Boeing 747-283B
Service difficulty reports · 267
Newest first. General aviation reporting is voluntary.
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 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.
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
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 P5CA0401294Drain Mast · leakingNR 3 ENGINE HYD LEAK AT DRAIN MAST. FOUND HYD LEAK WITHIN LIMITS PER MM 29-11-00 FIG 601.SDR P5CA0401289Proximity Switch · damagedNOSE LANDING GEAR ALT SQUAT SWITCH FOUND DAMAGED. REPLACED NLG ALT SQUAT SWITCH PER MM 32-60-00.SDR 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.SDR 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.SDR P5CA0401279Indicator · no indicationNR 3 ENGINE HAS NO EPR INDICATION WHEN ACCELERATING. TRANSFERRED TO DMI 33386 PER MEL 77-04-1.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.SDR P5CA0401242Flap · malfunctionedNR 2 LEFT LEADING EDGE WOULD NOT COME UP PNEUMATICALLY, OK ELECTRICALLY. RECYCLED FLAPS PNEUMATICALLY, NO HELP. TRANSFERRED TO DMI 33203.SDR 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.SDR 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.SDR 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. OSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 NOSDR 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.SDR 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.SDR 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.SDR 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.SDR 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 51-30-02SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR P5CA0401057Warning Light · illuminatedN4 T/R ARMED LIGHT ON DURING TAXI. OPENED MEL 78-06-A, CONFIRMED REVERSER STOWED.SDR 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.SDR P5CA0401055Intake · delaminatedNR 2 ENG INBOARD OUTSIDE FAN COWL REQ UPGRAGE, INTERNAL 84 X 20 INCH AREA DELAMINATED BEYOND LOCAL REPAIR. REPLACED COWLING.SDR P5CA0401054Fan Blade · brokenNR 3 ENG HAS ONE FAN BLADE TIP BENT, A SECOND FAN BLADE TIP BLADE FOUND DAMAGED & BROKEN. TWO BLADES REPLACED.SDR P5CA040154Panel · crackedLEFT WING UPPER LEADING EDGE PANEL CRACKED APPROX 18 INCHES BETWEEN STA WBL 470 & WBL 642. REPAIRED PANEL.SDR P5CA0401043Pitot Head · faultyRIGHT AUX PITOT PROBE FAULT LIGHT ON. REMOVED AND REPLACED RIGHT AUX PITOT PROBE GROUND TEST & LEAK CHECK OK.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR P5CA0300971Support · corrodedLBG - WING TO BODY FLAP TORQUE TUBE - LOWER GANG SEAL - SUPPORT BLOCK CORRODED - LEVEL ONE. REPLACED SUPPORT BLOCK PER SRM 51-10-01.SDR 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.SDR 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.SDR P5CA0300973Support Angle · crackedRIGHT I/B MID FLAP O/B L-SUPPORT ANGLE CRACKED 5 INCHES. REPAIR CARRIED OUT IAW SRM 51-40-03.SDR 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.SDR P5CA0300946Skin · delaminatedON MX PREFLIGHT, ON NR 3 ENG INSIDE REVERSER AREA FOUND DELAMINATION. PERFORMED REPAIR WITHIN 10 CYC - COI 921-150 ISSUED.SDR 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.SDR P5CA0300907Valve · malfunctionedNR 3 ENG PYLON VLV WOULD NOT OPEN. REMOVED AND REPLACED PYLON VLV IAW 36-11-00, LEAK CHECK OK.SDR P5CA0300908Connector · dirtyFLAP POS INDICATOR. CLEANED FLAP POS CONNECTOR, OPS CHECK FLAPS PER MM 27-51-00. CHECK OK.SDR 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.SDR P5CA0300827Intercostal · crackedBODY GEAR W/W STA 1394 - STA 1416 1 INCH CRACK INTERCOSTAL AT LONGERON BOX. REPAIR PER SRM 51-40-03 FIG 1.SDR P5CA0300825Access Panel · crackedNR 3 PYLON STRUT ACCESS PANEL 453FL CUTOUT CRACKED. REPAIRED PER SRM 54-34-03 FIG 2.3.
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