Boeing 747-283B

Service difficulty reports · 267

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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 aircraft_model_key = '747283B'
  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 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 FittingsSDR P5CA0401176Stiffener · corrodedSTIFFENER CORRODED ON O/B SIDE ELEV, STA 406-5 LEFT HORIZONTAL STAB. REMOVED CORROSION FOUND OUT OF LIMIT PER SRM 55-20-01. REMOVED AND REPLACED STIFFENER AS PER SRM 51-30-02.Jun 29, 2004 · N921FT · Boeing 747283B · Elevator Miscellaneous StructureSDR P5CA0401175Seat Track · crackedSEAT TRACK CORRODED & CRACKED B/W STA 580-560 LBL 62 UPPER DECK. REMOVED DAMAGE SECTION OF SEAT TRACK FROM STA 530-620 IAW SRM 51-30-08. NEW SECTION OF SEAT TRACK INSTALLED PER SRM 51-40-02, 51-11-25.Jun 29, 2004 · N921FT · Boeing 747283B · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0401125Angle · crackedLT WING IB MID FLAP IB FORE FLAP TRACK WBL535 CUT OUT IS CRACKED AT IB LEADING EDGE RIB. REMOVED CRACKED ANGLE IAW SRM 51-30-02, FABRICATED REPAIRED DOUBLER IAW SRM 51-40-02, FIG 2 TREATED AND PAINTED INST DOUBLER IAW SRM 51-30-02, INST ANGLE IAW SRM 51-30-02Jun 22, 2004 · N921FT · Boeing 747283B · Trailing Edge FlapsSDR P5CA0401127Skin · delaminatedLT IB AILERON DELAMINATED LOWER SIDE WBL500 2 PLACES. REPAIR 2EA DAMAGED AREA WITH FIBER GLASS IAW SRM 51-40-15, APPLIED CONDUCTIVELY COATING, PRIMED AND PAINTED.Jun 18, 2004 · N921FT · Boeing 747283B · AileronsSDR P5CA0401126Skin · erodedLT WING IB FORE FLAP UPPER TRAILING EDGE WBL235 EROSION MIDDLE SECTION. REMOVED DAMAGE, APPLIED FIBERGLASS OVERLAY IAW SRM 51-40-15, APPLIED ANTISTATIC TO REPAIR IAW SRM 51-40-15, PAINTED IAW SRM 51-40-15.Jun 17, 2004 · N921FT · Boeing 747283B · Trailing Edge FlapsSDR P5CA0401123Keelbeam · corrodedRT KEEL BEAM CORROSION FROM BS 1310 TO BS 1342. LT KEEL BEAM CORROSION FROM STA 1310 TO STA 1340. REPAIR IAW POLAR MA NR A5349-01-02.Jun 15, 2004 · N921FT · Boeing 747283B · Fuselage Main, KeelSDR UPS04442380Battery Pack · dischargedINSPECTION TYPE:N/A UPPER DECK SERVICE DOOR RT SIDE DOOR FRAME EMERGENCY LIGHTS INOP. TOP TRIM PANEL REMOVED FOR ACCESS TO BATTERY PACK. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.May 13, 2004 · N523UP · Boeing 747283B · Emergency LightingSDR P5CA0401063Drive Unit · malfunctionedNR 1 L/E FLAP REQUIRES ALTERNATE PROCEDURE TO EXTINGUISH IN TRANSIT LIGHT. R&R NR 1 L/E DRIVE UNIT PER MM 27-81-03.Mar 23, 2004 · N921FT · Boeing 747283B · Leading Edge Slat ActuatorSDR P5CA0401058Transmitter · failedNR 1 ENG WOULD NOT PRODUCE TAKEOFF THRUST OF 1.53 EPR. DROPPED TO 1.45 EPR AT FWD THROTTLE STOP. ABORTED T/O. REPLACED EPR TRANSMITTER PER MM 77-11-02. ENGINE GROUND OPS CHECK OK PER MM 71-00-11 TEST NR 9.Mar 11, 2004 · N921FT · Boeing 747283B · Engine Pressure Ratio (EPR)SDR P5CA0401057Warning Light · illuminatedN4 T/R ARMED LIGHT ON DURING TAXI. OPENED MEL 78-06-A, CONFIRMED REVERSER STOWED.Mar 11, 2004 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0401053Seal · brokenLEFT WING L/E OVERHEAT LIGHT ON. REPLACED BROKEN SEALS ON L/E DUCT INBOARD OF NR 2 ENG AND BY THE NR 3 PDU OPS AND LEAK CHECK OK PER MM 36-11-01 AND 26-18-01.Mar 9, 2004 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR P5CA0401055Intake · delaminatedNR 2 ENG INBOARD OUTSIDE FAN COWL REQ UPGRAGE, INTERNAL 84 X 20 INCH AREA DELAMINATED BEYOND LOCAL REPAIR. REPLACED COWLING.Mar 8, 2004 · N921FT · Boeing 747283B · Engine Air Intake SystemSDR P5CA0401054Fan Blade · brokenNR 3 ENG HAS ONE FAN BLADE TIP BENT, A SECOND FAN BLADE TIP BLADE FOUND DAMAGED & BROKEN. TWO BLADES REPLACED.Mar 8, 2004 · N921FT · Boeing 747283B · Turbine Engine Compressor SectionSDR P5CA040154Panel · crackedLEFT WING UPPER LEADING EDGE PANEL CRACKED APPROX 18 INCHES BETWEEN STA WBL 470 & WBL 642. REPAIRED PANEL.Mar 8, 2004 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0401043Pitot Head · faultyRIGHT AUX PITOT PROBE FAULT LIGHT ON. REMOVED AND REPLACED RIGHT AUX PITOT PROBE GROUND TEST & LEAK CHECK OK.Feb 21, 2004 · N921FT · Boeing 747283B · Pitot/Static SystemSDR P5CA0401040Clamp · failedWHILE IN CLIMB FL 29-30 NR 2 ENG FIRE WARNING ON HANDLE AND BOTH FIRE LOOPS CAME ON. ENG SHUT DOWN AND A/C DIVERTED TO NRT. REMOVED AND REPLACED NOSE COWL ANTI-ICE CLAMP. LEAK CK OK IAW MM 30-21-00.Feb 17, 2004 · N921FT · Boeing 747283B · Air Intake Anti/De-Ice SystemSDR P5CA0300993Fuel Control · leakingON ENG START NR 2 ENGINE ACCELERATED TO HIGH IDLE 75 PERCENT N2. REMOVED AND REPLACED NR 2 ENG FCU AND THE TT2 SENSOR UNIT IAW 73-21-01 AND AMM 73-21-04, OPS CK AND LEAK CHECK SATISFACTORY.Nov 23, 2003 · N921FT · Boeing 747283B · Fuel Control/Turbine EnginesSDR P5CA0300990Indicator · defectiveOUTBOARD T/E FLAPS LEFT SIDE STOPPED AT 4 DEGREES, RT SIDE STOPPED AT 10 DEG. REPLACED FLAP POS INDICATOR, OPS CHECK OK PER MM 27-58-00.Nov 18, 2003 · N921FT · Boeing 747283B · Trailing Flap Position Indicating SystemSDR P5CA0300989Control Unit · malfunctionedLT WING RT REAR ANTI-SKID WARNING LIGHT ILLUMINATED ON P-2 PANEL. REPLACED ANTI-SKID CONTROL UNIT AND TRANSDUCER IAW MM 32-41-00. SYSTEM CHECK GOOD.Nov 16, 2003 · N921FT · Boeing 747283B · Brake Anti-Skid SectionSDR P5CA0300975Bolt · shearedBODY STATION 2360 - (AFT PRESSURE BULKHEAD) TWO SHEARED BOLTS AT STRINGERS 11R & 20R. REPLACED BROKEN BOLTS - DETAILED VISUAL INSPECTION AND TORQUE CHECK REMAINING BOLTS - FOUR BOLTS FOUND BOTTOMED OUT. ADDED WASHERS AND RETORQUED PER SB 747-53A2474.Oct 29, 2003 · N921FT · Boeing 747283B · FastenersSDR P5CA0300971Support · corrodedLBG - WING TO BODY FLAP TORQUE TUBE - LOWER GANG SEAL - SUPPORT BLOCK CORRODED - LEVEL ONE. REPLACED SUPPORT BLOCK PER SRM 51-10-01.Oct 28, 2003 · N921FT · Boeing 747283B · Fuselage Miscellaneous StructureSDR P5CA0300972Panel · crackedRIGHT O/B MID FLAP, I/B LOWER AREA HAS A 12 INCH CRACK IN LOWER PANEL. FIBERGLASS REPAIR CARRIED OUT ON LOWER AREA OF MID FLAP AS PER SRM 51-40-09.Oct 28, 2003 · N921FT · Boeing 747283B · Trailing Edge FlapsSDR P5CA0300970Support · corrodedRBG - WING TO BODY SEAL - HYDRAULIC GANG CLAMP SUPPORT BLOCK CORRODED. REMOVED AND REPLACED SEAL BLOCK SUPPORT BLOCK PER SRM 51-10-01. CORROSION REMOVED WITH SEAL BLOCK. BASIC STRUCTURE NOT CORRODED.Oct 28, 2003 · N921FT · Boeing 747283B · Fuselage Miscellaneous StructureSDR P5CA0300973Support Angle · crackedRIGHT I/B MID FLAP O/B L-SUPPORT ANGLE CRACKED 5 INCHES. REPAIR CARRIED OUT IAW SRM 51-40-03.Oct 28, 2003 · N921FT · Boeing 747283B · Trailing Edge FlapsSDR P5CA0300962Thrust Reverser · deployedNR 2 ENG THRUST REVERSER DEPLOYED ON T/O ROLL AT 80 KTS. NR 2 ENG T/R DEACTIVATED PER DDPG 78-1 AND MM 78-31-00. ACCOMPLISHED HIGH ENERGY STOP HEAT DAMAGE CONDITIONAL INSP PER MM 5-51-10.Oct 8, 2003 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0300946Skin · delaminatedON MX PREFLIGHT, ON NR 3 ENG INSIDE REVERSER AREA FOUND DELAMINATION. PERFORMED REPAIR WITHIN 10 CYC - COI 921-150 ISSUED.Sep 20, 2003 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0300937Hose · chafedON MECHANIC PREFLIGHT FOUND HYD FLUID LEAKING FROM NR 1 ENG. REPAIRED PRESSURE LINE IAW 20-11-05 PERFORMED LEAK CHECK IAW 29-11-00.Sep 6, 2003 · N921FT · Boeing 747283B · Hydraulic System, MainSDR P5CA0300907Valve · malfunctionedNR 3 ENG PYLON VLV WOULD NOT OPEN. REMOVED AND REPLACED PYLON VLV IAW 36-11-00, LEAK CHECK OK.Aug 10, 2003 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR P5CA0300908Connector · dirtyFLAP POS INDICATOR. CLEANED FLAP POS CONNECTOR, OPS CHECK FLAPS PER MM 27-51-00. CHECK OK.Aug 7, 2003 · N921FT · Boeing 747283B · Trailing Flap Position Indicating SystemSDR P5CA0300903Inu · malfunctionedNR 2 INU HAD RED WARNING LIGHT CODE 02-50-42 (NR 3 WAS ALREADY DEFERRED). RE-RACKED NR 2 INU, PERFORMED REALIGNMENT & RESET FAULT CODES AS PER WC M3400-002.Jul 20, 2003 · N921FT · Boeing 747283B · Inertial Guidance SystemSDR P5CA0300827Intercostal · crackedBODY GEAR W/W STA 1394 - STA 1416 1 INCH CRACK INTERCOSTAL AT LONGERON BOX. REPAIR PER SRM 51-40-03 FIG 1.Apr 10, 2003 · N921FT · Boeing 747283B · Fuselage Miscellaneous StructureSDR P5CA0300825Access Panel · crackedNR 3 PYLON STRUT ACCESS PANEL 453FL CUTOUT CRACKED. REPAIRED PER SRM 54-34-03 FIG 2.3.Apr 10, 2003 · N921FT · Boeing 747283B · Nacelle/Pylon, Plate/Skin
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