Boeing 757-24APF

Service difficulty reports · 16,067

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.

SDR IPXA2572189Structure · dentedINSPECTION TYPE: C, MAIN CARGO COMPARTMENT STA 600R STR 17 DENTED. REPAIRED DENT IAW EA 120240IR, AND EO B757-5310-46219-A.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2572187Frame · chafedINSPECTION TYPE: C, MAIN CARGO BAY BS 345 S16R INBD SURFACE OF FRAME CHAFED FROM SIDEWALL FASTENER. REMOVED DAMAGE, ORIGINAL MATERIAL THICKNESS .050 LOSS OF .020 REMAINING .030 IS OUT OF LIMITS IAW SRM 53-00-07-1A1.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2572185Floorbeam · corrodedINSPECTION TYPE:C, MAIN CARGO BAY BS 1100, LBL 25 TO LBL 45 FLOORBEAM TEE CAP HAS CORROSION AROUND EVERY NUT PLATE HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .196 LOSS OF .056 WITH .140. REMAINING IS OUT OF SRM LIMITS REPAIRS IAW EA 120254 EO B757Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2572182Frame · dentedINSPECTION TYPE:C-CK, AFT CARGO BS 1500 FRAME DENTED AT STR 23R. CUT OUT DAMAGE AT FRAME STA 1500, STR 23R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-07-2R5.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12572146Skin · dentedINSPECTION TYPE: C, LEFT WING INBD MAIN FLAP, OTBD LOWER SURFACE DENTED, 38" FORWARD OF T/E AND 36" FROM OTBD EDGE. REPAIRED AREA IAW SRM 51-70-10-2R2.Feb 6, 2012 · N456UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA12572145Attach Angle · corrodedINSPECTION TYPE: C, AFT CARGO, BS 1480 RT SIDEWALL ATTACH ANGLE CORRODED JUST BELOW S26R. REMOVED SIDEWALL ATTACH ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-40-02 AND GMM 9-10-01-4.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA12572095Frame · dentedINSPECTION TYPE: C, AFT CARGO BAY, FRAME BS 1220 ABOVE S26R DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW EA 120180 IR/ EO B757-5310-46276-A.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA12572071Frame · dentedINSPECTION TYPE: C, MAIN FUSELAGE FRAME BS 720, S15L DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA EO B757-5310-46272-A.Feb 6, 2012 · N456UP · Boeing 75724APF · Fuselage Main, FrameSDR 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 IPXA2571869Crease Beam · damagedINSPECTION TYPE: C, MAIN CARGO AFT LEFT CREASE BEAM INNER CHORD HAS EXISTING DOUBLE DRILLED HOLES AT BS 1710, LBL 55. REPAIRED EA 120148 IR AND EO B757-5310-45960-A.Feb 6, 2012 · N405UP · Boeing 75724APF · Fuselage Main, StructureSDR 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 IPXA12571512Skin · dentedSKIN DENTS 4EA BETWEEN S23L AND S24L STA 1381. REPAIRED IAW EO B757-5330-45912-A.Feb 6, 2012 · N441UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR 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 IPXA12571740Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 252XKF DAMAGED. REPLACED FLOOR PANEL 252XKF IAW B757-5320-9692-H.Feb 4, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2571606Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 252XJF DAMAGED. REPLACE FLOOR PANEL 252XJF IAW B757-5320-9692-H.Feb 4, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2571596Floor Panel · damagedINSPECTION TYPE:C-CK MAIN CARGO COMPARTMENT FLOOR PANEL 252XBF DAMAGED. REPLACED FLOOR PANEL 252XBF IAW B757-5320-9692-H.Feb 4, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571583Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XGF DAMAGED. REPLACED FLOOR PANEL 251XGF IAW B757-5320-9692-H.Feb 4, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571580Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 242XCF DAMAGED. REPLACE FLOOR PANEL 242XCF IAW B757-5320-9692-H.Feb 4, 2012 · N405UP · 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 IPXA12571574Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 232XFF DAMAGED. REPLACED FLOOR PANEL 232XFF IAW B757-5320-9692-H.Feb 4, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571415Frame · dentedINSPECTION TYPE:C-CK FWD PIT STA 800 STR 24L VERTICAL FRAME IS DENTED. REMOVED DAMAGE FROM FWD PIT STA 800, STR 24L VERTICAL FRAME, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-972R, DETAIL 1.Feb 3, 2012 · N459UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA12572157Floorboard · damagedINSPECTION TYPE: C, MAIN DECK FLOORBOARD 252XBF EDGE DAMAGE. FABRICATED NEW FLOORBOARD IAW B757-5320-9692-H.Feb 2, 2012 · N408UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2571863Floor Panel · damagedINSPECTION TYPE: C, MAIN CARGO FLOOR PANEL 251XDF DAMAGED. FABRICATE NEW FLOOR PANEL 251XDF IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2571678Floor Panel · damagedINSPECTION TYPE:C-CK MAIN CARGO COMPARTMENT FLOOR PANEL 252XEF DAMAGED. FABRICATE NEW FLOOR PANEL 252 XEF IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2571677Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 252XFF DAMAGED. FABRICATE NEW FLOOR PANEL 252XFF IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571581Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XCF DAMAGED. FABRICATED NEW FLOOR PANEL 251XCF IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571573Floor Panel · damagedINSPECTION TYPE:C-CK, FLOOR PANEL NR 232XNF IS DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571562Floor Panel · damagedINSPECTION TYPE:C-CK MAIN CARGO COMPARTMENT FLOOR PANEL 252XHF DAMAGED. FABRICATED NEW FLOOR PANEL 252XHF IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA12571559Floor Panel · damagedINSPECTION TYPE:C-CK, MAIN CARGO COMPARTMENT FLOOR PANEL 251XLF IS DAMAGED. FABRICATED NEW FLOOR PANEL 251XLF IAW EO B757-5320-9692-H.Feb 2, 2012 · N405UP · Boeing 75724APF · Fuselage Floor Panel
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