Boeing 757-24APF

Service difficulty reports · 16,054

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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.

SDR IPXA2024040292431Motor · failedAT 38,000 MASTER CAUTION CABIN ALTITUDE EICAS MSG. AFTER LANDING CABIN ALT 2 STATUS MSG RAN FIM 21-30 FAULT TREE 802. #2 CABIN PRESSURE CONTROLLER FAULTED AC MOTOR. TECH RECOMMENDED REPLACING AC MOTOR & CABIN PRESSURE CONTROLLER. R&R'D CPC AND OUTFLOW VALVE ACApr 2, 2024 · N472UP · Boeing 75724APF · Pressure Regulator/Outflow ValveSDR IPXA2024041978080Skin · corrodedFAULT-STRUC-400-#2 PYLON OUTBD INNER SKIN FWD OF VENT PANEL OPENING HAS EXFOLATION CORROSION. DOT 8-010. WORK ACCOMPLISHED PER UPS EO:EO90099-REQ1 AND VTMAE 757-5450-27-A3572 REV-,FAA 8100-9.Apr 1, 2024 · N454UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024033153256Door · corrodedCORROSION FOUND AT APU DOOR STATION 1885 4 O CLOCK POSITION COMPLETED REPAIR SEE EO-89984-PRELIM2Mar 31, 2024 · N462UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2024033153261Door · corrodedCORROSION FOUND AT APU DOOR STATION 1885 8 O CLOCK POSITION.REMOVED FASTENERS AND DAMAGE TRIM OUT IS 3.50€? X 3.25€?. COMPLETED PARAGRAPHS 1 THRU 4 OF SRM 53-80-01-2 REPAIR 3. COMPLETED REPAIR IAW EO-89978-REQ1Mar 31, 2024 · N462UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2024040618602Floorbeam · corrodedMAIN DECK FLOOR - STA 1720 BETWEEN BL 0 AND RBL 45, 3 NUTPLATES STRAPS WITH CORROSION INSTALLED (3EA) ANGLES AND (3EA) NUTPLATES STRAP I.A.W. SRM 51-40-02-0G.Mar 28, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024040618589Floorbeam · corrodedMAIN DECK FLOOR - STA 1720 BETWEEN BL 0 AND LBL 45, 4 NUTPLATES STRAPS WITH CORROSION INSTALLED (2EA) NEW ANGLES, (4EA) NUTPLATES STRAP AND (2EA) EXISTING ANGLES I.A.W. SRM 51-40-02-0G.Mar 28, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024041599046Tee Fitting · corroded*** SUPPLEMENTAL SDR *** FAULT: THE CROSS-FLOOR SUPPORT TIE AT STA 1060 LBL ZERO HAS INITAIL SIGNS OF CORROSION. DOT 39-03 INSTALLED SUPPORT FLOOR P/N 144N5005-5 I.A.W. SRM 51-40-02 FASTENRES USED:MS20426AD3-12 BTCH: 0004238822, BACN10JZ3A2U BATCH:004200335.Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024041594591Tee Fitting · corroded*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1220 LH HAS CORROSION APPLIED TOPCOAT NEW T-CHORD I.A.W AMM51-21-15 PAINT CUP. #: 02-012-176.Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024040999046Floorbeam · corrodedMAJOR REPAIR. THE CROSS-FLOOR SUPPORT TIE AT STA 1060 LBL ZERO HAS INITAIL SIGNS OF CORROSION. DOT 39-03 AUDIT COMPLETEMar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024032894591Tee Fitting · corrodedWTB STRUCTURE - T-CHORD STA 1220 LH HAS CORROSION VERIFIED EVALUATED T-CHORD AT STA 1200 LH, 100% MATERIAL LOST, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71-1A-1 DETAIL V. AND REMOVED T-CHORD DAMAGED I.A.W. SRM 51-40-02-0G.Mar 27, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024041084031Frame · dented*** SUPPLEMENTAL SDR *** FAULT: AFT CARGO PIT - FRAME RH SIDE STA 1220 HAS A DENT IN UPPER FLANGE AT STR23R INSTALLED REPAIR SPLICE AT FRAME 1220 RH IAW SRM 51-40-02-0G AND 53-00-07-2R-6.Mar 26, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024032784031Frame · dentedAFT CARGO PIT - FRAME RH SIDE STA 1220 HAS A DENT IN UPPER FLANGE AT STR23R FRAME STA1220 RH THE DAMAGE FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-00-07-1A-9.Mar 26, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024041560472Tee Angle · corrodedWTB STRUCTURE - T-CHORD STA 1200 -1240 LH HAS CORROSION INSTALLED NEW T-CHORD I.A.W SRM 51-40-02-0G.Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024041060688Frame · dentedFWD CARGO PIT - FRAME STA 820 LH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 24L AND 25L. DOT 101-5 INSP COMPLETE JOB COMPLETE.Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024040860472Tee Fitting · corrodedWTB STRUCTURE - T-CHORD STA 1200 -1240 LH HAS CORROSION VERIFIED CIC.Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024040260754Transition Panel · dentedFWD CARGO PIT - TRANSITION PANEL BETWEEN FS580 TO 600 LH SIDE HAS A DENT. DOT 101-6 VERIFIED: AFTER FURTHER EVALUATION, DENT FOUND TO BE WITHIN LIMITS I.A.W. B757 SRM 53-00-53-1A-1, FIGURE 101 , DETAIL VI. VERIFIED JOB COMPLETE. REVIEWED.Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024032660576Frame · dentedFWD CARGO PIT - FRAME STA 780 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 23R AND 24R. DOT 101-3 APPROVED.Mar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024032660754Transition Panel · dentedFWD CARGO PIT - TRANSITION PANEL BETWEEN FS580 TO 600 LH SIDE HAS A DENT. DOT 101-6 VERIFIED: AFTER FURTHER EVALUATION, DENT FOUND TO BE WITHIN LIMITS I.A.W. B757 SRM 53-00-53-1A-1, FIGURE 101 , DETAIL VI. VERIFIED JOB COMPLETE. OPENMar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024032660672Frame · dentedFAULT: FWD CARGO PIT - FRAME STA 820 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 23R AND 24R. DOT 101-4 FRAME STA 820RH, DENT IN UPPER FLANGE IS NOT ALLOWED I.A.W. B757-200 S.R.M. 53-00-07-1A-1 FIG 101. OPENMar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024032660588Frame · dentedFWD CARGO PIT - FRAME STA 720 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 23R AND 24R. DOT 101-1 VERIFIED: TRIMMED OUT DAMAGED AREA I.A.W. B757-200 S.R.M. 51-10-02.<BR>DIMENSIONS CUT OUT L=1.800" W=.900". OPENMar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024032660625Frame · dentedFWD CARGO PIT - FRAME STA 760 RH SIDE HAS A DENT IN UPPER FLANGE BETWEEN STR 22R AND 23R.DOT 101-2 REQUEST NDT. OPENMar 25, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024041540206Transition Panel · corrodedAFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1200 TO STA 1310 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1220,1240,1260,1280,1300) DOT 07308-009 INSTALLED DOUBLER AND SIDE PANEL I.A.W B757 SRM 51-40-02-0G.Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024041540194Transition Panel · corroded*** SUPPLEMENTAL SDR *** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1310 TO STA 1380 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1320,1340,1360,1380) DOT 07308-007 INSTALLED NEW TRANSITION PANEL I.A.W B757 SRM 51-40-02-0G.Mar 23, 2024 · N451UP · Boeing 75724APF · Cargo CompartmentsSDR IPXA2024041540134Transition Panel · corrodedAFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1440 TO STA 1530 HAS CORROSION AROUND TIE DOWN FITTINGS ( STA 1460,1480,1500,1520) DOT 07308-002 INSTALLED TRANSITION PANEL I.A.W B757 SRM 51-40-02-0G.Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024041140134Transition Panel · corrodedAFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1440 TO STA 1530 HAS CORROSION AROUND TIE DOWN FITTINGS ( STA 1460,1480,1500,1520) DOT 07308-002 VERIFIED: INSTALLED TRANSITION PANEL I.A.W B757 SRM 51-40-02-0G.Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024041040212Frame · dented*MAJOR REPAIR* **SDR FILED OPEN** FAULT: AFT CARGO PIT - FRAME RH SIDE STA 1240 HAS A DENT IN UPPER FLANGE AT STR26R VERIFIED NDT FINDINGS FOR STEP #6 AND STEP #11, NO DEFECTS NOTED AT THIS TIME.Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024041040206Panel · corroded*MAJOR REPAIR* **SDR FILED OPEN** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1200 TO STA 1310 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1220,1240,1260,1280,1300) DOT 07308-009 REVIEWED.Mar 23, 2024 · N451UP · Boeing 75724APF · Cargo CompartmentsSDR IPXA2024041040194Panel · corroded*MAJOR REPAIR* **SDR FILED OPEN** FAULT: AFT CARGO PIT - RH SIDE TRANSITION PANEL FROM STA 1310 TO STA 1380 HAS CORROSION AROUND TIE DOWN FITTINGS (STA 1320,1340,1360,1380) DOT 07308-007 REF STEP 16. INSPECTED AND VERIFED TRANSITION PANEL IS INSTALLED. INSP Mar 23, 2024 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024041726547Door Latch · gougedCREW ENTRY DOOR LATCHES ( UPPER AND LOWER ) HAS SIGN OF GOUGES . 89-282 APPLIED TREAT AND PRIME I.A.W. SRM 51-20-01-OG. PRIME MIXED IN CUP P/N 02-012-176. ACCOMPLISHED STEP 5 AND 6 PER SREO-14721-REQ001.JOB COMPLETE.Mar 22, 2024 · N451UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024032526547Latch · gougedCREW ENTRY DOOR LATCHES ( UPPER AND LOWER ) HAS SIGN OF GOUGES . 89-282 VERIFIED: COMPLETED STEP 1 TASK CARD T3F18E004GCY I.A.W. B757 SRM 51-10-02.Mar 22, 2024 · N451UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024032045317Engine · slowLEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + MATCH RIGHT ENGINE. REMOVED AND REPLACED LH ENG FUEL FLOW GOVERNOR REF B757 AMM 73-21-01. PERFORMED Mar 14, 2024 · N469UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR IPXA2024031545317Governor · slowLEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + MATCH RIGHT ENGINE. REMOVED AND REPLACED LH ENG FUEL FLOW GOVERNOR REF B757 AMM 73-21-01. PERFORMED Mar 14, 2024 · N469UP · Boeing 75724APF · Turbine GovernorSDR IPXA2024031689909Stringer · corrodedCORROSION FOUND AT AFT PIT FUSELAGE AREA APPROX STA 1455 COMPLETED ALL STEPS OF EO-89792-REQ1 AS REQUIRED . THIS IS A PERMANENT REPAIRMar 11, 2024 · N452UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2024031189909Not Reported · corroded*SDR FILED OPEN* CORROSION FOUND AT AFT PIT FUSELAGE AREA APPROX STA 1455Mar 11, 2024 · N452UP · Boeing 75724APF · Fuselage Structure (General)SDR IPXA2024031397688Sliding Window · warning message*** SUPPLEMENTAL SDR *** L SIDE WINDOW EICAS WITH INOP LIGHT R&R LH #2 SLIDING WINDOW ASSY PER AMM 56-11-02. ALL TESTS SATIS, PLACARD REMOVED.Mar 5, 2024 · N451UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2024030597688Warning Light · illuminated*SDR FILED OPEN* L SIDE WINDOW EICAS WITH INOP LIGHT PART ON ORDER REQ # 489335Mar 5, 2024 · N451UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2024040259120Panel · damagedDAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DEFERED PER EO-89694 CORRECTIVE ACTION. SPEED TAPE APPLIED TO THE AREA. ITEM CLOSED AND FAULT TRANSFERRED TO BARCODE T3F18E0047VUR FOR REPAIR AND DEADLINE EXTENSION.Mar 2, 2024 · N469UP · Boeing 75724APF · Rudder StructureSDR IPXA2024032260994Skin Panel · corroded*SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT: EVIDENCE OF CORRISON ON INSIDE SURFACE OF #2 PYLON FWD OF PANEL 443CR. DOT 142-17. ACCOMPLISH EO-89829-REQ1 AND EA 757-5450-27-A3546. AUDIT COMPLETE.Mar 2, 2024 · N460UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024032659729Latch · gouged*SUPPLEMENTAL SDR* FAULT - CREW ENTRY DOOR LATCHES UPPER AND LOWER APPEAR TO HAVE GOUGES . 89-237 BLENDED OUT CREW DOOR LATCHES UPPER AND LOWER IAW SREO-14721-REQ001. HFEC PERFORMED ON CREW ENTRY DOOR LATCHES UPPER AND LOWER. NO DEFECTS FOUDN IAW 51-00-21. T96Mar 2, 2024 · N460UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024030459120Hinge · damaged*SDR FILED OPEN* DAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DAMAGED BONDED PANEL REMOVED. WAITING ON NEW PANELMar 2, 2024 · N469UP · Boeing 75724APF · Rudder StructureSDR IPXA2024030459729Latch · gougedCREW ENTRY DOOR LATCHES UPPER AND LOWER APPEAR TO HAVE GOUGES . 89-237 APPROVED OPENMar 2, 2024 · N460UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024030435420Metering Valve · faultedDURING PREFLIGHT BRAKE PRESSURE ACCUMULATOR LOSES PRESSURE FROM 3000 PSI TO 2500 PSI IN 1 MINUTE. POSSIBLE PRESSURE LEAK IN ACCUMULATOR. PRESSURIZED TO RESET STAB TRIM & SET PARKING BRAKE. CAPPED RETURN LINES TO PARKING BRAKE VALVE, LEAK DOWN STILL OUT OF LIMIMar 1, 2024 · N410UP · Boeing 75724APF · Landing Gear Brake SystemSDR IPXA2024031116195Intercostal · corroded*SDR FILED OPEN* FAULT: L/H FWD OF HOT AIR EXHAUST HAS CORROSION. DOT 33-007 INSTALLED NEW INTERCOSTAL IAW B757 SRM 51-40-02-0G. INSTALLED HOT AIR EXHAUST L/H COVER IAW B757 AMM 21-53-04-404-012. VERIFIED INSTALLATION OF COVER, JOB COMPLETEFeb 29, 2024 · N427UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024031805314Floorbeam · corrodedFLOORBEAM BS 1040 BETWEEN LBL 10 TO LBL 20 LOWER SURFACE WITH CHAFING INSTALLED T-CHORD STA 1040 I.A.W. B757 SRM 51-40-02-OG. JOB WAS ACCOMPLISHED PER UPS EO: EO-89720-REQ1 AND VT MAE EA 757-5340-27-A3538 REV -. WITHOUT ANY DEVIATIONS.Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024031405260Floorbeam · corrodedFAULT- T-CHORD STA 900 BETWEEN LBL 20 TO LBL 40 LOWER SURFACE WITH CHAFING. INSTALLED T-CHORD AND (8 EA) REPAIR SPLICE PLATES I.A.W. B757-200 SRM 51-40-02-0G AND SRM 51-70-12-05-0 DETAIL LLL.Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024031405314Floorbeam · chafedT-CHORD STA 1040 BETWEEN LBL 10 TO LBL 20 LOWER SURFACE WITH CHAFING VERIFIED ACCOMPLISHMENT OF EA 757-5340-27-A3538 STEPS 1-3 PRELIMINARY 1Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024031406476Frame · dentedAFT CARGO PIT STA 1320, SRG 26 RH HAS A DENT ON FRAME ACCOMPLISH REPAIR PER EO-89673-REQ1 REV 1 AND VT-MAE EA 757-5360-27-A3530, REV. -., PRIOR TO FURTHER FLIGHT.Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024031306423Shear Tie · dentedAFT CARGO PIT STA 1320, STG 25 LH HAS A DENT ON FRAME. VERIFIED ACCOMPLISMENT OF STEPS 12-27 OF EA 77-5360-27-A3533 REV. WITH NOTED DEVIATION.Feb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Internal Mounting StructureSDR IPXA2024031204950Tee Fitting · corroded*SDR FILED OPEN* FAULT - T-CHORD STA 1040 BETWEEN RBL 10 TO RBL 20 LOWER SURFACE WITH CHAFING. VERIFIED: INSTALLED T-CHORD STA 1040 I.A.W. B757 200 51-40-02-OG. INSTALLED COVER HOT AIR EXHAUST ACTUADOR I.A.W. SRM 51-40-02-OG. VERIFIED COVER INSTALLEDFeb 28, 2024 · N427UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024030781374Governor · unserviceable*SUPPLEMENTAL SDR* *IFSD* DURING DESCENT INTO TPA, OUT OF FL200,RIGHT ENGINE FLAMED OUT. ACCOMPLISHED QRH & LANDED, "R ENG LP PUMP" STATUS MSG DISPLAYED. DID NOT ATTEMPT RELIGHT. C/W RII 2. CESAR MENDIETA (TECHNICIAN), 28-FEB-2024 23:47 UTC INSTALLED RT ENG LPFeb 27, 2024 · N474UP · Boeing 75724APF · Engine Fuel and Control
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