Boeing 757-24APF
Service difficulty reports · 16,054
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 IPXA2024080321068Structure · corrodedMID FUS - WTB STRUCTURE STA 1220 RH SIDE HAS CORROSION.EVALUATED T-CHORD FROM STA 1220 RH TO 1240 RH FOUND EXFOLIATION THEREFORE OUT LIMITS I.A.W SRM 53-00-71-1A-1 DETAIL IX. AND REMOVED T-CHORD I.A.W SRM 51-40-02-0G. RESTORED SURFACE PROTECTION I.A.W. SRM 51-SDR IPXA2024080218851Floor Support · corrodedMAIN CARGO CORROSION UNDER FLOOR PANEL 241XAF AFT AREA. INSTALLED NEW UPPER CHORD IAW B757 SRM 51-40-02.SDR IPXA2024080218877Floor Support · corrodedMAIN CABIN CORROSION UNDER FLOOR PANEL 241XFF AFT AREA.REMOVED 01 NUT DOME IAW SRM 51-40-02-0G, CLEAN AREA AND REMOVED CORROSION IAW SRM 51-10-02, AFTER EVALUATION T-CHORD FOUND TO BE OUT OF LIMITS IAW SRM53-00-51-1A-1 DETAIL III, MEASUREMENTS: ORIGINAL THICKNSDR IPXA2024080318949Tee Fitting · corrodedFAULT: STR Z200, MAIN CABIN CORROSION UNDERFLOOR PANEL 242XDF AFT AREA INSTALLED UPPER CHORD IN MAIN CABIN UNDER FLOOR PANEL 242XDF AFT AREA, IAW 757-200PF SRM 53-00-51-2R-2. REVIEWED.SDR IPXA2024081089013Tee Angle · corrodedWTB STRUCTURE T-CHORD STA 1180 HAS CORROSION FROM RBL 0 TO RBL 60.AFTER FURTHER INVESTIGATION T-CHORD STA 1180 FROM RBL 0 TO RBL 60 FOUND 100% MATERIAL LOSS BY CORROSION THEREFORE IT'S OUT LIMITS IAW B757 SRM 53-00-71-1A-1, AND REMOVED T-CHORD IAW B757 SRM 51-SDR IPXA2024080389031Tee Angle · corrodedFAULT: STR Z100, MID FUS - WTB STRUCTURE T-CHORD FROM STA 1180 TO 1240 RBL 60 HAS CORROSION INSTALLED T-CHORD FROM STA1180 TO 1240 RBL 60, RIVET P/N:BACR15FT6D5C BATCH:004298336, HI-LOK P/N:BACB30NX6K6 BATCH:0004288696, BACB30NX6K4 BATCH:0004286459, WASHER P/NSDR IPXA2024080286954Tee Angle · corrodedFAULT: STR Z100, MID FUS -T-CHORD STA 900 HAS CORROSION AT RBL 10 INSTALLED T-CHORD MID FUS STA 900, IAW B757 SRM 51-40-02 AND SRM 51-70-12. MATERIAL USED: SOLID RIVETS P/N BACR15FT6KE10C BATCH NO: 0004254774, P/N BACB30NX6K6 BATCH NO: 0004288696, P/N BACC30M6SDR IPXA2024080386951Tee Fitting · corrodedFAULT: STR Z100, MID FUS -T-CHORD STA 1037 TO 1060 LH SIDE HAS CORROSION INSTALLED NEW T-CHORD IN STA 1037 TO 1060 LH IAW SRM 51-40-02 RIVET P/N BACR15FT6D7C BTCH: 0004201930 FASTENERS P/N BACB30MY6K5X BTCH: 0004279034 COLLAR P/N: BACC30M6 BTCH: 0004295539, PESDR IPXA2024083060457Skin · corrodedNR 2 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION. DOT 8-006 AND IN RED. COMPLETED REPAIR IAW EO-90940-REQ 1 AND EA 757-5450-27-A3651. REPAIRED #2 I/B SKIN IAW EO-90940 REQ1 & EA 757-5450-27-A3651A REV -. AUDIT COMPLETE.SDR IPXA2024081860457Skin · corrodedNR 2 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION. DOT 8-006 AND IN RED. VERIFIED PARTS. OPENSDR IPXA2024081260701Skin · corrodedNR 1 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION, DOT 8-004. AUDIT COMPLETE. OPENSDR IPXA2024081760669Skin · corrodedNR 1 ENGINE INBD PYLON INNER SKIN AFT OF THE SQUARE PANEL OPENING HAS EXFOLIATION CORROSION. DOT 8-003. ACCOMPLISHMENT OF E.O. AS PER UPS EO-90941-REQ1 AND VT-MAE EA 757-5450-27-A3650, REV. -. WITHOUT ANY DEVIATIONS.SDR IPXA2024081259225Stiffener · corrodedFAULT: STR Z600, RH WING - T/E STIFFENER PN: 113N1184-4 EXFOLIATED.REMOVED STIFFENER EXFOLIATED P/N 113N1184-4 FROM RH WING TRAILING EDGE IAW SRM 51-40-02-0G-0.INSTALLED NEW STIFFENER AND ATTACHING PARTS WITH FASTENERS PN: BACB30NY6K11, BT: 0004279074; BACB30NSDR IPXA2024080359746Tee Angle · corrodedWTB T-CHORD AT STA 1240 HAS CORROSION AT RBL 15. REMOVED CORROSION. AFTER EVALUATION AND LIMIT VERIFICATION THE WTB T-CHORD AT STA 1240 IS EXFOLIATED, OUT OF LIMITS. IAW SRM 53-00-71.RESTORED SURFACE PROTECCION T-CHORD AND SPLICES IAW SRM 51-20-01-0G-0SDR IPXA2024080359714Tee Angle · corrodedWTB T-CHORD BETWEEN STA 1180 TO 1240 RH SIDE HAS CORROSION (RAT AREA) REMOVED AND INSTALLED T-CHORD FROM STA1180 TO STA1240 B757 SRM 51-04-02-0G.SDR IPXA2024080359737Tee Angle · corrodedWTB T-CHORD AT STA 1200 RH SIDE HAS CORROSION AT WL 160.REMOVED T-CHORD AT STA 1200 RH SIDE, WL 160 IAW B757 SRM 51-40-02-0G.INSTALLED NEW T-CHORD AT STA 1200 RH IAW SRM 51-40-02-0G,SDR IPXA2024080159861Latch · inoperativeLOWER DOOR LATCH CAM GOUGED. DOT 59-003.BLENDED OUT GOUGE IAW SRM 51-10-02 ACCOMPLISHED STEP 1 SREO-14721-REQ001, T3F18E004V538.SDR IPXA2024080159841Latch · inoperativeUPPER DOOR LATCH CAM GOUGED. DOT 59-002.BLENDED OUT GOUGE IN UPPER DOOR LATCH IAW SRM 51-10-02, ACCOMPLISHED STEP 1 SREO-14721-REQ001, T3F18E004V50.SDR IPXA2024072259225Stiffener · corrodedRH WING - T/E STIFFENER PN: 113N1184-4 EXFOLIATED REF STEP 2. INSPECTED AND VERIFIED REMOVED STIFFENER EXFOLIATED P/N 113N1184-4 FROM RH WING TRAILING EDGE IAW SRM 51-40-02-0G-0.SDR IPXA2024071859861Latch · gougedZONE 800 LOWER DOOR LATCH CAM GOUGED. DOT 59-003 APPROVED.SDR IPXA2024071859841Latch · gougedSTR ZONE 800 UPPER DOOR LATCH CAM GOUGED. DOT 59-002 APPROVED.SDR IPXA2024071750251Window · leakingWATER DRIPPING FROM WINDOW INTO 02 MASK BETWEEN L1 AND L2. ADJUSTED THE LINK ARM TO PUSH WINDOW OUTBOARD TO MAKE CONTACT WITH SEAL. REF AMM 56-11-02-825-013.SDR IPXA2024072345670Seat Track · corrodedMCD, AT STA 1671, LBL 24.5 SEAT TRACK FLANGE, SHOWS EVIDENCE OF CORROSION. DOT 72-033.REMOVED DAMAGE SEAT TRACK SECTION BETWEEN STA 1640+9.45 IN TO STA 1681.8, LBL 24.5 PER SRM 53-00-52-2R-5, STEP 2.ACCOMPLISHED REPAIR PER 757-200PF SRM REV 120 CHAPTER 53-00-5SDR IPXA2024072631238Doubler · corrodedMCD, AFT DECK AREA (ON DOUBLER REPAIR) AT STA 1681.8 BTW BL 0/RBL 24.75 IS CORRODED. REMOVED AND REPLACED DOUBLER REPAIR ON AFT DECK AREA AT STA 1681.8 BTW BL 0 TO RBL 24.7. IAW B757-200 SRM 51-40-02.SDR IPXA2024072331663Seat Track · corrodedFAULT: STR Z200 MCD, AFT AREA STA. 1681.8 SEAT TRACK LBL 45.5 IS CORRODED. DOT 34-008. INSTALLED SEAT TRACK IN STA 1681.8 LBL 45.5 IAW SRM 53-00-52-2R-5,SRM 51-40-02. REVIEWEDSDR IPXA2024072214234Handle · gouged**SUPPLEMENTAL SDR** FAULT. FOUND GOUGE ON CREW DOOR HANDLE.RESTORED SURFACE IN AREA IAW SRM 51-20-01 AMM 51-21-15 P/N ALONINE 1132 BATCH 004253000 P/N 02-013-8 BATCH 4168824 P/N G6-W2-G2 BATCH 4159202. REVIEWEDSDR IPXA2024071014234Handle · gougedOPEN. FOUND GOUGE ON CREW DOOR HANDLE.SDR IPXA2024072301272Seat Track · corrodedCORROSION FOUND ON SEAT TRACKS AT STA 1680 BL 0.-REMOVED SEAT TRACK DAMAGED SECTION BETWEEN STA 1680-1650 BL PER SRM 53-00-52. ACCOMPLISHED REPAIR PER 757-200PF SRM REV 120 CHAP 53-00-52-2R-7.SDR IPXA2024072202331Frame · dentedDENT ON FRAME IN STA 720 RH BETWEEN STR 23R AND 25R. INSTALLED FRAME REPAIR, IAW SRM 53-00-07-2R-5, DETAIL I, MAT.SDR IPXA2024072695371Tee Angle · corrodedTEE CHORD WITH CORROSION AT BS 900 RT, UNDER PANEL 194AR. INSPECTED & VERIFIED INSTALLATION OF NEW MATERIAL IAW SRM 51-70-12-0G-0 ON STA 900.SDR IPXA2024072494273Transition Panel · corrodedTRANSITION PANEL STA 1440-1520 RH WITH CORROSION. INSTALLED TRANSITION PANEL IAW SRM 51-40-02. INSTALLED PANELS 161BF,161AF IAW SRM 51-40-02. INSTALLED LOWER MBA SYSTEM IAW SRM 51-40-02. REVIEWEDSDR IPXA2024071994561Nut Plate · corrodedFAULT: NUTPLATES UNDER FLOOR PANEL IN STA 1720 WITH CORROSION INSTALLED 1 NUTPLATE IAW B757-200 SRM 51-40-02. NUTPLATE P/N BACN10KE3DCD BTCH 4278069 RIVET P/N NAS1097AD3-8 BTCH 4234826. INSTALLED SHIM PLATE IAW B757-200, SRM 51-40-02 RIVET P/N NAS1097AD6-6 BTCSDR IPXA2024072394617Nut Plate · corrodedSUPPORT NUTPLATE UNDER FLOOR PANEL IN STA 1720 WITH CORROSION INSTALLED ANGLE AND SUPPORT NUTPLATE IAW B757 SRM 51-40-02 PARAGRAPH 4. RIVET P/N:MS20426AD6-10 BATCH:0004244858 REVIEWEDSDR IPXA2024072294617Nut Plate · corrodedSUPPORT NUTPLATE UNDER FLOOR PANEL IN STA 1720 WITH CORROSION.SDR IPXA2024071682131Mount · gougedCREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 HAS DEEP GOUGE. VERRIFIED RESTORED SURFACE PROTECTION IAW AMM 51-21-15-370-81A. P/N ALODINE1132 BTCH 4297395. PRIMER P/N 10-P4-2/2TU BTCH 4268566. TOPCOAT P/N PG6-W24Q BTCH 4281366.SDR IPXA202407082131Mount · gougedOPEN, CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 HAS DEEP GOUGE. REMOVED MARK BY METHOD ABRASION BY HAND AT CREW ENTRY DOOR FWD CUTOUT DOORSTOP FITTING MOUNT #2 IAW SOPM 20-30-03.SDR IPXA2024071536808Transition Panel · corrodedAFT CARGO PIT TRANSITION PANEL BS 1480-1500 HAS CORROSION. INSTALLED TRANSITION PANEL BS 1480 - 1500 IAW SRM 51-40-02-0G-0.SDR IPXA2024071134376Frame · dentedAFT CARGO PIT - FRAME STA 1340 HAS A DENT ON INNER CHORD BETWEEN STR 24R-25R. INSPECTED AND VERIFIED JOB WAS ACCOMPLISHED IAW UPS EO-90803-REQ1 AND VT MAE EA 757-5360-27-A3637 REV -. REVIEWED.SDR IPXA2024070228140Harness · missingON PRE FLIGHT SECURITY INSPECTION, "DEMO" EMERGENCY ESCAPE HARNESS MISSING INSTALLED EMERGENCY ESCAPE HARNESS REF AMM 25-61-00 THIS CLEAR THE DEFERRALSDR IPXA2024062828212Sliding Window · out of adjustFO'S NR 2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT. ADJUSTED FO'S NR 2 SLIDING WINDOW OPERATING MECHANISM IAW MM 56-11-02. OPS CHECKED GOOD.SDR IPXA2024062828190Sliding Window · out of adjustCAPTAIN'S NR 2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT. ADJUSTED CAPTAIN'S NR 2 SLIDING WINDOW OPERATING MECHANISM IAW MM 56-11-02. OPS CHECKED GOOD.SDR IPXA2024062734376Frame · dentedAFT CARGO PIT - FRAME STA 1340 HAS A DENT ON INNER CHORD BETWEEN STR 24R-25R APPROVED.SDR IPXA2024062728212Sliding Window · out of adjustFO'S #2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT READJUSTED FO'S #2 SLIDING WINDOW OPERATING MECHANISM IAW 757 MM 56-11-02 OPS CHECK GOOD.SDR IPXA2024062728190Sliding Window · out of adjustCAPTAIN'S #2 SLIDING WINDOW OPERATING MECHANISM OUT OF ADJUSTMENT READJUSTED CAPTAIN'S #2 SLIDING WINDOW OPERATING MECHANISM IAW 757 MM 56-11-02 OPS CHECK GOOD. OPENSDR IPXA2024062628140Harness · damagedON PRE FLIGHT SECURITY INSPECTION, "DEMO" EMERGENCY ESCAPE HARNESS MISSING ATTACHED P/N REQUIREMENT FOR MISSING DESCENT HARNESS ASSY. OPENSDR IPXA2024071215595Tee Fitting · corrodedKEEL BEAM AREA FOR PANEL 139CL STRUCTURE HAS CORROSION. INSTALLED NEW SUPPORT TEE I.A.W SRM 51-40-02-0G.SDR IPXA2024062486868Latch · gouged**SDR FILED OPEN** FAULT STR Z800 CREW CABIN DOOR UPPER/LOWER LATCHES ARE GOUGED.DOT 72-016 APPROVEDSDR IPXA2024062668347Fairing · crackedDURING PRE DEPARTURE CHECK FOUND #2 ENG NOSE CONE FAIRING CRACKED. REMOVED AND REPLACED NOSE CONE FAIRING WITH REPAIRED UNIT. REF AMM 72-35-01-004-001-R04 AND AMM 70-51-00. NO DEFECTS NOTED AT THIS TIME.SDR IPXA2024062468347Spinner · crackedDURING PRE DEPARTURE CHECK FOUND #2 ENG NOSE CONE FAIRING CRACKED REMOVED AND REPLACED NOSE CONE FAIRING WITH REPAIRED UNIT. REF AMM 72-35-01-004-001-R04 AND AMM 70-51-00. NO DEFECTS NOTED AT THIS TIME.SDR IPXA2024062459694Unknown · missingFO'S EVAS TEST TOOL MISSING. INSTALLED FO'S EVAS TEST TOOL AS REQUIRED
Back to Boeing 757-24APF