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 EIA2004063Stringer · brokenSTR 38R IS BROKEN AT STA 1000 AFT AT BATH TUB FITTING. REMOVED, FABRICATED AND REPLACED STR 38R AT STA 1000 PER SRM 53-10-03, 51-10-02, 51-10-06, 51-30-02 PAGES 2A, 2B, 3, 4, 4A, BAC 149B-147 PAGES 2-3, BAC 149B-131, AND SRM 53-11-04 PAGES 14-15.SDR EIA2004065Fitting · damaged1 EA HOLE HAS BREAKUP CONDITION ON THE STRINGER END FITTING AT BS 2141 LEFT AFT SIDE, STR 21L LOWER. REMOVED AND REPLACED END FITTING AT BS 1241 STR 21L, LOWER. REMOVED AND REPLACED STRINGER NR 21L LOWER BS 1241-1260. REMOVED AND REPLACED INTERCOSTAL WEB ATSDR EIA2004064Stringer · damagedSTA 220-240 RT, STR 14R FOUND TO BE DAMAGED UPON REMOVAL. FABRICATED NEW STRINGER AT STR 14R FROM STA 220-240 RT PER B747 SRM 51-20-01 PAGES 11, 14-21. LOCATED DRILLED STRINGER PER B747 SRM 51-30-05 PAGE 5. ALODINED AND PRIMED STR PER B747 SRM 51-10-02 PAGESDR EIA2004062Fitting · damaged4 EA HOLES HAVE BREAKUP CONDITION ON CENTER OF STRINGER END FITTING NR 23 AT THE BS 1241 AFT RT SIDE. REMOVED AND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGE 8-9 AT BS 1241 STR NR 23R. FABRICATED AND INSTALLED NEW STRINGER NR 23 RT STA 1241 PER B747SDR EIA2004060Skin · gougedPYLON NR 1 I/B SURFACE EXISTING REPAIR MISSING FASTNERS AND IS GOUGED AT AFT LOWER SECTION STA 221.90. REMOVED EXISTING REPAIR DOUBLER FROM PYLON NR 1 LOWER I/B SKIN. FABRICATED AND INSTALLED NEW REPAIR PER B747 SRM 51-30-02 PAGES 8, 9, 38 AND B747 SRM 54-30SDR EIA2004061Fitting · cracked1 EA HOLE HAS BREAKUP CONDITION ON THE CENTER OF STRINGER END FITTING NR 19 BS 1241 LEFT AFT SIDE. REMOVED AND INSTALLED STR END FITTING AT BS 1241 STR 19L. REMOVED AND REPLACED STR NR 19L AT BS 1241-1265. REMOVED AND REPLACED WEB AT BS 1241-1260 STR NR 19LSDR EIA2004059Fitting · damaged1 EA HOLE HAS BREAKUP CONDITION ON CENTER OF STRINGER END FITTING NR 21L AT BS 1241 AFT LT SIDE UPPER. REMOVED AND INSTALLED NEW END FITTING PER B747 51-30-02 PAGES 8-9 AT BS 1241 STR 21L. FABRICATED AND INSTALLED NEW STR NR 21L AT BS 1241-1265 PER B747 SRM SDR EIA2004058Fitting · damaged5 EA HOLES HAVE BREAK-UP CONDITION ON CENTER OF STRINGER END FITTING NR 23 AT THE END OF BS 1241 AFT 4H SIDE. REMOVED AND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGES 8-9 AT BS 1241 STR 23L. FABRICATED AND INSTALLED NEW STR NR 23L AT BS 1241-1265 PESDR EIA2004055Stringer · damagedMAIN DECK STA 160 FRAME STRINGER 6L HAS 1 EA EXISTING ELONGATED HOLE AT STRINGER CLIP LOCATION (APPROX ELONG DIAMETER .350 INCH) STR 6L P/N 65B 14211-13. REMOVED AND REPLACED STR 6L AT STA 140 TO STA 200 PER B747 SRM 51-30-02 PAGES 2,3,5; FIG 7 PAGE 32.SDR EIA2004054Pressure Panel · corrodedFUSELAGE INTERIOR, STA 1420, LBL 10 TO RBL 10 CORROSION ON UPPER SURFACE OF WHEEL WELL PRESSURE DECK WEB. REMOVED DAMAGED AREA. FABRICATED REPAIR FILLER AND DOUBLERS. INSTALLED REPAIR DOUBLERS AND FILLERS PER B747 SRM 53-10-07 FIG 2.SDR EIA2004050Stringer · crackedSTR 23R IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 4. REMOVED AND REINSTALLED END CAP FITSDR EIA2004049Stringer · crackedSTR 25L IS CRACKED AT END CAP FITTING STA 2360, AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 4. REMOVED AND REINSTALLED FOR ACCESS ENDSDR EIA2004053Stringer · crackedSTR 24R IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED HAT SECTION AND STR FILLER PER B747 SRM 53-10-03 FIG 4 PAGES 12-13. REMOVED AND REINSTALLEDSDR EIA2004057Floorbeam · corrodedMAIN DECK FLOORBEAM (UPPER CHORD) AT STA 1720, BETWEEN RBL 11.33 AND RBL 33.99 CHORD IS CORRODED AND HAS AN OVERSIZE HOLE IN THE AFT FLANGE (APPROX 348 INCH) AND ONE OVERSIZED HOLE IN THE FORWARD FLANGE (APPROX 258 INCH). REMOVED DAMAGED FLOORBEAM CHORD AND RSDR EIA2004051Stringer · crackedSTR 25R IS CRACKED AT END CAP FITTING STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 1 PAGES 2A-4. REMOVED AND REINSTALLED OSDR EIA2004048Stringer · crackedSTR 24L IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION, ALODINED, PRIMED AND INSTALLED STR FILLER AND HAD SECTION PER BOEING 747 SRM 51-10-03 FIG 4. REMOVED AND REINSTALLED FOR ACSDR EIA2004056Frame · damagedSTA 300 LOWER LOBE FRAME, 3 EXTRA HOLES WERE DRILLED AND PLUGGED INTO THE 141U1021-21 DOUBLER AND 1 OF THE EXTRA HOLES IS COMMON TO THE 141U1021-9 FRAME AT THE STR 27A 4H CLIP LOCATION. LOCATED AND DRILLED NEW -9 FRAME, DISCREPENT HOLES NOT DRILLED IN NEW FRASDR EIA2004052Stringer · crackedSTR 17L IS CRACKED AT STA 2340. REMOVED FASTENERS FOR ACCESS, PERFORMED HFEC ON SURFACE. CRACKED CONTAINED BY FASTENER HOLES. FABRICATED REPAIR U-CHANNEL. TREATED, PRIMED, AND INSTALLED U-CHANNEL PER B747 SRM 53-10-03 FIG 2, 51-10-01 FIG 7, BSOPM 21-41-00 SDR EIA2004092Splice · crackedSTA 520, STR 12R, STRINGER SPLICE FOUND CRACKED ON REMOVAL. REMOVED CRACKED SPLICE, LOCATED, DRILLED AND INSTALLED NEW SPLICE IAW SRM 51-30-02, PGS 2-3 AND 8-9.SDR EIA2004096Stringer · crackedSTR 27A R FROM BS 320-340 HAS SEVERAL FASTENER HOLES CRACKED. REMOVE DAMAGE, FAB & INSTL NEW STRINGER PER SRM 51-20-01 & 51-30-02.SDR EIA2004097Stringer · damagedSTR 24A BETWEEN BS 300-320 HAS ELONGATED FASTENER HOLES. REMOVE DAMAGE, FAB AND INSTALLED NEW STRINGER PER B747 SRM 51-30-02, 51-20-01, AND 51-30-02.SDR EIA2004095Floorbeam · damagedFLOORBEAM MAIN CABIN BS 1740 RBL 33-99 HAS 4 ELONGATED HOLES COMMON TO SEAT TRACK. REMOVE DAMAGED SECTION OF TEE CHORD BEAM BS 1740 RBL 33.99 & REPLACE WITH NEW SECTION PER B747 SRM 53-10-07 & 51-30-02SDR EIA20041130Pressure Panel · delaminatedMAIN CABIN STA 1380, RBL 75.9, PRESSURE DECK WEB SHOWS EVIDENCE OF DELAMINATION. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR IAW SRM 51-10-07, FIG 251-30-05 PGS 6-9, AND 51-30-02.SDR EIA2004100Floorbeam · crackedWEB BETWEEN FLOORBEAM STA 320-330, STR 12L IS CRACKED. REMOVED DAMAGED WEB, FAB & INSTL PER B747 SRM 51-30-02, 51-10-02, 51-20-01, & SOPM 20-41-02SDR EIA2004101Stringer · crackedSTR 31A CRACKED AT FS 500L. FAB & INSTL NEW STR & SPLICE CHANNELS PER B747 SRM 53-10-03, SHTS 6&7, 51-30-02, PGS 2-3 & 8-9.SDR EIA2004090Skin · corrodedSTR 43L FUS STA 1900, EXISTING REPAIR CORRODED, SKIN OUTBD AND FWD OF REPAIR CORRODED AND BULGING. REPAIRED CORRODED AND BULGING SKIN. REMOVED AND REPLACED CORRODED DOUBLER, PER B747 SRM 53-30-03, FIG 36, PAGES 99-100B, AT FS 1820 STR 48L.SDR EIA2004091Skin · corrodedCORROSION, FS 1960 STR 46R-46L. REMOVED EXTERNAL SKIN DOUBLER, INTERNAL SKIN BONDED DOUBLER AND EXISTING STRUCTURES, INCLUDING SHEAR AND STRINGER TIES, STRINGER SPLICE AT BS 1960 FROM STR 46R-50R. NO CORROSION FOUND ON INTERNAL AND EXTERNAL SKIN FROM STR 46LSDR EIA2004131Pressure Panel · corrodedMAIN CABIN STA 1460, RBL 120 HAS SURFACE CORROSION AT UPPER MAIN WHEEL WELL PRESS WEB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-07, FIG 2, PGS 4-10.SDR EIA2004093Pressure Panel · crackedNOSE WHEEL WELL SIDEWALL, LT SIDE HAS 6 INCH CRACK BETWEEN BS 264.5 AND 270.5, WL 154. REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS. INSTALLED PARTS PER B747 RM 53-10-04, FIG 116.SDR EIA2004102Stringer · crackedSTRINGER 37R AT STA 300R CRACKED AT FASTENER HOLE FOR STRINGER CLIP. REMOVED AND REPLACED DAMAGED STRINGER SECTION PER B747 SRM 51-30-02, PG 32, 51-30-05, PG 5-6, 51-30-02 PG 2-3, AND 51-20-01,PG 11 AND 14-20.SDR EIA2004098Stringer · crackedSTR 28A CRACKED AT BS 500 L. FABRICATED INSTALLED NEW STRINGER SECTION PER B747 SRM 51-30-05, 51-10-02, 51-30-02, AND SOPM 20-41-02.SDR EIA2004103Frame · crackedCRACK IN OUTER RING CHORD, STA 140R AT STR 20. STOP DRILL CRACK STA 140R AT STR 20. NDT VERIFIED NO CRACK CONDITION REMAINING, ALODINED AND PRIMED. REPAIRED PER EO53-747-1730-04 REV A, AND SB 747-53-2355, FIG 5, PG 52 AND 70-2138-05-0715.SDR EIA2004104Structure · crackedCRACK IN OUTER RING CHORD, STA 140R AT STR 22. STOP DRILL CRACK AT STA 140R, STR 22. NDT VERIFIED NO CRACK CONDITION REMAINED. ALODINED & PRIMED. REPAIRED PER EO 53-747-1730-04 REV A & SB 747-53-2355 FIG 5, PG 52, & 70-2138-05-0715SDR EIA2004094Skin · crackedSKIN CRACKS AT BS 335-345, STR 3AL AND 9L. REMOVE DAMAGE, FAB AND INSTALLED REPAIR PER ECRA 470-53-165-2.SDR EIA2004099Floorbeam · corrodedUPPER FLOORBEAM, CORROSION AT STA 720 RBL 84.0 WL 199 UNDER FLOOR BOARD. REMOVED FLOORBEAM AT STA 720 LBL TO RBL 15, PER B747 SRM 53-10-07.SDR EIA2004034Radome · bird strikeJUST AFTER ROTATION AIRCRAFT FLEW THROUGH A FLOCK OF SEAGULLS, IMPACTING SOUNDS HEARD. ALL INSTRUMENT AND ENGINE PARAMETERS NORMAL. NO VISIBLE DAMAGE SEEN FROM CARGO COMPARTMENT. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND RADOME DAMAGE BEYOND SDR EIA2004008Connector · looseEXIT LIGHTS AT L5 AND R5 DOORS INOP DURING "A" CHECK. RESEATED CONNECTOR ON POWER SUPPLY OPS CHECK GOOD.SDR EIA2003171Battery Pack · inoperativeUPPER DECK EMERGENCY LIGHTS ABOVE STAIRS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED IAW B747 MM 33-51-00.SDR EIA2003167Sign · shortedON DECENT TO JFK, FASTEN SEAT BELT SIGN TURNED ON AND OFF SMELLED SMOKE IN COCKPIT AND CIRCUIT BREAKER POPPED. TO REMAIN OPEN TILL FIX IS ACCOMPLISHED.SDR EIA2003126Battery Pack · inoperativePILOT REPORTED EMERGENCY LIGHT OVER CREW DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-07 AND LIGHT ASSY IAW MM 33-51-07. OPS CK GOOD.SDR EIA2003090Line · brokenENGINE NR 1 FIRE LIGHT ILLUMINATED DISCHARGED BOTH FIRE BOTTLES. EGT RED BALL AND NACELLE INDICATES IN RED ZONE SHUT DOWN ENG DUMPED FUEL LANDED JFK. NTSB NOTIFIED. INVESTIGATION IN PROGRESS. NR 4 BEARING OIL PRESSURE LINE BROKE EARLY INDICATION OF CAUSE.SDR EIA2003071Fitting · chafedNR 4R NOSE CARGO DOOR LATCH FITTING ON NR 4 BOLT HOLE LOCATION IS CHAFED. REAMED HOLE NR 4 FROM .530 TO .5605 PER EO 53-747-1633-01 REV-C , FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED.SDR EIA2003070Fitting · chafedNR 4R NOSE CARGO DOOR LATCH FITTING ON NR 3 BOLT HOLE LOCATION IS CHAFED. REAMED HOLE FROM .530 TO .671 PER EO 53-747-1633-01 REV-C, FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED.SDR EIA2003069Structure · corrodedNR 3L NOSE CARGO DOOR LATCH BOLT HOLE NR 2 HAS CORROSION. REAMED HOLE NR 2 FROM 0.623 TO 0.733 PER EO 53-747-1633-01 REV-C, FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED.SDR EIA2003068Structure · corrodedNR 3R NOSE CARGO DOOR LATCH BOLT HOLE NR 3 HAS CORROSION. REAMED HOLE NR 3 FROM 0.621 TO 0.671 PER EO 53-747-1633-01 REV-C, FOUND OUT OF LIMITS. REPAIRED PER ECRA 471-53-222-2 REV-A. ALODINED AND PRIMED.SDR EIA2003066Structure · corrodedRIGHT WING STA 1323 AFT OF NR 23 VARIABLE CAMBER FLAP LOWER T-CHORD CORRODED. REMOVED CORROSION, TRIMMED DAMAGE, INSPECTED AND NDT, FABRICATED REPAIR AND INSTALL PER ECRA 471-57-217-2 REV-A.SDR EIA2003065Skin · corrodedRIGHT UPPER WING UPPER SURFACE OF LOWER SKIN HAS HEAVY CORROSION AT FWD SPAR LOWER CHORD AT WS 1323. REMOVED DAMAGE, INSPECTED AND NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 471-57-217-2 REV-A.SDR EIA2003063Bulkhead · corrodedSTA 1241, LT WHEEL WELL AFT PRESSURE BULKHEAD, PRESSURE ANGLE (65B10821-1) IS CORRODED BEYOND THE SRM ALLOWABLE LIMITS AND REQUIRES REMOVAL AND REPLACEMENT. STA 1241 LT WHEEL WELL AFT PRESSURE BULKHEAD REPAIRED PER ECRA 471-57-212-2 AND ECRA 471-57-214-2.SDR EIA2003062Skin · wornRIGHT FUSELAGE SKIN STA 2280-2416 WORN AT INTERFACE OF VERT STAB. TRIMMED OUT DAMAGE, INSPECTED AND NDT AREA, FABBED AND INSTALLED REPAIR PARTS PER ECRA 471-53-221-2.SDR EIA2003061Skin · wornRIGHT FUSELAGE SKIN FS 2521-2598 WORN AT INTERFACE OF VERT STAB SEAL. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PARTS PER EO 53-747-1670-02 REV-A AND ECRA 471-53-218-2.
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