Boeing 747-228F
Service difficulty reports · 199
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 = '747228F' 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 = '747228F' 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 Q2SA2011121953010Fire Detector · false indicationWHEEL WELL FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED AFTER TAKEOFF AND GEAR UP. EXECUTED QRH MEMORY ITEMS AND DUMPED 139,000 LBS OF FUEL. ACFT RETURNED, VISUALLY VERIFIED NO ACTUAL WHEEL FIRE EXISTED IN ANY POSITION. FALSE WARNING. VISUALLY CHECKED ASDR Q2SA753009Tire · damagedUPON TAKEOFF, TOWER CALLED AND ADVISED THE CREW OF "LEAVING RUBBER ON THE RUNWAY". THE CREW RETURNED TO HAAB AND FOUND TREAD LOSS ON THE NUMBER EIGHT TIRE. IN ADDITION TO THE TIRE DAMAGE THE AIRCRAFT ALSO EXPERIENCED DAMAGE TO PANELS 193 C AND D. NUMBER EIGSDR Q2SA754013Fan · faultyAT 10,000 FEET, ELECTRICAL SMELL AND LIGHT SMOKE ENTERED THE COCKPIT. COMPLETED SMOKE SOURCE IDENTIFICATION PROCEDURE AND ELECTRICAL SYSTEM SMOKE OR FIRE CHECKLIST. THE SMOKE DISSIPATED ALONG WITH THE SMELL AT LANDING. TAXIED CLEAR OF THE RUNWAY TO PARKING SDR Q2SA754012Line · looseNR 1 HYDRAULIC SYSTEM QUANTITY LOW. RE-TORQUED HYDRAULIC LINE FROM THE NR 1 SYSTEM, RIGHT BODY GEAR DOOR LINE PER AMM 20-11-05, PG 401. OPERATIONAL AND LEAK CHECKED NORMAL PER AMM 29-11-00, PG 501. OK FOR SERVICE.SDR Q2SA754011Sequence Valve · crackedAFTER DEPARTURE FROM JNB, NR 1 ENGINE EDP AND ADP LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED. HYDRAULIC PRESSURE AND QUANTITY INDICATED "0". PERFORMED QRH PROCEDURES FOR AFFECTED HYDRAULIC SYSTEM. DECLARED EMERGENCY INBOUND TO ADD.SDR Q2SA754010Fan · vibrationFLIGHT DECK FAN RUMBLES WITH OCCASIONAL BURNED ODOR, SWITCHED OFF AND CIRCUIT BREAKER PULLED. PERFORMED SMOKE INSPECTION REFERENCE AMM 5-51-00, NO DEFECTS NOTED. REMOVED AND REPLACED RECIRCULATING FAN IAW AMM 21-25-06, OPS CHECKED NORMAL IAW 21-25-06.SDR Q2SA753008Fan · faultyFLIGHT DECK FAN IS BURNED UP. SEVERE ELECTRICAL BURNING SMELL WHEN TURNED ON. FOLLOW UP TO ASSIGNED DI 23969 - REMOVED AND REPLACED FLIGHT COMPARTMENT AIR RECIRCULATING FAN IAW B747 AMM 21-25-06, OPS CHECK GOOD. THIS CLEARS DI 23969 - PLACARD REMOVED.SDR Q2SA754009Connector · damagedDURING INITIAL CLIMB, THE FIRE ENGINE WARNING BELL FOR NR1 ENGINE SOUNDED BRIEFLY. AT THAT TIME THE CREW PERFORMED AN INSTRUMENT SCAN AND FOUND THE ENGINE INDICATIONS WERE NORMAL. APPROX 10 SECONDS LATER, THE NACELLE TEMP WENT FULL SCALE AND THE FIRE BELL SOUNSDR Q2SA753007Unknown · smokeSMOKE IN THE COCKPIT ON DESCENT. INSP ACFT IAW AMM 5-51-50. NO TROUBLE FOUND IN AIR-CONDITIONING SYS. REMOVED ALL PANELS IN F/E AREA P6, P7 AND P12 AND LOOKED FOR DAMAGE AND NONE FOUND. OPENED P52 PANEL, SMELL OF SMOKE SEEMS TO BE CENTERED THERE, NO SMOKE ATSDR VGQY2010082900130Frame · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND CRACK INDICATION ON 2 EA HOLES ON FRAME AND 2 EA HOLES ON FWD CHANNEL AT RT BS 820 AT TENSION TIE AREA. CHANNEL CUT OUT AS PER SRM 53-10-11 FIGURE 2 REVISION 117. FRAME CUTOUT AS PER SRM 53-10-04 FIGURE 132 REVISIOSDR VGQY2010082900129Frame · crackedDURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 900, FOUND 01 EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TENSION TIE AND FRAME AT RT BS 900 REPAIR CARRIED OUT REPAIR ON FWD CHANNEL AS PER SRM 53-10-11 REV 117 FIGURE 2.SDR VGQY2010082900128Shear Tie · crackedDURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 860, FOUND 02 HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TENSION TIE AND FRAME AT RT BS 860 CARRIED OUT REPAIR ON FWD 'C' CHANNEL AS PER SRM 53-10-11 REV 117 FIGURE 2.SDR VGQY2010082900126Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE ELONGATED AT BS 380 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE RBL 15. INSURANCE CUT ON FASTENER HOLE CARRIED-OUT PER SB 747-53A2439 REV 2. FINAL HOLE SIZE 0.341". HFEC INSPECTION CARRIED-OUT PER B747 NDTMSDR VGQY2010082900125Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 340 UPPER DECK FLOORBEAM AFT FLANGE LBL 15 AT 6 O'CLOCK BY PLAIN VIEW. INSURANCE CUT ON FASTENER HOLE CARRIED-OUT PER SB 747-53A2439 REV 2. FINAL HOLE SIZE 0.341". HFEC INPECTION SDR VGQY2010082900124Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 340 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE LBL 35 AT 12 O'CLOCK BY PLAIN VIEW. TRIMMED-OUT AND FABRICATED REPAIR FILLER AND STRAP INSTALLED PER SB B747-53A2429 REV 2.SDR VGQY2010081900114Skin · crackedHFEC OPEN HOLE CARRIED OUT AND FOUND CRACK INDICATION 01 EA HOLE AT 6 O'CLOCK DIRECTION BY LOOKING INBD AT FWD UPPER CORNER OF LOWER LOBE OF AFT CARGO DOOR CUTOUT. CRACKED AREA TRIMMED OUT AS PER SRM 53-30-03 FIGURE 62 REVISION 117. HFEC INSPECTION CARRIED OUSDR VGQY2010081700113Frame · crackedCABIN - DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 840, FOUND 01EA HOLE CRACK INDICATION ON FRAME WEB AND DOUBLER STACK UP. FRAME AT RIGHT BS 840 CUT OUT PER SRM 53-10-04 FIGURE 133 REVISION 117. HFEC INSPECTION CARRIED OUT ON CUT OUT AREA & FSDR VGQY2010081700112Channel · crackedCABIN - DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 840, FOUND 01EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL AS PER MARKED. REPAIR CARRIED OUT PER B747 SRM 53-10-11 REV 117 FIGURE 2.SDR VGQY2010081600111Fitting · damagedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 RT LWR CHORD FOUND WITH SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081600110Fitting · damagedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 L LWR CHORD FOUND WITH SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081600108Fitting · damagedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027, LT FWD VERTICAL CHORD FOUND WITH SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081600107Structure · crackedNOSE WHEEL WELL - DURING REMOVAL OF CHORD FOR EAM 4753027 MODIFICATION, RT FWD VERTICAL CHORD FOUND CRACKED. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081600106Fitting · damagedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND RT AFT VERTICAL CHORD SEM. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081400103Fairing · crackedLEFT WING -NR 6 LEADING EDGE V/C FLAP BULLNOSE FAIRING FOUND CRACK AT O/B AREA. REMOVED AND REPLACED PER AMM 27-81-02 REV 143.SDR VGQY2010081400102Support Channel · crackedRIGHT WING KRUEGER FLAP NR 14 LOWER SUPPORT CHANNEL FOUND CRACKED AT O/B AREA. FLAP ASSEMBLY REMOVED AND REPLACED PER AMM 27-81-01 REV 143.SDR VGQY2010081400101Support Channel · crackedRIGHT WING KRUEGER FLAP NR 15 UPPER SUPPORT CHANNEL FOUND CRACKED AT O/B END. REMOVED AND REPLACED PER AMM 27-81-01 REV 143.SDR VGQY2010081400100Web · crackedRIGHT WING VC FLAP NR 23 FOLDING NOSE I/B FITTING SUPPORT AREA WEB FOUND CRACKED. FLAP NR 23 REMOVED AND REPLACED PER AMM 27-81-02 REV 143.SDR VGQY2010081400099Web · crackedRIGHT WING VC FLAP NR 23 FOLDING NOSE O/B FITTING SUPPORT AREA WEB FOUND CRACKED. FLAP ASSEMBLY REMOVED AND REPLACED PER AMM 27-81-01 REV 143.SDR VGQY2010081300098Skin · dentedFUSELAGE AT ABOUT STA 2300 BETWEEN STRINGER 11R TO 12R FOUND DENT. DENT MARK AT FUSELAGE STA 2120 TO STA 2140 TRIMMED-OUT, REPAIR DOUBLER FABRICATED AND INSTALLED PER SRM 53-30-03 REV 117 FIGURE 1. REPAIR REPETITIVE INSPECTION THRESHOLD AT 15,000FC WITH INSDR VGQY2010081300097Skin · dentedFUSELAGE AT ABOUT STRINGER 43L, STA 545 FOUND DENT. DENT MARK AT FUSELAGE STA 545 BETWEEN STA STRINGERS 42L AND 43L TRIMMED-OUT, REPAIR DOUBLER FABRICATED AND INSTALLED AT STA 540-560, STA 42-44L PER SRM 53-30-03 REV 117 FIGURE 1.SDR VGQY10081300097Stringer · dentedFUSELAGE AT ABOUT STRINGER 43L, STA 545 FOUND DENTED.SDR VGQY2010081300096Channel · crackedCABIN - DURING HFEC INSPECTION ON TENSION TIE AND FRAME AT RT BS 800, FOUND 01 EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TRIMMED OUT & FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. CHANNEL INSTALLED PER SRM 51-30-02 REV 117.SDR VGQY2010081300095Channel · crackedCABIN - DURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT RT BS 880, FOUND 01 EA HOLE CRACK INDICATION ON FWD 'C' CHANNEL. TRIMMED OUT & FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. CHANNEL INSTALLED PER SRM 51-30-02 REV 117.SDR VGQY2010081300094Channel · crackedDURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT LT BS 860, FOUND 01 EA HOLE CRACK INDICATION ON FWD CHANNEL. CHANNEL TRIMMED OUT; FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. CHANNEL INSTALLED PER SRM 51-30-02 REV 117.SDR VGQY2010081300093Channel · crackedDURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT LT BS 820, FOUND 01 EA HOLE CRACK INDICATION ON FWD CHANNEL. FWD CHANNEL AT LT BS STA 820 TRIMMED OUT. FABRICATED NEW FWD CHANNEL PER SRM 53-10-11 REV 117, FIGURE 2. NEW CHANNEL INSTALLED PER SRM SDR VGQY2010081300092Frame · crackedCABIN - DURING HFEC OPEN HOLE INSPECTION ON TENSION TIE AND FRAME AT LT BS 820, FOUND 01 EA HOLE CRACK INDICATION ON FRAME WEB AND DOUBLE STACK UP. REPAIR CARRIED OUT AS PER B747 SRM 53-10-11 REV 117 FIGURE 2.SDR VGQY2010081300091Structure · crackedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND RT AFT VERTICAL CHORD FOUND CRACKED. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081300090Structure · corrodedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND LT AFT VERTICAL CHORD AT STA 340 LT CORROSION EXCEEDED LIMITS. COMPLIED WITH EN 1184-10, DISCREPANCIES FOUND WHILE PERFORMING BSB 747-53A2562.SDR VGQY2010081300089Structure · crackedNOSE WHEEL WELL - DURING ACCOMPLISHMENT OF EAM 4753027 FOUND RT UPPER CHORD CRACKED. RT UPPER CHORD FABRICATED PER DWG 65B07941, LT UPPER CHORD REMOVED AND REPLACED PER SRM 51-30-02 REV 117.SDR VGQY2010081300088Structure · corrodedDURING ACCOMPLISHMENT OF NOSE WHEEL WELL MODIFICATION (EAM 4753027) FOUND LT AFT VERTICAL CHORD AT STA 340 CORROSION EXCEEDED LIMITS. LT UPPER CHORD FABRICATED PER BOEING DWG 65B02941, CONTROL NO: P0225289 LT UPPER CHORD REMOVED AND REPLACED PER SRM 51-30-02SDR VGQY2010081300087Skin · damagedAFT CARGO DOOR LWR SKIN EDGE FOUND TRIM-OUT OF ABOUT .5 INCH FROM THE EDGE AT STA 1875 -1880. NEW FILLER AND DOUBLER FABRICATED USING 2024T3-0.12" MATERIAL AND INSTALLED AT AFT CARGO DOOR LOWER SKIN AT STA 1875-1880 PER SRM 52-30-06 REV 117 FIGURE 1.SDR VGQY2010081100077Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 420 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 3 AT 6 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR BOEING UPPER TEE HOLES FOUND CRACKED STA 420 & STA 520.SDR VGQY2010081000075Skin · crackedNR 2 PYLON, PYLON SKIN FOUND CRACK AT PANEL 463AR CUTOUT AREA. NO SRM REPAIR. HFEC INSPECTION CARRIED OUT PER SA NDTPM D6-7170 REV 134 PART 6 51-00-00 FIGURE 23 ON PYLON NR 2 PANEL SKIN 463AR CUTOUT AREA. FOUND NO CRACK EVIDENT.SDR VGQY2010081000074Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE RBL 15 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACK SDR VGQY2010081000073Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE RBL 10 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOOR BEAM UPPER T-CHORD HOLES FOUND CRACSDR VGQY2010081000072Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 15.5 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACSDR VGQY2010081000071Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 10 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACK SDR VGQY2010081000070Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE LBL 5 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOOR BEAM UPPER T-CHORD HOLES FOUND CRACK SDR VGQY2010081000069Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD AFT FLANGE BBL 0 AT 6 AND 12 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER T-CHORD HOLES FOUND CRACK ASDR VGQY2010081000068Floorbeam · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND ONE HOLE WITH CRACK INDICATION AT BS 520 UPPER DECK FLOORBEAM UPPER CHORD FWD FLANGE RBL 22 AT 6 O'CLOCK BY PLAIN VIEW. COMPLIED WITH EN 1191-10, REPAIR FOR UPPER DECK FLOORBEAM UPPER TEE CHORD HOLES FOUND CRACK AT ST
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