N456UP

Service difficulty reports · 269

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N456UP' AND registry_match = 'registration'
  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 IPXA12572070Frame · dentedINSPECTION TYPE: C, AFT CARGO BAY, FRAME BS 1300 ABOVE S26R DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW EA 120181, EO B757-5310-46279-A.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12572065Frame · dentedINSPECTION TYPE: C, MAIN CARGO BAY, BS 1180 BETWEEN STRINGER 15L AND 16L, FRAME FREE FLANGE IS GOUGED. REMOVED DAMAGE, ORIGINAL THICKNESS .375 WITH A LOSS OF .045 AND .330. OUT OF LIMITS IAW SRM 53-40-08-1A3. ACCOMPLISHED EA 120250, EO B757-5310-46174-A.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12572064Frame · dentedINSPECTION TYPE: C, FWD CARGO BAY, BS 780, S24R VERTICAL FRAME DENTED. REMOVED DAMAGE AT FRAME, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-07-2R5, DETAIL 3.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12572045Frame · wornINSPECTION TYPE: C, MAIN CARGO BS 680R, FRAME FLANGE WEAR AREA 14" ABOVE FLOOR. BLENDED DAMAGE AREA AT BS 680R FRAME FLANGE 14" ABOVE FLOOR ORIGINAL MATERIAL .056" WITH A LOSS OF .007" AND .049" REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A-1 ACCOMPLISHED EFeb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12572044Cargo Track · corrodedINSPECTION TYPE: C, MAIN CARGO BAY BS 1063-1080, LBL 25 OTBD SEAT TRACK FLANGE HAS CORROSION AROUND 4EA NUT PLATE HOLES. BLENDED CORROSION ORIGINAL MATERIAL THICKNESS .090 WITH A LOSS OF .033 AND .057 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A1. REMOVED,Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2572033Floorbeam · corrodedINSPECTION TYPE: C, MAIN CARGO BS 1055, BL 0 TO RBL 25 FLOOR SUPPORT INTERCOSTAL HAS CORROSION AROUND 4 EA NUT PLATE HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050 MATERIAL LOSS OF .013 WITH .037 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A1. FFeb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2572032Frame · dentedINSPECTION TYPE:C-CK, AFT CARGO STA 1560 FRAME DENTED AT STR 26L. REMOVED DAMAGE AT STA 1560 FRAME, STR 26L FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-07-2R5, DETAIL 2.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2572023Frame · gougedINSPECTION TYPE:C, MAIN CARGO PIT STA 940, BETWEEN STRINGER 15R AND 16R, FRAME FREE FLANGE IS GOUGED IN 1 EA AREAS. BLENDED GOUGE AT STA 940. BETWEEN STR 15R AND 16R, ORIGINAL THICKNESS .163 WITH A LOSS OF .021 WTIH .142 REMAINING IS OUT OF LIMITS IAW SRM 5Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2572022Frame · damagedINSPECTION TYPE:C, MAIN CARGO UPSTAIRS FRAME 740 STR 15L DAMAGED. BLENDED DAMAGE AT FRAME STA 740, STR 15L, ORIGINAL THICKNESS .063 WITH A LOSS OF .011 ANS .052 REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A1 ACCOMPLISHED STEPS OF EA FOR EXTENDED LIMITS IAW EFeb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2572021Frame · wornINSPECTION TYPE:C, MAIN CARGO BS 640R FRAME FLANGE HAS WEAR AREA 14" ABOVE FLOOR. BLENDED WEAR AREA AT BS 640R FRAME FLANGE 14" ABOVE FLOOR, ORIGINAL MATERIAL THICKNESS .056 WITH A LOSS OF .007 AND .049 REMAINING IS OUT OF LIMITS IAW SRM 53-00-07-1A1. ACCOMFeb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571949Frame · dentedINSPECTION TYPE: C, FWD CARGO BAY BS 760 STR 23L VERTICAL FRAME IS DENTED. REMOVED DAMAGE FROM FRAME. FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 53-00-07-2R5, DETAIL 2.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571948Frame · dentedINSPECTION TYPE: C, FWD CARGO BAY BS 780 VERTICAL FRAME IS DENTED BETWEEN STR 23L AND 24L. REMOVED DAMAGE AT FWD CARGO PIT STA 780, VERTICAL FRAME BETWEEN STR 23L AND 24L. FABRICATED AND INSTALLED FRAME REPAIR MADE FROM 7075.0 .063 AND HEAT TREATED TO T6 COFeb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571868Frame · dentedINSPECTION TYPE: C, AFT CARGO FRAME DENTED AT BS 1320, S26L. REPAIRED FRAME IAW SRM 53-00-07-2R 5, DETAIL REV 82.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571867Frame · dentedINSPECTION TYPE: C, AFT CARGO BS 1580 FRAME DENTED BETWEEN S25L AND S26L REPAIRED FRAME IAW SRM 53-0 0-07-2R REPAIR 5, DETAIL 3, REV 82.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571866Frame · dentedINSPECTION TYPE: C, AFT CARGO STA 1520 FRAME DENTED JUST INBD OF S25L. REPAIRED FRAME IAW SRM 53-00-07-2R, REPAIR 5, DETAIL 3, REV 82.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571865Frame · dentedINSPECTION TYPE: C, FWD CARGO BAY BS 760 VERTICAL FRAME IS DENTED BETWEEN S-23R AND S-24R. REPAIRED FRAME IAW SRM 53-00 -07-2R REPAIR 5, DETAIL 1, REV 82.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571846Frame · dentedINSPECTION TYPE: C, AFT CARGO BS 1540 FRAME DENTED AT S26R, REPAIRED FRAME IAW SRM 53-00-07-2R, REPAIR 5, DETAIL 1, REV 82.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571845Frame · dentedINSPECTION TYPE: C, AFT CARGO BS 1540, FRAME DENTED AT S22R. REPAIRED FRAME IAW SRM 53-00-07 2R REPAIR 5, TABLE 2.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571844Frame · dentedINSPECTION TYPE: C, BS 1480 FRAME DENTED AT S26L. REPAIRED FRAME IAW SRM 53-00-07 2R REPAIR 5, DETAIL 1.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571842Frame · dentedINSPECTION TYPE: C, AFT CARGO BS 1500 FRAME DENTED AT S 26L. REPAIRED FRAME IAW SRM 53-00-07 2R, REPAIR 5, DETAIL 1.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571823Frame · dentedINSPECTION TYPE: C, FWD CARGO BAY BS 700, S24R VERTICAL FRAME IS DENTED CUTOUT DAMAGE AND REPAIRED FRAME AT STA 700, STR 24R BY INSTALLING REP AIR DOUBLER FABRICATED FROM 7075-T6- .071 IAW SRM 53-00-07-2R5, DETAIL 3.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571822Frame · dentedINSPECTION TYPE:C-CK, FWD CARGO PIT STA 820 VERTICAL FRAME IS DENTED BETWEEN STR 23L AND 24L. CUT OUT DAMAGE AND REPAIRED FRAME AT STA 820 BETWEEN STR 23L AND 24L BY INSTALLING REPAIR DOUBLER FABRICATED FROM 7075-T6-.063 IAW SRM 53-00 -07-2R5 DETAIL 2.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12571810Frame · dentedINSPECTION TYPE:C-CK, FWD CARGO PIT STA 800, STR 24L VERTICAL FRAME IS DENTED. CUT OUT DAMAGE AND REPAIRED FRAME AT STA 800, STR 24L BY INSTALLING REPAIR DOUBLER FABRICATED FROM 7075-T6-.080 IAW SRM 53-00-07-2R5 DETAIL 3.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2571975Floor Panel · damagedINSPECTION TYPE:C, FLOOR PANEL 212XAF HAS EDGE DAMGE AND SEVERAL PUNCTURES. FABRICATED NEW FLOOR PANEL 212XAF IAW EO B757-5320-9692-H.Feb 5, 2012 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571579Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XJF DAMAGED. REPLACE FLOOR PANEL 251XJF IAW B757-5320-9692-H.Feb 4, 2012 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA11570131Skin · damagedMAIN CARGO DOOR SKIN DAMAGED. REPAIRED IAW EO B757-5230-44889A.Oct 31, 2011 · N456UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA1569356Skin · dentedMAIN CARGO DOOR OUTER SKIN DENTED. REPAIRED FWD DENT ON MCD STA 520 IAW EO B757-5230-44346-A AND SRM 52-30-01-2R, REPAIR 4.Sep 19, 2011 · N456UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA10561496Battery Pack · inoperativeEMERGENCY EXIT LIGHTS GO OFF AFTER 5 SEC. R & R BATTERY PACK IAW AMM 33-51-07-2. OPS CK NORMAL.Aug 3, 2010 · N456UP · Boeing 75724APF · Emergency LightingSDR IPXA10558910Module · leakingSHORTLY AFTER TAKEOFF CREW NOTICED LT SYS HYD QTY MSG. DID ATB ACFT LANDED WITH .08 REMAINING QTY. MAINT FOUND LT ENG DRIVEN HYD PRESSURE AND CASE DRAIN MODULE LEAKING. REPLACED FILTER MODULE ASSY, IAW MM 29-11-17-4. CHECKED GOOD.Mar 22, 2010 · N456UP · Boeing 75724APF · Hydraulic System, MainSDR IPXA10558733Seat Track · corrodedINSPECTION TYPE:C3 UPON REMOVAL OF FLOOR PANEL FROM BS 1100-1200, FOUND SEAT TRACK TO HAVE CORROSION AROUND NUT PLATE HOLES BS 1160-1187, RBL 65, WL 208. REMOVED AND REPLACE SEAT TRACK B/S 1060-1180, RBL 65, WL 208 IAW SRM 51-40-05, 51-40-08-0G, 51-40-02-0G, Feb 23, 2010 · N456UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA10558684Channel · damagedINSPECTION TYPE:MOD RIGHT PYLON LEFT UNDERWING FAIRING SUPPORT STRUCTURE BULLNOSE ATTACH BRACKET HAS ELONGATED FASTENER HOLES AT PPS 170. REPLACED CHANNEL IAW SRM 51-40-02-0G, SRM 51-40-05, DWG313N5004 AMM 51-21-10.Feb 22, 2010 · N456UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10558679Angle · chafedINSPECTION TYPE:MOD NR 2 PYLON AFT FAIRING STRUCTURE RT FWD VERTICAL ANGLE IS CHAFED ON THE OUTER RADIUS. PPS 208.47 P/N 313N5033-100. REPLACED ANGLE IAW SRM 51-40-02-0G, SRM 51-40-05-0G, BOEING DWG 313N5033, SRM 51-40-08-0G, AMM 51-21-04-07, AMM 51-21-10-7.Feb 20, 2010 · N456UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10558683Brace · brokenINSPECTION TYPE:MOD RIGHT PYLON RT UNDERWING FAIRING SUPPORT STRUCTURE FWD BRACE HAS UPPER TAB BROKEN OFF AT PPS 185.35. REPLACED BRACE IAW SRM 51-40-02, SRM 51-40-05, SRM 54-50-71-1A 1.Feb 18, 2010 · N456UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10558682Angle · crackedINSPECTION TYPE:MOD RT PYLON RT UNDER WING FAIRING SUPPORT STRUCTURE AFT BRACE HAS A CRACK IN THE UPPER RADIUS AT PPS 185.35. REPLACED RT PYLON RT UNDERWING FAIRING SUPPORT STRUCTURE AFT BRACE PER SRM 51-40-05-0G, SRM 51-40-08-0G, SRM 51-40-02, SRM 54-50-71-1Feb 18, 2010 · N456UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA10558685Floor Panel · misrepairedINSPECTION TYPE:C3 REPAIR VALIDATION REQUIRED FOR EFN 4562008 1013, MAIN DECK FLOOR PANEL AT BS 1100-1200, LBL 45-65. FLOOR PANEL WAS REPLACED PER EO B757-5320-9692-G.Feb 16, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558582Floor Panel · corrodedINSP TYPE:C3 FWD CARGO BAY FLOOR PANEL NR 4 IS CORRODED. FABRICATED FLOOR PANEL IAW SRM 53-60-53-01-1, SRM 51-40-05 AND SRM 51-40-08.Feb 15, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558581Floor Panel · corrodedINSP TYPE:C3, FWD CARGO BAY FLOOR PANEL NR 3 IS CORRODED. FABRICATED FLOOR PANEL IAW SRM 51-40-08-0G, SRM 53-30-53-01-1 AND DWG 435N1170.Feb 15, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558579Floor Panel · puncturedINSP TYPE:C3, AFT CARGO BAY FLOOR PANEL NR 2 IS PUNCTURED. REPLACED IAW SRM 53-60-53-0I1, SRM 51-40-05, SRM 51-40-08, SRM 51-20-01-0G.Feb 15, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558578Floor Panel · corrodedINSP TYPE:C3, AFT CARGO BAY FLOOR PANEL NR 3 IS CORRODED ON UPPER SURFACE. REPLACED FLOOR PANEL IAW SRM 53-60-53-0I1, SRM 51-40-05, SRM 51-40-08, AND SRM 51-20-01-0G.Feb 15, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558561Floor Panel · corrodedINSPECTION TYPE:C3 AFT CARGO BAY FLOOR PANEL NR 4 IS CORRODED ON UPR SURFACE. R & R FLOOR PANEL IAW SRM 51-40-02; SRM 51-40-08; SRM 53-00-53-1A1; 53-60-53-01-1.Feb 15, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558560Floor Panel · corrodedINSPECTION TYPE:C3, AFT CARGO BAY FLOOR PANEL NR4 IS CORRODED ON UPPER SURFACE. R & R AFT CARGO FLOOR PNL IAW SRM 51-40-02; SRM 51-40-08; SRM 51-20-01; SRM 53-60-53-0I-1.Feb 15, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558813Panel · corrodedINSPECTION TYPE:C3, RT WING FUELING PANEL 621GB IS CORRODED UNDER THE GAUGES. FUELING PANEL WAS REPLACED IAW MM 28-21-08-4.Feb 14, 2010 · N456UP · Boeing 75724APF · Aircraft Fuel Distribution SystemSDR IPXA10558643Skin · delaminatedINSPECTION TYPE:C3, WHILE PERFORMING THE REPAIR ASSESSMENT FOUND THE NR7 SLAT T/E WEDGE TO HAVE A DELAM AT THE PREVIOUS REPAIR AT OSS 377.45-383.15 AND 4.5" FWD OF THE T/E EDGE (456-W4-03). NR 7 SLAT T/E WEDGE UPPER SURFACE WAS REPAIRED IAW SRM 51-70-10-2R.Feb 14, 2010 · N456UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA10558710Skin · gougedINSPECTION TYPE:C3 RT HORIZONTAL STAB LOWER SURFACE HAS "OUT OF LIMITS" GOUGE APPROXIMATELY 8 FT FROM OTBD END, 14 INCHES AFT OF L/. BLENDED AREA, ACCOMPLISHED REMAINING MATERIAL THICKNESS CHECK ACCOMPLISHED NDI TO VERIFY NO CRACK OR DELAMINATION PRESENT, FILFeb 13, 2010 · N456UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA10558601Floor Panel · brokenINSP TYPE:C3, MAIN CABIN INTERIOR, SECT 44, RBL 45-65, BS 900-BS 1000, FLOOR PANEL OTBD AFT CORNER IS BROKEN. PANEL WAS REPLACED IAW EO B757-5320-9692-G.Feb 13, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558600Floor Panel · damagedINSPECTION TYPE:C3, MCB FLOOR PANEL, LBL 45-65, BS 900-1020 IS DAMAGED AT FASTENER HOLE. PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.Feb 13, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558599Floor Panel · brokenINSP TYPE:C3, MCB FLOOR PANEL, LBL 25-45, BS 900-1020 INBD CORNER IS BROKEN PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.Feb 13, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558598Floor Panel · damagedINSP TYPE:C3, MCB FLOOR PANEL, RBL 25-45, BS 900-1020 IS DAMAGED. PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.Feb 13, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558597Floor Panel · damagedINSP TYPE:C3, MCB FLOOR PANEL, RBL 25-45, BS 1020-1060 IS DAMAGED AT FASTENER HOLES. PANEL WAS REPLACED IAW EO NR B757-5320-9692-G.Feb 13, 2010 · N456UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA10558596Floor Panel · delaminatedINSP TYPE:C3, MCB FLOOR PANEL LT 1680-1720 IS DELAMINATED. PANEL WAS REPLACED IAW EO B757-5320-9692-G.Feb 13, 2010 · N456UP · Boeing 75724APF · Fuselage Floor Panel
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