Boeing 757-24APF
Service difficulty reports · 16,046
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 = '75724APF' 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 = '75724APF' 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 IPXA2026070391033Support Bracket · corrodedLEFT MLG WHEEL WELL, ACMP CD/PRESSURE FILTER MODULE SUPPORT BRACKET CRACKED. INSTALLED BRACKET FRAME NEW WITH IAW SRM 51-40-05.SDR IPXA2026070290181Support · corrodedNLG WHEEL WELL CUT-OUT AT BS 324 RT SIDE, GUSSET REINFORCEMENT PLATE IS CRACKED. INSTALLED NEW SUPPORT AT NLG WHEEL WELL CUT-OUT AT BS 324 RT SIDE, IAW SRM 51-40-02-0G.SDR IPXA2026070591072Support Bracket · crackedLEFT MLG WHEEL WELL, FWD CUT-OUT SEAL HAS 3EA RETAINERS CRACKED AT BS 1060. INSTALLED CHANNEL AND SUPPORT BRACKET AT LT MLG WHEEL WELL, FWD CUT-OUT SEAL HAS 3EA RETAINERS CRACKED AT BS 1060 IAW SRM 51-40-02-0G.SDR IPXA2026070693040Angle · corrodedRIGHT WTB BS 1300 WTB SUPPORT BRACKET AT LWR SIDE IS CRACKED. INSTALLED ANGLE AT RT WTB BS 1300 IAW SRM 51-470-02-0G.SDR IPXA2026070782144Seal · tornLH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL TORN. REPAIRED LH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL IAW AMM 52-09-00-308-001.SDR IPXA2026062791765Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 24. INSTALLED NUT PLATE STRAP ASSY ON AFT CARGO COMPARTMENT. DECK PLATE FLOOR STRUCTURE APPROX AT 1715, LBL 24. IAW SRM 51-40SDR IPXA2026062791791Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 36. INSTALLED NUT PLATE STRAP ASSY ON AFT OF BULK CARGO COMPARMENT DECK PLATE FLOOR STRUCTURE APPROX AT BS 1715. LBL 36. IAW SSDR IPXA2026062982144Seal · tornLH FWD UPPER FUSELAGE CREW DOOR CUTOUT AFT EDGE BULB SEAL TORN.SDR IPXA2026062791739Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, LBL 12. INSTALLED NUT PLATE STRAP ASSY ON AFT BULK CARGO BAY DECK PLATE FLOOR STRUCTURE APPROX AT BS 1715.LBL 12 IAW SRM 51-40-02-OG-0.SDR IPXA2026062282121Latch · wornCREW ENTRANCE DOOR FWD EDGE UPPER AND LOWER LATCHES BARE METAL EXPOSED.SDR IPXA2026062282132Latch · gougedLEFT UPPER FWD FUSELAGE CREW ENTRANCE DOOR FWD EDGE UPPER LATCH GOUGED AT INNER SIDE.SDR IPXA2026071878612Floor Support · dentedAFT CARGO COMPARTMENT FLOOR STRINGER HAS 2 EA DENTS, APPROX BTW BS 1240 AND BS 1260, LBL 7.55, INSTALLED NEW FLOOR STRINGER AT CARGO COMPARTMENT LBL 7.55 AND BETWEEN BS 1200 TO BS 1340 IAW SRM 51-40-02-0G-0.SDR IPXA2026070271202Retainer · corrodedRIGHT MLG WW, AT AFT OTBD DOOR-CUTOUT, UPON THE REMOVAL OF BULB SEAL, FOUND THE RETAINER WITH CORROSION END TO END. REMOVED DAMAGED SEAL RETAINER AT AFT OTBD DOOR-CUTOUT UPON IAW SRM 51-40-02-0G-0, REQUEST FABRICATE SEAL RETAINER. INSTALLED CHANNEL SESDR IPXA2026063078648Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER HAS CORROSION AT NUT PLATE BOTTOM AREA, APPROX AT BS 1200, LBL 2.90. REMOVED CORROSION AT AFT CARGO COMP. FLOOR STRINGER AT NUT PLATE AREA UPPER AND LOWER SIDE AT APPROX BS 1200 LBL 2.90. INSTALLED NEW FLOOR STRINGER AT AFSDR IPXA2026062778873Sidewall Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS, APPROX BTW BS 1410 AND BS 1530, LBL 16.10 THRU LBL 25, REMOVED CORROSION AT AFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL FROM BETWEEN BS 1495 BS 1530 L/H IAW SRM 51-10-02-0GSDR IPXA2026062578498Bracket · corrodedRIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. REMOVED BRACHET (1EA) AND ATTACHED NUTPLATES FOR ACCESS AT RT WING TO BODY OVER WING IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED ANGLE AT RT WING TO BODY OVER WING IAW SRM 51-40-05-0G-0 OK TO INSTALL SDR IPXA2026062578491Bracket · corrodedRIGHT WING TO BODY OVER WING BRACKET HAS SIGNS OF CORROSION. REMOVED BRACKET (1EA) AND ATTACHED NUTPLATES FOR ACCESS AT RT WING TO BODY OVER IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED ANGLE AT RT WING TO BODY OVER WING IAW SRM 51-40-05-0G-0 OK TO INSTALL ANGLESDR IPXA2026081558961Skin · corrodedUPON REMOVAL OF THE LT HORIZONTAL STAB UPPER SLIDING FAIRING FOUND CORRODED ON THE HORIZONTAL STAB UPPER SKIN ALONG RIB 3 BTWN FRONT & REAR SPAR. REMOVED THE CORROSION AT LT HORIZONTAL STAB UPPER SURFACE SKIN AT HSS 81.965 BTWN FRONT SPAR TO REAR SPAR IAW SRSDR IPXA2026063066478Floor Support · corrodedAFT CARGO RH SIDE OTBD FLOOR STRINGER UPPER SURFACE HAS CORROSION STA 1510. INSTALLED REPAIR CHANNEL AT AFT CARGO RT SIDE OTBD FLOOR STRINGER AT BS 1510, RBL 10.45 IAW SRM 53-00-53-2R-1, REPAIR 1, PARAG 4, DETAIL XII AND SRM 51-40-02-0G-0.SDR IPXA2026062358961Fairing · corrodedUPON REMOVAL OF THE LT HORIZONAL STAB UPPER SLIDING FAIRING FOUND CORROSION ON THE HORIZONTAL STAB UPPER SKIN ALONG RIB 3 BETWEEN THE FRONT AND REAR SPAR (CT-A).SDR IPXA2026082353773Angle · crackedLOWER MID FUSELAGE, RT SIDE ANGLE, JUST OTBD OF KEEL BEAM & BS 1180, RBL 11, HAS A CRACK. INSTALLED REPLACEMENT ANGLE IAW SRM 51-40-02-0G-0.SDR IPXA2026070154082Isolation Mount · crackedCOCKPIT CEILING ABOVE OVERHEAD PANEL ISOLATOR BRACKET CRACKED. REMOVED DAMAGED BRACKET AT COCKPIT CEILING ABOVE OVERHEAD PANEL BS 297 IAW SRM 51-40-02-0G-0 PAR 4. INSTALLED PANEL 232N1642-4 AT COCKPIT CEILING ABOVE OVERHEAD IAW SRM 51-40-02-0G-0.SDR IPXA2026062754538Pad · corrodedNR 1 ENGINE O/B CORE COWL T/E RUB PAD, 3RD FROM BOTTOM, HAS AREA OF CORROSION. INSTALEED SERVICEABLE PART AT NR 1 ENGINE OTBD CORE COWL T/E STOP PAD, 3RD FROM BOTTOM IAW SRM 51-40-02-0G-0.SDR IPXA2026081327919Inlet · corroded*** SUPPLEMENTAL SDR *** HORZ STAB COMPT. APU INLET SURROUND STRUCTURE ANGLE IS CORRODED BETWN STA. 1787.45 TO 1825 STGR S-6R (059-07) ATA: 53-80 SKILL: STR APU INLET SURROUNDIN STRUCTURE FROM STA 1787.45-1825 WILL BE REPAIR ON LINE # 711 T3F18E0090LLM. NO FUTSDR IPXA2026071737767Bracket · brokenIAW TASK CARD T3F18E004V6MO LINE 267 STEP 10, LEFT STRUT STA 149.5 BRACKET WAS INSPECTED AND FOUND BROKEN, FLL-050, INSTALLED FRAME ANGLE AT #1 PYLON UPPER SIDE IAW B757-200PF SRM 51-40-02-0G-0SDR IPXA2026071426239Attach Angle · wornVERTICAL STAB TRAILING EDGE PANEL 324AL LOWER AFT CORNER SUPPORT STRUCTURE SECTION MISSING AND FUSELAGE ATTACH ANGLE WORN THIN IN SEVERAL AREAS. DAMAGED WELL MARKED RL004. REMOVED 1EA DAMAGED ANGLE FIN FAIRING AT VERTICAL STABILIZER TRAILING EDGE PANEL 324AL LSDR IPXA2026063033532Skin · corrodedLEFT WING INBD FLAP HAS CORROSION AT T/E OTBD UPPER SURFACE.SDR IPXA2026070724890Splice Plate · corrodedRIGHT ELEVATOR T/E UPPER AND LOWER SPICE PLATES BETWEEN TIP AND CONDUCTOR FRAME HAVE CORROSION. INSTALLED NEW UPPER CONDUCTIVE FRAME, LOWER CONDUCTIVE FRAME, UPPER SPLICE PLATE, LOWER SPLICE FRAME AND STATIC WICK BASE ASSY AT RT ELEVATOR T/E IAW SRM 51-40-02-SDR IPXA2026062431723Cover · corrodedFUSELAGE INTERIOR CENTER SECTION FLOOR PANEL 241XAF PLATE SUPPORT FLOOR PANEL HAS CORROSION, INSTALLED FLOOR SUPPORT HAT CHANNEL AND SUPPORT COVER IN MAIN CABIN, INTERIOR WING CENTER SECTION UNDER FLOOR PANEL 241XAF REF B757-200PF-SRM 51-40-02-0G-0.SDR IPXA2026061925530Skin · damagedRIGHT ELEVATOR T/E UPPER AND LOWER SPICE PLATES BETWEEN TIP AND CONDUCTOR FRAME HAVE CORROSION. OKAY TO FABRICATE PER DOCUMENTS ON STEP 1.SDR IPXA2026062032578Skin · damagedAFT LOWER EXTERNAL FUSELAGE SKIN AT SEAM AT STA. 1460 HAS SMALL AREAS OF BUBBLING PAINT, LIGHT CORROSION PRESENT. SRM 53-00-01-1A-1 DETAIL II FIG 101. OK TO TREAT AND PRIME.SDR IPXA2026061936844Gusset · corrodedFOUND CORROSION ON 4EA GUSSETS, BS 1885.20 BETWEEN S25R AND S25L REMOVED FOUR CORRODED GUSSETS AT BS 1885.20 BETWEEN S-25R TO S-25L IAW SRM 51-40-02-0G-0 PAR 4 AND 7. INSTALLED THE NEW GUSSETS AT STA 1885.20 BETWEEN S-25R TO S-25L IAW SRM 51-40-02-0G-0 AND DSDR IPXA2026061936748Strap · corrodedFOUND CORROSION ON FRAME STRAP P/N 148N6613-2 STA 1885.20 S25R TO S25L. INSTALLED 1 EA NEW STRAP IAW SRM 51-40-02-0G-0 AND DWG 148N6613.SDR IPXA2026061827919Angle · corrodedHORZIZONAL STAB COMPT. APU INLET SURROUND STRUCTURE ANGLE IS CORRODED BETWN STA. 1787.45 TO 1825 STGR S-6R (059-07) ATA: 53-80 SKILL: STRSDR IPXA2026071104567Retainer · corrodedLEFT ELEVATOR T/E COUNT FROM OTBD TO INBD NR 2 STATIC WICK BASE HAS CORROSION. REMOVED AND REPLACED NR 2 STATIC WICK BASE ( MOUNTING STATIC DISCHARGER) P/N 16335, BATCH 0004414980 AND WICK DISCHARGER P/N 10-900-25A, BATCH 0004493176 ON SUPPORT PLATE IAW AMM SDR IPXA2026070219049Support Angle · crackedRIGHT AFT WTB PANEL LANDING UPPER SUPPORT ANGLE HAS A CRACK.
REMOVED SUPPORT ANGLE AT RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW SUPPORT ANGLE RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-OG-0.SDR IPXA2026061806583Window · arcedL1 WINDOW ARCING IN LEFT TOP CORNER INSTALLED L1 WINDSHIELD REF MM 56-11€“01-424-015 UP TO AND INCLUDING STEP 3.E.(13). FIRST TORQUE ACCOMPLISHED AT 1400L. COMPLETED SECOND AND THIRD TORQUE AT !900 AND SEALED. CONNECTED SENSORS AND WIRES TO WINDSHIELD AND TORSDR IPXA2026061706583Windshield · arcedL1 WINDOW ARCING IN LEFT TOP CORNER INSTALLED L1 WINDSHIELD REF MM 56-11€“01-424-015 UP TO AND INCLUDING STEP 3.E.(13). FIRST TORQUE ACCOMPLISHED AT 1400L.SDR IPXA2026062300366Door Frame · corrodedAPU INLET DOOR FRAME HAS CORROSION. INSTALLED SUPPORT ANGLES AND ONE STRAP AT BELOW APU INLET DOOR FRAME APPROX BS 1787-1825, STRINGERS 3 - 6R IAW SRM 51-40-02-0G-0.SDR IPXA2026071492921Skin · damagedFWD FUSELAGE BTW BS 540 - 560 AND S-29L TO S-29R HAVE LIGHTNING STRIKES 3 EA, FLL-006, INSTALLED 3 EA 7/32" DIAMETER PROTRUDING RIVETS ON FWD FUSELAGE BETWEEN BS 540-560 AND S-29L-S-29R IAW SRM 53-00-01-2R-6 REPAIR 6, FIGURE 201.SDR IPXA2026061695676Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT SUPPORT ANGLE, NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, BTW BL 0 AND RBL 9.SDR IPXA2026070198178Pan · crackedFLIGHT COMPT RT FIRST OBSERVERS SEAT BACK PAN IS CRACKED. REPLACED FIRST OBSERVERS SEAT IN FLIGHT COMPARTMENT IAW B757 AMM 25-11-01-000-802 AND B757 AMM 25-11-01-402-061.SDR IPXA2026070193398Door · damagedAFT FUSELAGE RT APU DOOR ACCESS 316AL IS BENDED ON FWD CORNER AND HAS SEVERAL GOUGES ALONG OUTER EDGE, FLL-015, INSTALLED 2 EACH REPAIR DOUBLERS AND 2 EACH FILLERS ON R/H APU DOOR LWR SURFACE AT FS 1925.329 AND FS 1946.774 IAW SRM 51-70-13-0G-0 FIG 1 AND SRMSDR IPXA2026063088739Bonding Strap · corrodedRIGHT HORIZONAL STAB OTBD END TO ELEVATOR BONDING STRAP AND BOTH FWD AND AFT ATTACH BRACKETS HAVE CORROSION. RL025 VERIFIED ITEMS IN STEP 7 ARE INSTALLED PER DOCUMENTS.SDR IPXA2026062787236Bonding Jumper · corrodedL/H HORZ STAB OTBD END TO ELEVATOR BONDING STRAP AND BOTH FWD AND AFT ATTACH BRACKETS HAVE CORROSION. INSTALLED ONE ANGLE BRACKET STRAP JUMPER & REINSTALLED ONE BRACKET ATTACH BY ACCESS IAW SRM 51-40-02-0G-0.SDR IPXA2026062794337Support · corrodedAPU COMPARTMENT L/H LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION, ACCOMPLISHED REPAIR PER EO-98077-REQ1 AND STE-SAA EA 757-5330-01-B0762, REV IRSDR IPXA2026062794351Longeron · corrodedAPU COMPARTMENT RT LOWER FWD CORNER OF FUESELAGE SKIN ACCESS DOOR HINGE SUPPORT LONGERON HAS CORROSION. ACCOMPLISHED REPAIR PER EO-98076-REQ1 AND STE-SAA EA 757-5330-01-B0763, REV IRSDR IPXA2026062792720Frame · corrodedRIGHT FWD LOWER FUSELAGE WASTE DISPOSAL ACCESS PANEL 118AR HAS CORROSION ON INNER AND LOWER FRAME. INSTALLED PANEL 118AR IN FWD FUSELAGE LAVATORY DISPOSAL IAW SRM 51-40-02-0G-0.SDR IPXA2026061994597Access Panel · corrodedAFT FUSELAGE INSIDE ACCESS PANEL 313AL STA 1885.20 AND FROM S-25L TO S-25R HAS CORROSION, FLL-030, REMOVED CORRODED CHORD AT BS 1885.20 BETWEEN S-23L TO S-23R IAW SRM 51-40-02-0G-0 PAR. 4 AND 7. REINSTALLED 2 EA BRACKETS, 1 EA FENCE-DRIP AND INSTALLED NEW CHOSDR IPXA2026061785122Fuse · failedWHEN WE PUT THE GEAR DOWN ON APPROAH, WE HAD THE GEAR DOORS EICAS MESSAGE AND DOORS LIGHT IS ON R & R RT MLG EXT/RET HYD FUSES PER AMM 32-32-19. OPS CHECKS AND LEAK CHECKED GOOD.
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