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 EIA2005252Light · inoperativeR5 DOOR FWD SILL EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT AASY AT DOOR R5 IAW 33-51-07, OPS CHECKED GOOD.SDR EIA2005251Cover · missingCEILING EMERGENCY LIGHT AT L5 DOOR MISSING LIGHT COVER. REPLACED LENS COVER IAW MM 33-51-07, OPS CHECKED GOOD.SDR EIA2005163Cover · missingM/D STA 380 & 680 & R5 EMERGENCY LIGHT COVER MISSING. REPLACED COVERS PER B747 33-51-07.SDR EIA2005162Cover · missingR5 DOOR SILL EMERGENCY LIGHT 2 EA COVERS MISSING. REPLACED 2 EA COVERS AND OPS CHECKED GOOD PER B747 MM 33-51-00.SDR EIA2005161Battery · dischargedM/D RIGHT STA 2180 1EA EMERGENCY LIGHT INOP. RECHARGED LIGHT BATTERY AND OPS CHECKED GOOD PER B747 MM 33-51-00.SDR EIA2005165Light · inoperativeL5 DOOR SILL EMERGENCY LIGHT INOP. REPLACED BULB AND OPS CHECKED GOOD PER B747 MM 33-51-50.SDR EIA2005164Battery · dischargedR5 DOOR EMERGENCY LIGHT INOP. RECHARGED BATTERY AND OPS CHECKED PER B747 MM 33-51-50.SDR EIA2005134Bulb · inoperativeR5 AND L5 AND L1 DOOR EMERGENCY EXIT LIGHTS, SILL LIGHTS, AND EXIT SIGNS WILL NOT ILLUMINATE. REMOVED AND REPLACED BULBS, LIGHT ASSY'S AND POWER SUPPLY BATTERY IAW 33-51-00. OPS CK OK.SDR EIA2005132Engine · failedFL 340 IN CRUISE, NO TURBULENCE LOUD BANG WITH YAW TO RIGHT ENG NR 4 N1, N2 EGT PARAMETERS INDICATION EXCEEDENCES (RED) ENGINE FLAMED OUT. SECURED ENG. NO FIRE WARNING. METAL IN TAILPIPE REMOVED AND REPLACED NR 4 ENGINE IAW F7201/9724001.SDR EIA2005125Connector · looseFOUND NR 5 EMERGENCY EXIT SIGN AT R5 DOOR INOPERATIVE, DMI 962 ISSUED. RECONNECTED CONNECTORS TO WIRING FROM SIGN. R5 DOOR EMERGENCY EXIT SIGN OPS CKS OK IAW MM 33-51-00 PG 501. DMI CLEARED. PLACARD REMOVED.SDR EIA2005124Light · inoperativeDURING INSPECTION, FOUND EMERGENCY LIGHT AT STATION 600 L/S INOPERATIVE. RELAMPED LIGHT ASSEMBLY 600 L/S, OP'S CHECK GOOD IAW MM 33-51-07.SDR EIA2005026Frame · crackedFUSELAGE STA 1000 CHORD IS CRACKED BETWEEN STR 37L-38L NEAR BATHTUB FITTING AT EXTERIOR SIDE UNDER RAM AIR DUCT. REMOVED DAMAGED CHORD FROM STA 1000 BETWEEN STR 37-38 LT AND REPLACED PER B747 SERVICE BULLETIN 747-53A2471 FIG 13 AND EO 53-747-1072-90 REV A PARSDR EIA2005025Stringer · crackedBETWEEN STA 260-280 STRINGER 41 LT CRACKED AT AFT END. REMOVED AND REPLACED STRINGER STA 260-280 NR 41 LT PER B747 SRM 51-30-02 PG 2-9. FABRICATED NEW STRINGER NR 41 LT STA 260-280 PER B747 SRM 51-20-01 PAGE 11-20.SDR EIA2005024Skin · corrodedFUSELAGE BS 1000 LT BETWEEN STR 37 & 40 HAS CORROSION ON SKIN INSIDE OF FWD PIT. REMOVED CORROSION AT STA 1000 STR 39-41 LT PER B747 SRM 53-30-03 FIG 12. CUT OUT LIMIT SKIN AREA PER B747 SRM 53-10-01 FIG 1, NDT CHECKED NO CRACK NOTED FABRICATED INSTALLED REPSDR EIA2005023Floorbeam · crackedBS 420 LBL 43 UPPER DECK FLOORBEAM WEB HAS CRACK AT UPPER T-CHORD AREA. REMOVED DAMAGED SECTION OF WEB AND REPAIRED PER B747 SRM 53-10-07 PG 47-50 FIG II. BONDED WEB AND DOUBLER FOR STA 420 LBL 34-54 PER BAC 5514-5101 BOEING DRAWING 65B10931 SHEET 75 AND B74SDR EIA2005022Skin · damagedSTA 240 AFT OF NOSE CARGO DOOR BOTTOM FUSELAGE SKIN WRINKLED. LOWER SKIN REPAIRED PER ECRA 471-53-246-2.SDR EIA2005021Spar · corrodedRT WING FWD T-CHORD CORRODED AT WSS 1336 FSSO 1349.0 LOWER T-CHORD. REPAIRED RIGHT WING FWD SPAR T-CHORD AT WS 1336 (FSSO 1349.0) LOWER CHORD PER ECRA 471-57-242-2.SDR EIA2005020Frame · crackedCRACK AT LOWER FRAME STR 25R, R5 DOOR STA 2231. INSTALLED NEW LOWER FRAME STA 2231 AT STR 25R PER B747 SRM 51-30-02 PG 8-9.SDR EIA2005019Spar · crackedLEFT WING, FWD SPAR, LWR CHORD HEAVY CORROSION AND CONFIRMED CRACK AT FSSO 1410. REPAIRED LEFT WING, FWD SPAR LOWER CHORD AND LOWER WING SKIN FROM FSSO 1370-1410 PER ECRA 471-57-247-2.SDR EIA2005018Frame · crackedCRACK INDICATION NOTED IN LWR FASTENER HOLES IN LTC-3 FRAME UPPER CLOSURE FITTING DURING OPEN HOLE HFEC INSPECTION. REAMED HOLE INSTALLED FREEZE PLUG IN LOWER HOLE AND INSTALLED FASTENER PER B747 SRM 51-10-08 PGS 1-11, 51-30-09 PGS 1-16, 20, 29, 30 AND BOEINGSDR EIA2005017Skin · delaminatedNR 2 SPOILER LOWER SURFACE SKIN DOUBLER DELAMINATED. COMPOSITE REPAIR MADE TO DELAMINATION ON PANEL EDGE NR 2 SPOILER PER B747 SRM 51-40-06 PG 13.SDR EIA2005016Stringer · crackedBETWEEN STA 300-320 STR 34 RT CRACK AT UPPER SURFACE. REMOVED DAMAGED SECTION BETWEEN STA 280-320 PER B747 SRM 53-10-03 PG 8-10. FABRICATED NEW STRINGER PER B747 SRM 53-10-03 PG 8, 51-30-02, 51-10-02 AND BSOPM 20-41-02 PG 7-9 NDT FOUND NO CRACKS. INSTALLED SDR EIA2005015Frame · crackedCRACK INDICATION NOTED IN 4 EA FASTENER HOLES AT STA 800, STR 16L, FWD INNER FRAME CHORD. REMOVED EXISTING REPAIR PARTS, FABRICATED NEW STRAPS AND INSTALLED REQUIRED EXISTING AND FABRICATED STRAPS PER ECRA 471-53-230-2.SDR EIA2005014Frame · crackedMAIN CABIN INTERIOR, RT MAIN FRAME CRACK AT BS 360, BETWEEN STR 14 & 15. REMOVED AND REPLACED MAIN FRAME AT STA 360 RT MAIN CABIN PER ECRA 471-53-240-2 BETWEEN STR 13A TO 23 B747 SRM 51-30-02 PAGES 2, 3, 8 & 9.SDR EIA2005028Floorbeam · crackedBS 420 UPPER FLOORBEAM TOP CHORD AT RBL 57 AND OUTBOARD HAS NUMEROUS (5) FASTENER HOLES WITH CRACK INDICATIONS (RBL 57.75, 58.25, 63, 67.5, AND 89.5). REMOVED AND REPLACED STA 420 FLOORBEAM UPPER CHORD DUE TO NUMEROUS CRACK INDICATIONS PER SERVICE BULLETIN 74SDR EIA2005013Skin · crackedRIGHT WING EXTERIOR, L/E NOSE IS CRACKED AT FASTENER HOLE 10 INCHES LONG AT WS 200.0. HOT BONDED METAL TO METAL REPAIR MADE TO RT WING L/E NOSE AT WS 200.0 PER ECRA 471-57-241-2 AND 747 SRM 51-40-06 PG 23.SDR EIA2005012Strap · crackedCRACK IN FRAME INNER STRAP AT STA 2231 LT FROM STR 25 TO STR 26 AT L-5 DOOR FWD FRAME. REMOVED STRUCTURE AS REQUIRED. FABRICATED REQUIRED PARTS AND INSTALLED FABRICATED STRAPS ALL PER ECRA 471-53-236-2P AND B747 SRM 53-10-04 PG 689-694.SDR EIA2005008Frame · crackedCRACK INDICATION IN LWR TWO FASTENER HOLES IN RT C-3 FRAME UPPER CLOSURE FITTING. REPAIRED RT C-3 FRAME UPPER CLOSURE FITTING PER ECRA 471-53-243-2.SDR EIA2005011Spar · corrodedRIGHT WING FWD SPAR AT WS 1485 LOWER T-CHORD CORRODED. REPAIRED THE RIGHT WING FWD SPAR WS 1485 PER ECRA 471-57-238-2P.SDR EIA2005010Doubler · damagedREMOVED EXTERNAL DOUBLER REPAIR NR 3 EXTERNAL FUSELAGE BS 2144-2164.5, STR 46R-48R. REMOVED EXTERNAL DOUBLER, FABRICATED REPAIR DOUBLERS AND FILLERS. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER B747 SRM 53-30-03 FIG 19.SDR EIA2005009Light · inoperativeUPPER DECK EMERGENCY LIGHT INOP. REPLACED INOP EMERGENCY LIGHT PER B747 MM 33-51-00.SDR EIA2005007Stringer · crackedSTR 22L CRACKED AT STA 303 UNDERNEATH STRINGER. REPAIRED CRACKED STRINGER AT 22L, STA 303 PER ECRA 471-53-248-2.SDR 200500289Spar · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT HAND WING LOWER FRONT SPAR CHORD. THE MAJOR REPAIR REQUIRED REPLACING 186 INCHES OF THE SPAR CHORD.SDR EIA2004145Structure · corrodedBS 1480 MCD, CORROSION ON WHEEL WELL CHORDS AND STRIP, LBL 98-0 - LBL 57.5, AND LBL 35.0 - RBL 21.0. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2PL.SDR EIA2004144Pressure Panel · corrodedSURFACE CORROSION ON PRESSURE WEB COMMON TO LONGITUDINAL FLOORBEAM MATING SURFACE AT BS 1480, LBL 11.33. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2PL.SDR EIA2004143Structure · corrodedBS 1480, LBL 74.92, TOP OF MLG BOX HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2P-1.SDR EIA2004142Skin · corrodedBS 1200, LBL 98.5, UPPER SKIN CENTER TANK HAS CORROSION. REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-270-2.SDR EIA2004141Skin · corrodedBS 1180 LBL 95-100 CENTER TANK UPPER SKIN HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-270-2.SDR EIA2004140Skin · corrodedSKIN AT BS 1140, LBL 98.58, LBL 110 AT BUTT JOINT OVER MID SPAR HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-269-2.SDR EIA2004139Bulkhead · crackedBS 1241 BULKHEAD CANTED WEB, RBL 30, HAS CRACK AT LOWER CORNER OF AIR DUCT CUTOUT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-177-2 AND B747 SRM 51-10-01.SDR EIA2004138Frame · crackedBS 360 RT STRINGER 15-16 RT, FOUND WEB OF LOWER FRAME CRACKED. FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-267-2.SDR EIA2004137Floorbeam · corrodedBS 540, UPPER DECK FLOORBEAM, UPPER FORWARD SIDE OF CHORD LBL3 THRU LBL6 HAS EXFOLIATING CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CHORD PER B747 SRM 53-30-03, FIGURE 1, ALONG WITH MM 51-30-05 AND 51-20-02.SDR EIA2004132Strap · corrodedUPPER DECK FLOORBEAM STRAP HAS EXFOLIATION CORROSION, STA 420R, 3 INCHES IB FUSELAGE SKIN. REPLACED STRAP IAW SRM 51-30-02, PGS 8-9, 51-30-05, FIG 4, AND 51-30-02, PGS 8-9SDR EIA2004133Skin · corrodedAFT LWR CARGO DOOR, 3RD LWR ACCESS PANEL, INNER SKIN CORRODED. REMOVED DAMAGE AND REPAIRED PER ECRA 470-52-240-2.SDR EIA2004134Support Beam · crackedRT WING STA 665-685, TRAILING EDGE SUPPORT BEAM, LOWER CHORD CRACKED ON FORWARD SIDE. REPAIRED RT WING TRAILING EDGE SUPPORT BEAM, LOWER CHORD BETWEEN WS 665-685, PER ECRA 470-57-227-2, REV A.SDR EIA2004135Web · cracked1.1 INCH CRACK ON NOSE WHEEL WELL BOX WEB, STA. 340, RBL 15, WL 150. REMOVED DAMAGED WEB, FABBED AND INSTALLED REPLACEMENT PARTS IAW ECRA 470-53-207-2SDR EIA2004106Floorbeam · damagedBS 420 FLOORBEAM UPPER DECK, UPPER CHORD FWD FLANGE. HOLE AT RBL 52.0 WAS REAMED TO MAX 0.34 DIAM, WITH CRACK INDICATIONS REMAINING. MUST BE REPAIRED PER SB. REPAIR HOLE BS 420, RBL 52.0 FWD HORIZ FLANGE PER SB 747-53-2439, FIG 9, SHT 1-6SDR EIA2004105Stringer · crackedSTR 41L STA 260-280 FOUND CRACKED DURING INSULATION BUY BACK. R&R STRINGER SECTION 41L @ STA 260-280, PER B747 SRM 51-30-02, PG 2-3 & 8-9SDR EIA2004129Stringer Clip · crackedSTRINGER 23L CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 52-10-03, FIG 4SDR EIA2004066Fitting · damaged4 EA HOLES HAVE BREAKUP CONDITION ON THE CENTER OF STRINGER END FITTING NR 25 BS 1241 RT AFT SIDE. REMOVED AND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGES 8-9, AT BS 1241 STR 25R. FABRICATED AND INSTALLED NEW STR 25R AT BS 1241-1265 PER B747 SRM 5
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