Boeing 757-24APF

Service difficulty reports · 16,054

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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.

SDR IPXA2024092491833Gauge · damagedCREW ENTRY DOOR, LOWER LATCH HOOK W/GAUGE DAMAGE; DOT-005, JR-117. VERIFIED WORK ACCOMPLISHED PER SREO-14721-REQ001. REVIEWEDSep 14, 2024 · N419UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024092491775Hook · damagedCREW ENTRY DOOR, UPPER LATCH HOOK W/GAUGE DAMAGE; DOT-004, JR-117. VERIFIED WORK ACCOMPLISHED PER SREO-14721-REQ001. REVIEWEDSep 14, 2024 · N419UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024091691775Latch · damagedCREW ENTRY DOOR, UPPER LATCH HOOK W/GAUGE DAMAGE; DOT-004, JR-117. APPROVED.Sep 14, 2024 · N419UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024091691833Hook · damagedCREW ENTRY DOOR, LOWER LATCH HOOK W/GAUGE DAMAGE; DOT-005, JR-117.Sep 14, 2024 · N419UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024101790819Seat Track · corrodedCORROSION ON SEAT TRACK AT LBL 62 STA 1078-1184. INSTALLED NEW SEAT TRACK P/N 144N5016-3 IAW B757-200 SRM 51-40-02-0G-0. REINSTALLED DATTO PANEL AT MAIN CARGO LBL-62 STA-1060 TO STA 1180 IAW B757-200 SRM 51-40-02-0G-0.Sep 13, 2024 · N463UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024101189030Floorbeam · corrodedCORROSION ON FLOOR BEAM AT STA 1200 LBL 62 TO RBL 62. ACCOMPLISHED REPAIR PER BOEING 757-200PF SRM 53-00-51-2R-6 REPAIR 6 FIGURE 201 REV 121.Sep 13, 2024 · N463UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024091982984Frame · dentedFAULT ZONE 100, STR: 02 EA DENTS ON FR STA 1480 AND BTW STRG 22R TO 23R, AFT CARGO COMPARTMENT. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, TABLE III. VERIFIED ACCOMPLISHMENT OF REPAIR ON FR 1480, BETWEEN STR 22R-23R.Sep 13, 2024 · N419UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024091983273Frame · dentedFAULT ZONE 100, STR: 01 EA DENTS ON FR STA 1300 AND BTW STRG 23R TO 24R, AFT CARGO COMPARTMENT. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-6, DETAIL IV PER SRM 53-60-07-2R. VERIFIED ACCOMPLISHMENT OF REPAIR ON FR 1300, BETWEEN STR 23R-24Sep 13, 2024 · N419UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2024092472968Skin · damagedR/H LOWER FUSELAGE STA 1500-1520 MARKED WITH #7 BETWEEN STRINGERS 26-25 HAS A NICK. DOT 75-021 HA-75. AFTER REMEASUREMENTS AT SKIN BETWEEN STA 1500-1520, BTW STRINGERS 26-25. P/N PR5044, BATCH# 40497. FOUND THE REAL REMAINED MATERIAL THICKNESS IS 0.034 IN. IS Sep 13, 2024 · N419UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2024091972968Skin · nickedR/H LOWER FUSELAGE STA 1500-1520 MARKED WITH #7 BETWEEN STRINGERS 26-25 HAS A NICK. DOT 75-021 HA-75 INSPECTED RESTORED SURFACE PROTECTION.<BR>JOB COMPLETED. OPENSep 13, 2024 · N419UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2024100744451Floorbeam · corrodedMC FLOOR BEAM, AT STA 1200 LBL 12 FOUND CORROSION. ACCOMPLISH PERMANENT REPAIR PER EO-91419-REQ1 AND VT-MAE 757-5360-27-A3686, REV- REVIEWEDSep 11, 2024 · N419UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024091944456Seat Track · corrodedSEAT TRACK AT STA 1195<BR> BL0 FOUND CORROSION. INSTALLED SEAT TRACK AT STA 1195, BL0. IAW B757-200 SRM 51-40-02, MATERIAL USED P/N: BACB30NX8K6, BATCH: 0004304741, COLLAR P/N: BACC30MB, BATCH: 0004287028, AND SEALANT P/N: 04-001-0109, BATCH: 0004304384. REVIESep 11, 2024 · N419UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024091944451Floorbeam · corroded*** SDR FILED OPEN *** MAJOR REPAIR *** FAULT: STR. ZONE 200 MC FLOOR BEAM, AT STA 1200 LBL 12 FOUND CORROSION. REVIEWEDSep 11, 2024 · N419UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024092433591Window · warning messageON PREFLIGHT L SIDE WINDOW EICAS MESSAGE DISPLAYED. FINISHED REMOVAL OF L/H #2 WINDOW IAW B757 AMM 56-11-02-004-010. INSTALLED L/H #2 WINDOW IAW B757 AMM 56-11-02-404-020. OPS AND LEAK CHECK PASS. DMP REVERSED. THIS CLEARS 2823959. INSTALLATION AND OPS CK OF LSep 11, 2024 · N459UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2024091133591Warning Message · illuminatedSDR FILED OPEN, ON PREFLIGHT L SIDE WINDOW EICAS MESSAGE DISPLAYED STARTED REMOVAL OF #2 WINDOW IAW B757 AMM 56-11-02-004-010 UP TO STEP 5(G) 2).Sep 11, 2024 · N459UP · Boeing 75724APF · Windshield/Door Rain/Ice RemovalSDR IPXA2024091345662Splash Guard · missing**SUPPLEMENTAL SDR** F/O EVAS SPLASH GUARD COVER MISSING. INSTALLED SPLASH GUARD AS NEEDED MM 25-60-00Sep 11, 2024 · N461UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2024091345563Splash Guard · missing**SUPPLEMENTAL SDR** CAPT EVAS SPLASH GUARD COVER MISSING. INSTALLED SPLASH GUARD AS NEEDED MM 25-60-00Sep 11, 2024 · N461UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2024091333751Torque Tube · faultedON APPROACH SELECTED FLAP 20 AND RECEIVED TE FLAP ASYM. EICAS PLUS TRAILING EDGE LIGHT. FLAPS ASYMETRY GREATHER THAN 5 AND LESS THAN 20. RII REMOVED AND REPLACED #3 TORQUE TUBE IAW AMM 27-51-25/201.Sep 11, 2024 · N430UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2024091245563Cover · damaged**SDR FILED OPEN** CAPT EVAS SPLASH GUARD COVER MISSING PART ON ORDER ZERO STOCK M-25-021-101Sep 11, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091245662Cover · damaged**SDR FILED OPEN** F/O EVAS SPLASH GUARD COVER MISSING PART ON ORDER ZERO STOCK M-25-021-101.Sep 11, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091133751Warning Light · illuminatedON APPROACH SELECTED FLAP 20 AND RECEIVED TE FLAP ASYM. EICAS PLUS TRAILING EDGE LIGHT. FLAPS ASYMETRY GREATHER THAN 5 AND LESS THAN 20.Sep 11, 2024 · N430UP · Boeing 75724APF · Trailing Flap Position Indicating SystemSDR IPXA2024091117131Escape Reel · misroutedALL 6 EMER DECENT REEL ATTACHMENT CABLES MIS-ROUTED "BACKWARDS & TWISTED TOGETHER". UN-TWISTED AND RE-ROUTED ALL DECENT CABLES TO PROPER ALLIGNMENT AND SEQUENCE PER AMM 25-61-02-201 FIG 201Sep 10, 2024 · N434UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2024091121256Light · inoperativeEMERGENCY LIGHT ANNUNCIATION INOP. R&R IAW AMM 33-51-08. OPS CHECK GOOD AT THIS TIMESep 10, 2024 · N404UP · Boeing 75724APF · Emergency LightingSDR IPXA2024092772985Plate · damagedLH ELEV O/B LWR SIDE METAL PLATE BULGING AS MARKED. FABRICATED PRIMED AND INSTALLED SPLICE PLATE PER REF DWG N. 183N2007 FROM MAT P/N: SHT-6061T4-.063 BATCH: 0003785803 REF 757-200 51-40-02-0G-0 / 51-40-05-0G-0.Sep 7, 2024 · N441UP · Boeing 75724APF · Elevator, Plate/SkinSDR IPXA2024092772979Plate · damagedRH ELEV O/B LWR SIDE METAL PLATE BULGING AS MARKED. FABRICATED PRIMED AND INSTALLED SPLICE PLATE PER REF DWG N. 183N2007 FROM MAT P/N: SHT-6061T4-.063 BATCH: 0003785803 REF 757-200 51-40-05-0G-0 / 51-40-02-0G-0Sep 7, 2024 · N441UP · Boeing 75724APF · Elevator, Plate/SkinSDR IPXA2024092474202Angle · corroded(STR) CORROSION AT FWD LOWER CARGO DOOR. I/B SIDE, LOWER AREA. PM 040-11. LOCATED, DRILLED AND INSTALLED NEW ANGLE AND RIVETS AT FWD LWR CARGO DOOR I/B SIDE LWR AREA FWD PER REF 757-200 SRM 51-40-02-0G-0. REVIEWED.Sep 7, 2024 · N441UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2024101823274Seat Track · corrodedMAIN CABIN. SEAT TRACK HAS CORROSION LOCATED AT BL0 BETWEEN STA1160 AND STA1200. (015-43) ATA53. ACCOMPLISHED REPAIR PER 757-S00PF SRM REV 121 53-00-52-2R-7 REPAIR 7.Sep 4, 2024 · N463UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024100923346Seat Track · corrodedMAIN CABIN. SEAT TRACK HAS CORROSION LOCATED AT LBL62 BETWEEN STA1140 AND STA1200. (015-45) ATA53. ACCOMPLISHED VT-SAA EA 757-5310-01-B0282 I/R AND EO-91510-REQ1, PRIOR TO FURTHER FLIGHT.Sep 4, 2024 · N463UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024091499980Tee Fitting · corrodedT-CHORD AT AIR EXHAUST AREA BETWEEN STA 1037.67 - STA 1060 R/H SIDE WITH EXFOLIATION.REMOVED CORROSION IN T-CHORD AT AIR EXHAUST AREA BETWEEN STA 1037.67 - STA 1060 R/H SIDE ORIGINAL MATERIAL: 0,115" MATERIAL LOSS: 0,0425", MAXIMUM MATERIAL LOSS ALLOWED: 0,011Sep 3, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024092390936Strap · corrodedINSIDE AFT TAIL COMPARTMENT EXFOILATION CORROSION AT STA 1787.4 R/H INTERNAL UPPER AT APU AIR INLET DUCT. DOT 140-007 INSTALLED 5EA REPAIR PARTS, 1EA AFT STRAP, NEW STRAP P/N 148N3138-20, 2 UPPER ANGLES STRAP, 2 LOWER ANGLES STRAP AND REPAIR WASHER IAW B757 SRSep 2, 2024 · N402UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2024090489688Engine · malfunctionedAIR TURNBACK DUE TO LEFT ENGINE INDICATIONS DEF PER MEL 77-11-1-1 DI # 2823227. PERFORMED TEST 13 TAKE-OFF POWER PER M/M REF 71-00-00-715-223-R03. OPS CK NORMAL ALL PARAMETERS FELL IN NORMAL RANGE.Sep 2, 2024 · N467UP · Boeing 75724APF · Engine Indicating SystemSDR IPXA2024090289688Engine · indicationAIR TURNBACK DUE TO LEFT ENGINE INDICATIONS DEF PER MEL 77-11-1-1. OPENSep 2, 2024 · N467UP · Boeing 75724APF · Engine Indicating SystemSDR IPXA2024091850713Tee Angle · corrodedUPPER T-CHORD BETWEEN STA 1180- STA 1200 L/H SIDE WITH EXFOLIATON. INSTALLED T-CHORD BETWEEN IN STA 1180- STA 1200 L/H, INSTALLED 2 EA HINGES IN STA 1140 - 1160 LH AND BTW STA 1140 - 1170 LH AND BTW STA1170 - 1180 LH INSTALLED STRAP IAW B757-200 SRM 51-40-02-0Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091855209Tee Angle · corrodedT-CHORD STA 1240 R/H RBL 59 WITH EXFOLIATION. INSTALLED NEW T-CHORD AT STA 1240 RH, I.A.W. SRM 51-40-02-0G.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091242076Barrier · corrodedMAIN CABIN RCB WALL HAS CORROSION LOCATED ON LOWER AREA BETWEEN STA BL0 AND RBL51. (015-42) ATA53. ACCOMPLISHED REPAIR PER VT-SAA EA 757-2550-01-B0269 IR AND EO-91356-REQ1, PRIOR TO FURTHER FLIGHT.Aug 30, 2024 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091249582Tee Angle · corrodedLOWER T-CHORD BETWEEN STA 1180 - STA 1260 RH SIDE WITH EXFOLIATION.VERIFIED FOUND TO BE OUT OF LIMITS. REMOVED T-CHORD IAW SRM 51-40-02. VERIFIED AND DRILLED NEW T-CHORD APPLIED ALODINE P/N ALODINEE1132 PRIMER P/N 02-013-8 IAW SRM 51-20-01.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091047960Tee Angle · corrodedT-CHORD STA 1220 R/H SIDE WITH EXFOLIATION. INSTALLED T-CHORD AT STA 1220 RH IAW SRM 51-40-02-0G.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091050624Tee Angle · corrodedLOWER T-CHORD BETWEEN STA 1180- STA 1240 L/H SIDE WITH CORROSION. INSTALLED NEW LOWER T-CHORD BETWEEN STA 1180 - STA 1240 LH I.A.W. SRM 51-40-02-0G.Aug 30, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024101012333Thrust Reverser · damagedENG#1 RH T/R TORQUE RING INNER FAIRING V BLADE NICK DAMAGE ABOUT 1 0' CLOCK POSITION (CT-10B) ATA 78 SKILL STR. ACCOMPLISHED REPAIR PER VT-SAA EA 757-7830-01-B0284 IR AND EO-91509-REQ1, PRIOR TO FURTHER FLIGHT.Aug 29, 2024 · N463UP · Boeing 75724APF · Engine Thrust ReverserSDR IPXA2024091427226Support · corrodedLOWER FWD WING TO BODY SUPPORT IN FRONT OF LEFT ECS BAY DOOR STA 900 HAS EXFOLIATING CORROSION DOT 47-10 VERIFIED INSTALLED NEW T-CHORD IN STRUCTURES ZONE 100 LOWER FWD WING TO BODY FRONT OF LEFT ECS BAY DOOR STA 900 IAW SRM 51-4O-02. MATERIAL USED: RIVET HI-LAug 29, 2024 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091126805Tee Fitting · corrodedRT MLG W/W FWD OUTBD PANEL SUPPORT T-CHORD LOWER AREA HAS EXFOLIATING CORROSION DOT 47-09. INSTALLED T-CHORD AT RH MLG W/W FWD O/B PANEL SUPPORT IAW SRM 51-40-02-0G.Aug 29, 2024 · N402UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024083095805Torque Tube · unserviceableFLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT. REPLACED TORQUE TUBES 251N4281-16,-17,-18 WITH 251N4281-26,-27,-28. REPLACED BEARING 251N4318-1 WITH 251N4381-6. ACCOMPLISHED PER AMM 27-Aug 28, 2024 · N418UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2024082995805Flap System · faultedEMERGENCY DECLARED, FLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT PER THE FIM 27-51 TREE 809 ,DID A FSEU BITE PER 27-51-00 FIG 104 . FOUND A RIGHT FLAP DRIVE FAULT. MORE TROUBLE SHOOTAug 28, 2024 · N418UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2024101779771Floor Support · corrodedMAIN CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1140 - 1200 LBL 26" - LBL 40", 4-018 , ATA 53 SKILL STR. PERFORMED FPI PER SOPM 20-20-02 IAW 757 SRM 51-10-02-OG-0. NO DEFECTS NOTED AT SEAT TRACK FLANGE LBL 40 STA=1140 TO STA=1200. REVIEW COMPLETAug 27, 2024 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024101579654Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1018 LBL 46. ACCOMPLISHED EA 757-5340-01-B0280 IR AND EO-91447-REQ1.Aug 27, 2024 · N463UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2024101179720Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE UPPER SURFACE HAS CORROSION AT STA 1140 - 1200 LBL 48", INSTALLED SEAT TRACK SECTION BTW STA 1075.5 TO 1180 LBL 45.5 IAW B757PF SRM 51-40-02-0G-0.Aug 27, 2024 · N463UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024092464213Support · looseLOWER FWD WING TO BODY SUPPORT IN FRONT OF LEFT ECS BAY DOOR STA 900 HAS EXFOLIATING CORROSION DOT 47-10. INSTALLED NEW T-CHORD IN STRUCTURES ZONE 100 LOWER FWD WING TO BODY FRONT OF LEFT ECS BAY DOOR STA 900 IAW SRM 51-4O-02.Aug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024091164453Door Frame · damagedCREW ENTRY DOOR STOP FITTING HAS MATERIAL LOSE. DOT 28-02. (RO-28). APPLIED TREATMENT, PRIMER AND TOP COAT AT CREW ENTRY DOOR STOP FITTING IAW B757 SRM 51-20-01 AND AMM 51-21-15; REVIEWEDAug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2024082764213Skin · damagedCREW ENTRY DOOR CUTOUT, INTERNAL LINNING HAS MATERIAL LOSE. DOT 28-01. (RO-28)Aug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2024082764453Stop Fitting · damagedCREW ENTRY DOOR STOP FITTING HAS MATERIAL LOSE. DOT 28-02. (RO-28)Aug 26, 2024 · N402UP · Boeing 75724APF · Fuselage Main, Structure
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