Boeing 747-230B
Service difficulty reports · 618
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 = '747230B' 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 = '747230B' 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 Q2S2010F00044Mount · crackedWS NR 0844, WC SAI NR 4754020R1. NR 1 PYLON AFT ENGINE MOUNT INBD UPPER CHORD FOUND CRACKED. REPAIR CARRIED OUT IAW EN 1013-10. FORM 8100-9, DATED 19 MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00043Skin · corrodedWS NR 0827, WC NR 53-176-02-01. LOWER FUSELAGE SKIN AT STA 1504, STRINGER 26L FOUND SKIN CORROSION. REPAIR CARRIED OUT IAW EN NR 1010-10. FORM 8100-9, DATED 22, MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00041Bear Strap · corrodedWS NR 0809, WC NR SAI EAO NR 4753028R2. MAIN ENTRY DOOR NR 3 RIGHT CUT OUT AFT TOP SIDE FOUND CORROSION. REPAIR CARRIED OUT IAW EN NR 1019-10. FORM 8100-9, DATED 29, MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00029Frame · corrodedWORKSHEET NR 0823, WORKCARD NR 53-176-02-01. LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 920 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.SDR Q2S2010F00028Frame · corrodedWORKSHEET NR 0824, WORKCARD NR 53-176-02-01. LOWER FUSELAGE RT BODY FAIRING SUPPORT AT STA 920 FOUND CORROSION. REPALCED FRAME ASSY IAW SRM 51-30-02, REV 116.SDR Q2S2010F00024Frame · corrodedWOKSHEET NR 0821, WORKCARD NR 53-176-02-01, LOWER FUSELAGE RT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.SDR Q2S2010F00023Plate · crackedWORKSHEET NR 0810, WORKCARD NR 4753028R2. MAIN DECK, FWD OF MAIN ENTRY DOOR L1 CUT OUT FOUND DOUBLER PLATE CRACKED AT STA 430, STR 23L. REPLACED NEW STRAP IAW SRM 51-30-02, REV 116. PN ON : 141U1050-193.SDR Q2S2010F00022Frame · corrodedWORKSHEET NR 0819, WORKCARD NR 53-176-02-01, LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.SDR Q2S2010F00026Floor Support · crackedWORKSHEET NR 0743. WORKCARD NR 53-520-01-01. FWD CARGO COMPARTMENT AT STA 570, LBL 23 FOUND FLOOR SUPPORT FRAME WEB CRACKED. DAMAGED AREA TRIMMED IAW SRM 51-40-03 FIGURE 1 REVISION 116. FABRICATED REPAIR CHANNEL AND FILLER IAW SRM 51-40-03, FIG 1 REVISION 1SDR Q2S2010F00025Floor Support · crackedWORKSHEET NR 0745, WORKCARD REF NR 53-520-01-01. FWD CARGO COMPARTMENT AT STA 570, LBL 44 FOUND FLOOR SUPPORT FRAME WEB CRACKED. CRACKED FLOOR SUPPORT WEB REMOVED IAW SRM 51-30-02 REV 116. NEW FLOOR SUPPORT WEB FASTENER HOLES TRANSFERRED AND INSTALLED IAW SSDR Q2S2010F00030Frame · crackedWORKSHEET NR 0654, WORKCARD NR 54-410-01-01. PRESSURE BULKHEAD FWD FACE/TOP LT RING FRAME (FACING THE FWD FACE) AT BS 134 FOUND CRACKED AT TOP MOST CORNER. CRCKED RING FRAME REMOVED IAW SRM 51-30-02, REV 116. NEW RING FRAME FABRICATED IAW DWG 65B01700, HEATSDR Q2S2010F00038Spar · corrodedWS NR 0630, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD EXTENSION AT APPROX OLES 1361 FOUND CORROSION. REPAIR CARRIED OUT IAW EN 1020-10. FORM 8100-9, DATED 22 MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00035Spar · corrodedWS NR 0631, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD AT APPROX OLES 1305 FOUND EXFOLIATION. REPAIR CARRIED OUT IAW EN NR 1020-10. FORM 8100-9 DATED 22, MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00027Web · crackedWORKSHEET NR 0620, WORKCARD NR 53-850-01-01. AFT CARGO COMPARTMENT AT STA 1850, RBL 28 FOUND LATERAL GUIDE SUPPORT WEB CRACKED. CRACKED SUPPORT WEB REMOVED IAW SRM 51-30-02 REV 116. NEW SUPPORT WEB FABRICATED IAW DWD 69B03257. NEW FABRICATED SUPPORT WEB HESDR Q2S2010F00020Strap · corrodedWORKSHEET NR 0628, WORKCARD 57-830-01-01. LT WING L/E FRONT SPAR UPPER CHORD STRAP AT APPROX OLES 1481 FOUND CORROSION. CORRODED STRAP REPLACED IAW SRM 51-30-02 REV 116. PN ON: 65B016877.SDR Q2S2010F00040Pressure Panel · crackedWS NR 0437, WC NR 53-842-01-01. LT BODY LANDING GEAR WHEEL WELL AT ABOUT STA 1480 ABOVE ANTI-SKID VALVE MODULE FOUND PRESSURE DECK WEB CRACKED. REPAIR CARRIED OUT IAW EN NR 1011-10, FORM 8100-9, DATED 22 MARCH 2010 ISSUED FOR THE REPAIRED.SDR Q2S2010F00021Mount · corrodedWORKSHEET NR 0435, WORKCARD NR 71-012-01-03, ENGINE NR 3 AFT UPPER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT UPPER MOUNT IAW AMM 71-21-03, REV 142. PN ON: 65B94349-1, SN ON: SA-982.SDR Q2S2010F00019Mount · corrodedENGINE NR 3 AFT LOWER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT LOWER MOUNT IAW AMM 71-21-04, REV 142. PN ON: 65B94350-5, SN ON: P181R.SDR Q2S2010F00032Floor Support · crackedWORKSHEET NR 0292, WORKCARD NR 53-550-02-01. AFT CARGO COMPARTMENT, LT NR 3 PDU SUPPORT WEB AT STATION 1600 TO 1620, LBL 44 FOUND CRACKED. CRACKED FLOOR SUPPORT WEB, REMOVED IAW SRM 51-30-02 REV 116. NEW FLOOR SUPPORT WEB FASTENER HOLES TRANSFERRED AND INSTSDR Q2S2010F00031Skin · damagedWORKSHEET NR 0127, WORKCARD NR SAI RNR 4753078. FUSELAGE-CURRENTLY 02 EXISTING DOUBLERS FOUND SIDE BY SIDE AT BS 520 TO 550, STRINGER 34R TO 36R. REPAIR CARRIED OUT IAW SASCO EN 1012-10. FORM 8100-9, DATED 18 MARCH 2010.SDR Q2S2010F00037Hinge · crackedWS NR 0066, WC NR 57-530-01-01. LT WING NR 6 GROUND SPOILER LOWER SURFACE FOUND CRACKED AT INBD OF ACTUATOR LUG HINGE ALONG FASTENERS. LT WING NR 6 GROUND SPOILER REPLACED IAW AMM 27-61-01, REV 142. PN 65B023101. SN 001395.SDR EIAA2010006Wire · burnedAUTO PRESS CONTROL A/C CIRCUIT BREAKER TRIP, LEF OUT FLOW VALVE ON DMI. FOUND A LARGE BUNDLE OF WIRES SEVERELY DAMAGED (APPROXIMATELY 20-30) AT STA 2020-2040, ABOVE BULK CARGO BAY. REPAIRED WIRE BUNDLE TO LT OUTFLOW VALVE PER AMM 20 STANDARD WIRE PRACTICE, 3SDR EIAA2010003Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED BS 545 STR 35R - 36R. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 PG 2A-2I DETAIL III.SDR EIAA200900129Mec · malfunctionedREJECTED TAKEOFF, NR 4 ENGINE DID NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED MEC IAW 73-21-01. REMOVED AND REPLACED USV FEEDBACK CABLE IAW MM 75-31-03. REMOVED AND REPLACED USV ACTUATORS IAW MM 73-31-02. REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01. OSDR EIAA200900128Indicator · defectiveON CLIMBOUT WHEN RETRACTING FLAPS, INBOARD FLAPS STOPPED AT 2 PERCENT. WHEN ALTERNATE RETRACT WAS ATTEMPTED LJ INBOARD FLAPS DID NOT MOVE AND RESULTED IN AN ASYMMETRIC LOCKOUT. FLAPS DISCREPANCY RECTIFIED WITH NEW INDICATOR.SDR EIAA200900126Pressure Switch · malfunctionedDURING CRUISE APPROX 7 HOURS INTO FLIGHT NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED FLASHING. RETARDED NR 2 THRUST LEVER, LIGHT CONTINUED TO FLASH. ACCOMPLISHED INFLIGHT ENGINE FAILURE AND SHUTDOWN PROCEDURE. FILTER BYPASS LIGHT REMAINED ON STEADY AFTESDR Q2SA760001Flex Duct · crackedON TAKEOFF CLIMBOUT OF EBLG ENGINE FIRE WARNING CAME ON FOR ENGINE NR 2, CREW ELECTED TO SHUTDOWN ENGINE NR 2, DUMPED 77,000 LBS OF FUEL, RETURNED TO AND LANDED SAFELY AT EBLG. AFTER LANDING MAINTENANCE CREW IN EBLG INSPECTED ENGINE NR 2 AND FOUND A CRACKED PSDR EIAA200900114Battery Pack · failedUPPER DECK EMERGENCY LIGHT BETWEEN LAV INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL ON GROUND, REF MM 33-51-50 PAGE 201.SDR EIAA200900113Battery Pack · failedUPPER DECK LEFT EXIT DOOR EMERGENCY SILL LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LT UPPER DECK SILL DOOR BATTERY PACK. OPS CHECK NORMAL ON GROUND. REF MM 31-51-50 PAGE 201.SDR EIAA200900109Light · inoperativeEMERGENCY LIGHT OVER STAIRS INOP. DEFERRED PER MEL 33-13, TRANSFERRED TO DMI 979. REPOSITIONED LT UPPER DECK EMERGENCY EXIT SILL LIGHT RETAINING CLIP PER MM 33-13-00, OPS CHECK GOOD.SDR EIAA200900108Light · inoperativeLEFT UPPER DECK EMERGENCY EXIT SILL LIGHT INOP. DEFERRED PER MEL 33-13 DMI 977 ENTERED. REPOSITIONED LT UPPER DECK EMERGENCY EXIT SILL LIGHT RETAINING CLIP PER MM 33-13-00, OPS CHECK GOOD. TOTAL TIME - 91073.5 TOTAL CYCLES 16390SDR EIAA200900099Tray · damagedRIVETS MISSING AND MISDRILLED HOLE 2EA MAIN DECK ROLLER TRAY SUPPORTS STA 1660 LBL 88 AND 92. REMOVED DAMAGED, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 3.SDR EIAA200900102Panel · crackedNR 2 PYLON EXTERIOR SKIN CRACK O/B SIDE AT ACCESS PANEL 463 BL CUT OUT APPROX NAC STA 318. FABBED AND INSTALLED REPAIR PER ECRA 488-54-033-2.SDR EIAA200900101Skin · deformedNR 2 PYLON ESTERIOR SKIN I/B SIDE AT ACCESS PANEL 463 AR CUTOUT AREA HAS CHIPPED AND DEFORMED EDGES. FABRICATED AND INSTALLED REPAIR PER ECRA 488-54-031-2 REV A.SDR EIAA200900100Tension Tie · damagedTENSION TIE STA. 940 LT AND RT HAS APPROX 30EA OUT OF ROUND HOLES. REMOVED AND REPLACED TENSION TIE BEAM AT BS 940 FROM RBL 99 TO LBL 99 PER SRM 51-30-02 PG. 2-3,4 AND 33-35.SDR EIAA200900098Stringer · damagedBS 193 STR 42 AL LOWER STRINGER LEG DENTED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-03 FIG. 3.SDR EIAA200900097Structure · damagedBS 240 STR. 34L HAS ONE ELONGATED HOLE AND DENT COMMONT TO STR. CLIP. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER SRM 53-10-03 FIG 3 DETAIL II.SDR EIAA200900096Structure · damagedBS 220 STR 28 AR HAS A ELONGATED HOLE COMMON TO STRIP CLIP. REMOVED AND REPLACED STR AT BS 220-240 STR 28 AR PER SRM 51-30-02 PG 2-3 AND7-8SDR EIAA200900095Stringer · damaged2 FASTENERS MISSING RT FUSELAGE, BS 500 STR 15 R AND HOLE ENLOGATED. REMOVED DAMAGE STRINGER, FABBED LOCATED AND INSTALLED REPLACEMENT STR B747 SRM 51-30-02 PG. 23 AND 8-9, 53-10-20 PG 241-243 AND 51-30-05 PG 5-9SDR EIAA200900094Stringer · crackedCRACKED STRINGER AT BS 240 STR 45L. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-03 FIG 3.SDR EIAA200900093Floorbeam · gougedLONGITUDINAL FLOOR BEAM RBL 98 BS 1350 HAS GOUGE AT UPPER CHORD. BLEND OUT OF LIMITS, REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER SRM 53-10-01, 53-30-02 AND 53-10-05SDR EIAA2009000092Frame · damagedFASTENER MISSING AND HOLE ENLOGATED IN RT FUSELAGE FRAME BS 640 STR. 20 R. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER SRM 63-10-04 FIG. 11.SDR EIAA200900091Frame · misrepairedMAIN DECK FRAME REPAIR INCORRECT, BS 320 STR 15L. REMOVED OLD REPAIR, FABBED AND INSTASLL NEW REPAIR PER B747 SRM 51-30-02, 53-10-20 FIG 25 AND 51-40-03 FIG 3 SHT. 1-4SDR EIAA20090090Floorbeam · damagedBS 1660 RBL 89 FLOOR BOARD HOLE ON FLOORBEAM FALLS NEXT TO A RIVET AND EDGE OF CARGO RAIL SUPPORT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER SRM 51-40-04 FIG. 3.SDR EIAA20090089Floorbeam · damagedMAIN DECK FLOORBEAM BS 1700 BL 0 DRILL STRUT NEXT TO FASTENER HOLE. REMOVED DAMAGE, FABRICATED REPAIR STRAP AND FILLER AND STIFFENER PER SRM 53-10-07 FIG 2 AND 51-30-02 PG 8-9SDR EIAA20090055Oil System · low pressureDURING CRUISE AT FL 310, NR 4 ENGINE OIL PRESSURE ILLUMINATED. CHECKED OIL QUANTITY GAUGE IT READ ZERO, AND OIL PRESSURE READ 10 PSI. SHUTDOWN ENGINE USING IN-FLIGHT FAILURE AN SHUT DOWN CHECKLIST. WINDMILL FOR 76 MIN, NOTIFY ATC AND DISPATCH, DUMPED FUEL ASDR EIAA20090025Cargo Track · damagedMAIN TRACK CARGO TRACK DAMAGED AT STA 1950 AND 2000, LBL 11.33. REPAIRED PER SRM 53-10-05, FIGURE 14,SDR EIAA20090022ASkin · puncturedFUSELAGE SKIN PUNCTURED BY DE-ICE BOOM DURING DE-ICING. AREA OF DAMAGE APPROX 3.5H X 4.5W X AT BS 1450 BETWEEN LT STR 10 & 11. REPAIRED PER SRM 53-30-03 PG 2H, DETAIL III. SKIN CUT OUT 4.5 X 6 INCHES FINISHED REPAIR DIMENSION 18 X 15.7.SDR EIAA20090037Skin · damagedLIGHTNING STRIKE DAMAGE BETWEEN STA 140 AND 160 AND STR 23R TO 34R. REPAIRED FOR SRM 53-30-03, FIG 3A AND 3B.SDR EIAA20090036Spar · corrodedRT WING REAR SPAR UPPER SURFACE HAS CORROSION FROM WS 565 TO 575. REPAIRED PER 742-EO-53-2848. FAA APPROVAL THROUGH FAA FORM 8100-9 ISSUED BY BOEING.
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