Boeing 747-273C
Service difficulty reports · 647
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 = '747273C' 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 = '747273C' 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 EIAA2010050Battery Pack · dischargedWITH EMERGENCY LIGHTS IN ON POSITION CREW SERVICE DOOR EMERGENCY LIGHTS DID COME ON, LEFT FWD DOOR OVERHEAD EMERGENCY LIGHTS CAME ON THEN WENT OUT. BOTH ITEMS DEFERRED TO DMI 91 AND 92 PER MEL 33-13 OPT 2. REMOVED AND REPLACED EMGER LIGHT BATTERY PACK REF. 3SDR EIAA2010074Connector · not seatedEMERGENCY LIGHTS WHEN IN ARMED POSITION ILLUM. RIGHT OVERHEAD LIGHT IN AFT FLT DECK & UPPER DECK CEILING LIGHT NEAR CREW SERVICE DOOR. RE-SEATED SWITCH CONTROL PANEL CONNECTOR ON P5. OPS CHECK NORMAL REF MM 33-51-00.SDR EIAA2010051Doubler · crackedNR 3 PYLON INBOARD SIDE NAC STA 252 APPROX 22 INCHES ABOVE SKIRT REPAIR DOUBLER HAS CRACK. REMOVED DAMAGE, NDT AREA FABBED REPAIR AND INSTALLED PER ECRA 470-54-309-2.SDR EIAA2010047Skin · bentBS 426 STR. 37R HAS A STR. FLANGE TO SKIN BENT. REMOVED DAMAGED AND FABRICATED REPAIR IAW SRM 51-40-3, PG 1-6.SDR EIAA2010048ACartridge · false activationDURING POST FLIGHT EMERGENCY LIGHT SWITCH TESTED TO ON, THEN BACK TO ARMED EMERGENCY LIGHTS STAYED ILLUMINATED. SYS OP'S CHECKED UPPER DECK CREW ESCAPE DOOR LIGHTS AND ONLY ONE DOOR STAYED ILLUMINATED ALL OTHER LIGHTS NORMAL ITEM DEFERRED TO DMI 350. CORRECTSDR EIAA2010048Light · malfunctionedDURING POST FLIGHT EMERGENCY LIGHT SWITCH TESTED TO ON, THEN BACK TO ARMED EMERGENCY LIGHTS STAYED ILLUMINATED. SYS OP'S CHECKED UPPER DECK CREW ESCAPE DOOR LIGHTS AND ONLY ONE DOOR STAYED ILLUMINATED ALL OTHER LIGHTS NORMAL ITEM DEFFERED TO DMI.SDR EIAA2010073Light · intermittentEMERGENCY LIGHT IN LIGHT ASSY OVER UPPER DECK STAIRWELL FLICKERED ON AND OFF WITH SWITCH IN ARM POSITION. REMOVED AND REPLACED EMERGENCY LIGHT OVER UPPER DECK STAIRWELL REF MM 33-51-07 SYSTEM OPS CHECKED NORMAL.SDR EIAA2010072Connector · not seatedDURING CRUISE, FLT EMERGENCY EXIT LIGHTS CAME ON. EMERGENCY LIGHTS SWITCH WAS IN ARMED POSITION. THERE WAS NO LOSS OF ECS PC POWER. RE-SEATED SWITCH CONTROL PANEL CONNECTOR ON P5. OPS CHECKED NORMAL PER AMM 33-51-00.SDR EIAA2010071Wire · damagedON SECURING KSUU, EMERGENCY LIGHTS REMAINED OFF WITH EMERGENCY LIGHT SWITCH SELECTED TO ON. REPAIRED WIRES L5155, L5156 AND L5157 PER WDM 33-51-00 AND SWPM 20-60-12. OPS CHECK GOOD PER MM 33-51-00.SDR EIAA2010060Socket · damagedEMERGENCY LIGHTS STAY ON IN ARMED POSITION. FOUND SOCKET FOR CONNECTOR TO EMERGENCY LIGHT MODULE PIN 13 (GROUND) WITH NUMEROUS BROKEN STRANDS. RE-PINNED PER SWPM 20-60-00 AND WDM 33-51-11. SYSTEM OP'S CHECK NORMAL PER AMM 33-51-00.SDR EIAA2010046Skin · dentedEXTERNAL SKIN DENT AT BS 380-400 STRINGER 34R TO 35R. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER PER B747 SRM 53-30-03 PAGE 73.SDR EIAA2010015Structure · corrodedLEFT WING FWD SPAR LOWER CHORD AT F550/1512 HAS CORROSION CHORD TO WEB. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 471-57-272-2.SDR EIAA2010014Skin · damagedLEFT WING LEADING EDGE SPAR AT F550/1512 HAS EXFOLIATION LIFTING UPPER SKIN. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 471-57-272-2.SDR EIAA200900132Engine · malfunctionedNR 3 ENGINE SURGE/STALL AT MAX TAKEOFF POWER. EGT EXCEEDANCE 1088 DEG CELSIUS. REMOVED AND REPLACED NR 3 ENGINE PER WORKCARDS F7201, F7204, F7207, F7209. OPS & LEAK CHECK GOOD.SDR EIAA200900115Casting · damagedNUMBER 6 SPOILER CASTING ON FALSE SPAR DAMAGED FROM ACTUATOR IMPACT. REMOVED AND REPLACED CASTING FITTING PER B747 SRM 51-30-02 PG 6-8 AND ECRA 471-57-271-2.SDR EIAA20090088Actuator · malfunctionedDURING DIVERSION TO JFK AT 15000FT SMOKE AND FUMES DEVELOPED IN THE COCKPIT. ACCOMPLISHED A/C SMOKE ABNORMAL C/L. SMOKE DISSIPATED AFTER CLOSING NR 4 ENGINE BLEED VALVE. REMOVED AND REPLACED EVC ACTUATOR AND FCU. OPERATIONAL CHECKS GOOD. ALL FOLLOW-ON MAINTESDR EIAA200900086A/C Pack · odorLIGHT SMOKE AND OILY SMELLING FUMES IN COCKPIT ON TAKE-OFF. SMOKE DISSAPETED AFTER CLIMB POOWER SET. REMOVED AND REPLACED EVC, CONDUCTED WET BLEED CK AND EVC TRIM ADJUSTMENT PER 71-00-00 OPS. CK. NORMAL. OPS RAN AIR-CONDITIONING SMOKE CHECKLIST AND DETERMINEDSDR EIAA20090059SUPAcm · defectiveNR 1 PACK PRODUCING ODOR OF TURBINE OIL. REPLACED NR 1 ACM PER MM 21-51-04 AND RESET NR 1 PACK VALVE PER DDPG AND MM 21-51-00.SDR EIAA20090059A/C Pack · odorNR 1 PACK PRODUCING ODOR OF TURBINE OIL.SDR EIAA20090057SUPCoalescer Bag · contaminatedDURING HIGH POWER SETTING (1.45 AND ABOVE) A SWEET ODOR OF OIL ENTERS AIRCRAFT. SIGNS OF OIL LEAK AT NR 1 PACK ACM AND DUCTING, DEACTIVATED NR 1 PACK, DEFERRED AS PER DDPG 21-1-2A. TRANSFERRED TO DMI 008, AS PER MEL 21-1-2C, CAT D, DUE DATE 9-8-9, INSTALLED SDR EIAA20090058Engine · stalledAT FLT LEVEL 280 DURING DESCENT WHEN POWER WAS PARTIALLY REDUCED, NR 2 ENG STALLED. N1 40 PERCENT, EGT 850, TAT-16. ENG WAS SECURED AND RESTARTED IN ACCORDANCE WITH ALL CHECKLIST, INFLIGHT START PERFORMED AND NR 2 ENG RETURNED TO NORMAL OPERATION. PERFORMEDSDR EIAA20090057Acm · leakingDURING HIGH POWER SETTING (1.45 AND ABOVE) A SWEET SMELL OF OIL ENTERS AIRCRAFT. SIGNS OF OIL LEAK AT NR 1 PACK ACM AND DUCTING, DEACTIVATED NR 1 PACK, DEFERRED AS PER DDPG 21-1-2A. TRANSFERRED TO DMI 008, AS PER MEL 21-1-2C, CAT D, DUE DATE 9-8-9, INSTALLEDSDR EIAA20090056Door · dentedREPAIR DENT IN NOSE DOOR BS 190 STR 39. REMOVED DAMAGED STRINGER, RE-CONTOURED SKIN, FABBED AND INSTALLED NEW STRINGER PER B747 SRM 53-10-03 PG 8-10H AND 51-10-02 PG 6-7.SDR EIAA2009054Panel · looseABORTED TAKEOFF DUE TO FIRST OFFICER INSTRUMENT PANEL SLID BACK WHEN TAKEOFF POWER WAS APPLIED. SECURED FIRST OFFICERS P3 INSTRUMENT PANEL.SDR EIAA20090052Light · inoperativeEMERGENCY LIGHT CEILLING OF CREW EXIT DOOR. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECK SATISFACTORY PER MM 33-51-00.SDR EIAA20090024Light · inoperativeUPPER DECK RIGHT SIDE EMERGENCY EXIT LIGHT INOP. ASSY REPLACED PER MM 33-51-06.SDR EIAA20090050SUPLight · inoperativeU/D RT SIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED U/D RT SIDE EMERGENCY LIGHT ASSY AS PER MM 33-51-06.SDR EIAA20090049SUPBattery Pack · inoperativeUPPER DECK CREW EXIT DOOR SLIDE LIGHT INOP. BATTERY REPLACED ON UPPER DECK CREW DOOR AS PER 33-51-00 PG 9. OPS CK OK.SDR EIAA20090050Light · inoperativeU/D RT SIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED U/D RT SIDE EMERGENCY LIGHT ASSY AS PER MM 33-51-06.SDR EIAA20090049Power Supply · inoperativeUPPER DECK CREW EXIT DOOR SLIDE LIGHT INOP. BATTERY REPLACED ON UPPER DECK CREW DOOR AS PER 33-51-00 PG 9. OPS CK OK.SDR EIAA20090048SUPFuel Tank · corrodedCTR FUEL TANK LWR SKIN, LWR SURFACE HAS CORROSION AT BS 1000 LBL 85. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 471-57-267-2.SDR EIAA20090048Fuel Cell · corrodedCTR FUEL TANK LWR SKIN, LWR SURFACE HAS CORROSION AT BS 1000 LBL 85. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 471-57-267-2.SDR EIAA20090047SUPFrame · damagedUPPER DECK FRAME BS 660 HAS 15 MISDRILLED HOLES. REAMED 13 TO ALLOWABLE LIMITS PER B747 SRM 53-10-01 FIG 1. REMOVED, FABBED AND INSTALLED REPLACEMENT CHORD LWR STA 660 RBL 80 PER B747 SRM 51-40-01 FIG 1.SDR EIAA20090047Frame · damagedUPPER DECK FRAME BS 660 HAS 15 MISDRILLED HOLES. REAMED 13 TO ALLOWABLE LIMITS PER B747 SRM 53-10-01 FIG 1. REMOVED, FABBED AND INSTALLED REPLACEMENT CHORD LWR STA 660 RBL 80 PER B747 SRM 51-40-01 FIG 1.SDR EIAA20090046SUPFloorbeam · damagedMAIN DECK FLOORBEAM UPPER CHORD BS 520 LBL 80 HAS 2 DOUBLE DRILLED HOLES. FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-07 FIG 10.SDR EIAA20090045SUPFloorbeam · damagedHOLE IN FLOORBEAM BS 420 UPPER DECK CENTER HAS NO EDGE DISTANCE. FABBED AND INSTALLED REPAIR FLOORBEAM LWR CHORD STA 4020 CENTER PER B747 SRM 51-30-02 PG 8-9.SDR EIAA20090046Floorbeam · damagedMAIN DECK FLOORBEAM UPPER CHORD BS 520 LBL 80 HAS 2 DOUBLE DRILLED HOLES. FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-07 FIG 10.SDR EIAA20090045Floorbeam · damagedHOLE IN FLOORBEAM BS 420 UPPER DECK CENTER HAS NO EDGE DISTANCE. FABBED AND INSTALLED REPAIR FLOORBEAM LWR CHORD STA 4020 CENTER PER B747 SRM 51-30-02 PG 8-9.SDR EIAA20090039SUPSkin · dentedAFT LT EXTERIOR FUSELAGE BS 2470 STR 36 SKIN HAS 2 DENTS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 PG 2A-2I, 53-32-02 PG 16-17.SDR EIAA20090039Skin · dentedAFT LT EXTERIOR FUSELAGE BS 2470 STR 36 SKIN HAS 2 DENTS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 PG 2A-2I, 53-32-02 PG 16-17.SDR EIAA20090044SUPFrame · damagedUPPER DECK FRAME BS 680 RT SIDE HAS MISDRILLED HOLES. REMOVED, FABBED AND INSTALLED LWR CHORD FRAME PLATES AND STIFFENERS AT UPPER DECK FRAME PER SRM 51-40-04 FIG 1.SDR EIAA20090044Frame · damagedUPPER DECK FRAME BS 680 RT SIDE HAS MISDRILLED HOLES. REMOVED, FABBED AND INSTALLED LWR CHORD FRAME PLATES AND STIFFENERS AT UPPER DECK FRAME PER SRM 51-40-04 FIG 1.SDR EIAA20090043SUPFloorbeam · damagedMAIN CABIN BS 820, BL 84, WATER LINE 199 FLOORBEAM UPPER CHORD DOUBLE DRILLED HOLE. FABBED REPAIR AND INSTALLED PER B747 SRM 53-10-07 FIG 10.SDR EIAA20090043Floorbeam · damagedMAIN CABIN BS 820, BL 84, WATER LINE 199 FLOORBEAM UPPER CHORD DOUBLE DRILLED HOLE. FABBED REPAIR AND INSTALLED PER B747 SRM 53-10-07 FIG 10.SDR EIAA20090042SUPFrame · damagedUPPER DECK FRAME BS 460 LEFT OF LADDER CUTOUT HAS 14 MISDRILLED HOLES. REAMED 13 HOLES AT BS 460 WITHIN LIMITS PER SRM 53-10-01 FIG 1 AND REMOVED AND REPLACED LOWER CHORD AT BS 480 LT PER SRM 51-30-02 PG 6-9.SDR EIAA20090042Frame · damagedUPPER DECK FRAMES BS 460 TO 480 LEFT OF LADDER CUTOUT HAS 14 MISDRILLED HOLES. REAMED 13 HOLES AT BS 460 WITHIN LIMITS PER B747 SRM 53-10-01 FIG 1 AND REMOVED AND REPLACED LOWER CHORD AT BS 480 LT PER B747 SRM 51-30-02 PG 6-9.SDR EIAA20090041SUPSkin · dentedEXT FUSELAGE BS 2170, STR 23L DENT ACROSS SKIN LAP 4 INCH LONG. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER SRM 53-30-03 FIG 19.SDR EIAA20090041Stringer · dentedEXT FUSELAGE BS 2170, STR 23L DENT ACROSS SKIN LAP 4 INCH LONG. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER SRM 53-30-03 FIG 19.SDR EIAA20090040SUPStringer · crackedBS 1520-1540, STR 13 L CRACKED. FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-03 FIG 14.SDR EIAA20090040Stringer · crackedBS 1520-1540, STR 13 L CRACKED. FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-03 FIG 14.
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