND HYD LEAK WITHIN LIMITS PER MM 29-11-00 FIG 601.Dec 23, 2004 · N921FT · Boeing 747283B · Hydraulic System, MainSDR P5CA0401289Proximity Switch · damagedNOSE LANDING GEAR ALT SQUAT SWITCH FOUND DAMAGED. REPLACED NLG ALT SQUAT SWITCH PER MM 32-60-00.Dec 20, 2004 · N921FT · Boeing 747283B · Landing Gear Position and WarningSDR P5CA0401284Thrust Reverser · malfunctionedNR 4 ENGINE THRUST REVERSER OPERATING LIGHT CAME ON IN FLIGHT. NO ADVERSE INDICATIONS. REPLACED PDU, NO HELP REV INOP. TRANSFERRED TO DMI 33496 PER MEL 78-2A. PLACARD INSTALLED.Dec 10, 2004 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0401278Thrust Reverser · damagedON POST FLIGHT, MAINTENANCE WALK AROUND, FOUND NR 1 RT REVERSER HALF HAS DAMAGE TO PREVIOUSLY REPAIRED AREA AT FWD EDGE BETWEEN 4 O'CLOCK AND 6 O'CLOCK. REPAIRED CARRIED OUT PER SRM 54-30-03 AND 54-03.Nov 17, 2004 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0401279Indicator · no indicationNR 3 ENGINE HAS NO EPR INDICATION WHEN ACCELERATING. TRANSFERRED TO DMI 33386 PER MEL 77-04-1.Nov 17, 2004 · N921FT · Boeing 747283B · Engine Pressure Ratio (EPR)SDR P5CA0401266Starter · malfunctionedNR 1 ENGINE WOULD NOT TURN ON, PYLON VALVE & START VALVE INDICATES OPEN. REPLACED STARTER, OPS CHECK OK PER AMM 80-11-00.Oct 30, 2004 · N921FT · Boeing 747283B · Engine StarterSDR P5CA0401242Flap · malfunctionedNR 2 LEFT LEADING EDGE WOULD NOT COME UP PNEUMATICALLY, OK ELECTRICALLY. RECYCLED FLAPS PNEUMATICALLY, NO HELP. TRANSFERRED TO DMI 33203.Oct 4, 2004 · N921FT · Boeing 747283B · Leading Edge Slat Control SystemSDR P5CA0401192Warning Light · illuminatedNR 2 ENG THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON FORWARD ANNUNCIATOR PANEL ON POWER UP FOR TAKEOFF. REPEATED THRUST REVERSER LIGHT ON FLIGHT ENGINEER PANEL. LOCKED OUT REVERSER PER AMM 78-00-00, OPENED MEL 78-12A.Sep 9, 2004 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0401191Actuator · malfunctionedAFTER PUSHBACK, ON ENGINE START NR 1 ENGINE FUEL CONDITION ACTUATOR CIRCUIT BREAKER OPENED. REMOVED AND REPLACED NR 1 FUEL CONDITION ACTUATOR, ALL OPS NORMAL.Sep 9, 2004 · N921FT · Boeing 747283B · Power LeverSDR P5CA0401183Seal · leakingDURING CRUISE, NR 1 ENG OIL QTY GRADUALLY DECREASED, OIL PRESSURE & TEMP NORMAL, CLOSELY MONITERED OIL QTY, WHEN ZERO OIL PRESSURE INDICATED, GAUGE FLUCTUATED & OIL PRESSURE LIGHT FLICKERED, SHUTDOWN ENGINE, ENGINE FAILURE / SHUTDOWN CHECKLIST ACCOMPLISHED. OAug 28, 2004 · N921FT · Boeing 747283B · Turbine Engine Oil SystemSDR P5CA0401182Line · leakingVIA PHONE PATCH, CREW REPORTS 0 PSI/0 QTY ON NR 1 HYDRAULIC SYSTEM. INSTALLED TEMP FLEX LINE PER MM 20-11-18 & GMM 3-17-1, PLACED ITEM ON COI 921-163. LINE IS LOCATED AFT OF STATION 23600 ON LT SIDE.Aug 27, 2004 · N921FT · Boeing 747283B · Hydraulic System, MainSDR P5CA0401135Clamp · damagedNR 3 ENGINE HIGH STAGE VALVE WILL NOT OPEN AT ALTITUDE WITH THRUST LEVER CLOSED. REPLACED CLAMP ON HIGH STAGE VALVE, OPERATIONAL CHECK & LEAK CHECK OK PER MM 36-11-00.Aug 8, 2004 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR P5CA0401134Light · inoperativeTAT, SAT, IB FLAPS AND P-10 PANEL LIGHTS OUT, ALSO BACKGROUND HSI, CLOCK AND AIR SPEED IND. TRANSFERED TO DMI NR 32904 IAW MEL 33-1.Aug 4, 2004 · N921FT · Boeing 747283B · Instrument PanelSDR P5CA0401132Structure · damagedNR 3 THRUST REVERSER DAMAGED. PERFORMED INTEAM REPAIR IAW SRM 54-07-00. THRUST REVERSER REPAIR PLACARD ON COI NR 162. TRANSFERED TO DMI NR 32887 T/R DEACTIVATED IAW MEL 78-1-2.Jul 31, 2004 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0401124Web · crackedWEB CRACK FOR CENTER WEIGHT, LT OB ELEVATORS OB ACTUATOR ELEV STA 256. REMOVED CRACKED WEB IAW SRM 51-30-02, FABRICATED WEB IAW SRM 55-20-02, INSTALLED WEB IAW SRM 51-30-02.Jul 27, 2004 · N921FT · Boeing 747283B · Elevator StructureSDR P5CA0401128Packing · leakingNR 4 ENGINE IN OIL QTY DROPPED FROM 10.5 GAL BEFORE START TO 8.5 GAL AT IDLE. ON APPROACH INDICATION WENT TO ZERO WITH PRESSURE FLUXUATION B/W 40 AND 25 PSI. REMOVED CSD FOR OIL LEAK, INSTALLED CSD WITH NEW O-RING, OPS CHECK OK, LEAK CHECK OK, OIL PRESSURE NOJul 26, 2004 · N921FT · Boeing 747283B · Turbine Engine Oil SystemSDR P5CA0401121Keelbeam · corrodedCORROSION ON KEELBEAM 2 PLACES, AT BS 1332 AND STA 1319 RT SIZE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW MA NR A5349-01-02, WORK ACCOMPLISH ON T160-468.Jul 12, 2004 · N921FT · Boeing 747283B · Fuselage Main, KeelSDR P5CA0401122Seat Track · corrodedCORROSION UPPER DECK SEAT TRACK BS 540-580 RBL 46.65-WL 310. REMOVED AND REPLACED SEAT TRACK FROM BS 530-660, IAW SRM 53-10-05-53-30-08-53-30-02.Jul 6, 2004 · N921FT · Boeing 747283B · Fuselage, Seat/Cargo Attach Fittings
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