Boeing 757-24APF

Service difficulty reports · 16,067

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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"

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SDR UPS09554512Sill · corrodedINSPECTION TYPE:C2 CORROSION ON FWD CARGO DOOR CUTOUT UPPER SILL UPPER SURFACE AT WIRE STANDOFF BS 587 RBL 62 WL 201. REMOVED CORROSION, HFEC, INSTALLED REPAIR DOUBLER IAW SRM 51-70-13-0G.Jan 30, 2009 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR UPS09554585Panel · corrodedINSPECTION TYPE:C3 FUEL PANEL 642BB IS CORRODED. REPLACED PANEL WITH NEW.Jan 30, 2009 · N417UP · Boeing 75724APF · Wing, Plate/SkinSDR UPS09554584Angle · chafedINSPECTION TYPE:C3 LOWER SLIDING DOOR RECEPTACLE CLIP AT STA 336 BETWEEN 14L AND 15L IS CHAFING ON ANGLE. REPLACED ANGLE PER SRM 51-40-06-0G, AMM51-21-04-7 AND AMM 51-21-10-7.Jan 30, 2009 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR UPS09554574Support · corrodedINSPECTION TYPE:C3 FORWARD CARGO BAY, RIGHT FLOOR TO SIDEWALL SUPPORT PLATE IS CORRODED, BS 560 - BS 645 RBL 20 - RBL 25. REPAIRED SIDEWALL SUPPORT PER ER09-1274, EO B757-5330-32116-A.Jan 30, 2009 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR UPS09554572Support · corrodedINSPECTION TYPE:C3 FORWARD CARGO BAY, RIGHT FLOOR TO SIDEWALL SUPPORT PLATE IS CORRODED, BS 765 TO 845, RBL 20-RBL 25. REPAIRED FLOOR TO SIDEWALL SUPPORT PER ER 09-1275 & B757-5330-32113-A.Jan 30, 2009 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR UPS09554571Skin · dentedINSPECTION TYPE:C3 FORWARD CARGO DOOR OUTER SKIN IS DENTED 16 INCHES FROM LEADING EDGE AND 16 INCHES FROM LOWER EDGE. REPAIRED SKIN PER SRM 52-30-01-2R2.Jan 30, 2009 · N417UP · Boeing 75724APF · Cargo/Baggage DoorsSDR UPS09554489Skin · damagedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN IS DENTED AND GOUGED 15 INCHES FROM SPAR AND 80 INCHES FROM FUSELAGE. REPAIRED SKIN PER SRM 51-70-10-2R-2 PAR 4D CONTROL 09-1327.Jan 30, 2009 · N463UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR UPS09554731Wedge · dentedINSPECTION TYPE:C RT WING NR 9 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY, 9.5 INCHES FROM I/B END, 8.4 INCHES FROM T/E, .50 INCH DIA. REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 EA DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 201/Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554701Skin · dentedINSPECTION TYPE:C LT WING-35 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-15.25 INCH FROM INBD END, 5.6 INCH FROM T/E, 2.0 INCH DIA. REMOVED TOPCOAT PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E(C) PG203 FIG 201. CLEANED/PREP FORJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554700Wedge · dentedINSPECTION TYPE:C- LT WING, NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 71.75 INCH FROM INBD END, 4.5 INCH FROM T/E, 1.8 INCH DIA. REMOVED TOPCOAT PREP FOR BOND OF DOUBLER IAW SRM 57-43-02/51-70-10, REPAIR NR 2 E(C) PG 203 FIG 201. CLEANEDJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554699Skin · dentedINSPECTION TYPE:C LT WING NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 69.0 INCHES FROM OTBD END, 1.6 INCH FROM T/E, 1.7 INCH DIA. REMOVED TOPCOAT TO PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E(C) PG 203 FIG 201. CLEANED/Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554698Skin · dentedINSPECTION TYPE:C LT WING NR 5 SLAT T/E WEDGE HAS 2 DENT INCH DIA. REMOVED TOPCOAT PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E,(C) PAGE 203M FIG 201. CLEANED AND PREP FOR BOND IAW SRM 57-43-02/51-70-10 REPAIR NR 2, (C) PG 203 FIG 201. FABRJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554697Skin · dentedINSPECTION TYPE:C LT WING, NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-16.25 INCH FROM OTBD END, 2.8 INCH FROM T/E 1.5 INCH DIAMETER. REMOVED TOPCOAT FOR BOND OF DOUBLER IAW SRM 57-43-02/57-70-10, REPAIR NR 2 E(C) PG 203, FIG 201. CLEANED/Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554696Skin · dentedINSPECTION TYPE:C RT WING, NR 6 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-58.0 INCH FROM OTBD END, 4.8 INCH FROM T/E 1.5 INCH DIA. EVAL DENT DUE TO HAIL DAMAGE IAW SRM 57-43-03-A1 FIG 101 SHT 4. REMOVED SURF FINISH PREP FOR BOND IAW SRM 57-43Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554695Wedge · dentedINSPECTION TYPE:C RT WING, NR 6 SLAT T/E WEDGE HAS 1 WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY-36.5 INCHES FROM OTBD END,1.45 INCH FROM T/E .050 INCH DIA. REMOVED SUR FINISH AND PREP FOR BOND IAW SRM 57-43-02 REP 1 FIG 201/SRM 51-70 10 REP NR 2, E(C) PJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554694Wedge · dentedINSPECTION TYPE:C LT WING, NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 73 INCHES FROM OTBD END, 1.7 INCH FROM T/E. REMOVED TOPCOAT TO PREPARE BOND DOUBLER IAW SRM 57-43-02/51-70-10, REPAIR NR 2 E(C) PG 203, FIG 201. CLEANED AND PREPPED FOR Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554693Wedge · dentedINSPECTION TYPE:C LT WING NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 6.5 INCHES FROM OTBD END, 6.3 INCHES FROM T/E (MARKED AS GROUP 1). REMOVED TOPCOAT TO PREPARE BOND DOUBLER IAW SRM 57-43-02 AND SRM 51-70-10, REP NR 2, E(C) PG 203, FIG 20Jan 29, 2009 · N440UP · Boeing 75724APF · Wing Main, Frame StructureSDR UPS09554691Wedge · dentedINSPECTION TYPE:C LT WING-NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY-97.5 INCH FROM OTBD END, 2.1 INCH FROM T/E (MARKED GRP 3). REMOVED TOPCOAT TO PREPARE FOR BOND OF DOUBLER IAW SRM 57-43-02 AND SRM 51-70-10 PRE NR 2,E, (C)PG203, FIG201. Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554673Skin · dentedINSPECTION TYPE:C RT WING, NR 9 SLAT T/E EDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 57.1 INCH FROM INBD END, 8.3 INCH FROM T/E, .70 INCH DIA. REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 201 SRM 51-70-1Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554672Skin · dentedINSPECTION TYPE:C RT WING, NR 9 SLAT T/E HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 19.9 INCH FROM OTBD END, 6.4 INCH FROM T/E, 1.8 INCH DIA (MARKED GROUP 3). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 2Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554665Wedge · dentedINSPECTION TYPE:C RT WING NR 10 SLAT T/E WEDGE HAS 2 (EA) DENTS OUT OF LIMITS DUE TO PROXIMITY 36.75 INCHES FROM T/E, 2.0 INCHES DIA (MARKED GROUP 2). REMOVED SURFACE FINISH FAB AND BONDED 1(EA) DOUBLER IAW SRM 57-43-02 & SRM 51-70-10-R2 FIG 201.Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554664Wedge · dentedINSPECTION TYPE:C RT WING NR 8 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY 46.7 INCHES FROM O/B END, 8.25A INCHES FROM T/E .60 DIA (MARKED GROUP 2). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-53-02 REPAIR 1 FIG 201 Jan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554663Wedge · dentedINSPECTION TYPE:C RT WING NR 8 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY 36.5 INCHES FROM O/B END, 1.2 INCH FROM T/E, .65 INCH DIA (MARKED GROUP 1). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIGJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554662Wedge · dentedINSPECTION TYPE:C RT WING - NR 7 SLAT T/E WEDGE HAS 1(EA) DENT OUT OF LIMITS DUE TO PROXIMITY 100.26 INCHES FROM O/B END, 1.6 INCH FROM T/E, .50 INCH DIA (MARKED GROUP 1). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02, REPAIR 1 FIJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554661Wedge · dentedINSPECTION TYPE:C RT WING - NR 7 SLAT T/E WEDGE HAS 1EA DENT OUT OF LIMITS DUE TO PROXIMITY 46.7 INCHES FROM O/B END, 4.55 FROM T/E IN A 1.7 DIA (MARKED AS GROUP 2). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02 REPAIR 1 FIG 201 PJan 29, 2009 · N440UP · Boeing 75724APF · Leading Edge DevicesSDR UPS09554531Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1060-1100 RBL 25, EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1060-1100 RBL 25 PER SAMPLE IAW EO B757-5520-9692-F. MATERIAL P/N A402H-48X144. MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALJan 29, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554479Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1020-1055 LBL 24-45 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1020-1055 LBL 24-45, PER SAMPLE IAW EO B757-5320-9692-F, MATERIAL A402H-48X144 MATERIAL BATCH 0001333438. PART IS AIRWORTHY AND IS OK TO INSTALLJan 29, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554474Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1020-1055 LBL 24-45 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1020-1055 LBL 24-45, PER SAMPLE IAW EO B757-5320-9692-F, MATERIAL A402H-48X144 MATERIAL BATCH 0001333 438.Jan 29, 2009 · N440UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS09554461Pump · failedINSPECTION TYPE:N/A LEFT EDP HYD LOW PRESS LIGHT ILLUM. EICAS MSG DISPLAYED L HYD ENG PUMP. EICAS MSG L HYD SYS MAINT WAS NOT DISPLAYED. HYD QTY NORMAL. POWER XFER UNIT STATUS MSG DISPLAYED. REPLACED LT HYD EDP, CASE DRAIN FILTER, AND PRESSURE FILTER. ACJan 29, 2009 · N452UP · Boeing 75724APF · Hydraulic Pump (Electric/Engine), MainSDR UPS09554611Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE ON INBOARD FLANGE STR 15R BS 1300. REPAIRED PER B757-5310-19952C AND SRM 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554610Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15R BS 1220. REPAIRED PER B757-5310-19952C AND SRM 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554609Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1620. REPAIRED DAMAGE INBOARD FLANGE AT STR 15L BS 1620 IAW UPS EO B757-5310-19952C AND B757 SRM 51-40-09-0G, 51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554608Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1580. REPAIRED PER B757-5310-19952C AND SRM 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554607Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1540. REPAIRED PER B757-5310-19952C AND SRM 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554606Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1500. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554605Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1460. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND SRM 51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554604Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1420. REMOVED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554603Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1380. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554602Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOUND AT STR 15L BS 1340. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554601Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1260. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554600Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1220. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-40-02-0G 51-20-01-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554599Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15R BS 1180. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-40-09-0G 51-20-01-0G, 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554598Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15R BS 1100. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-20-01-0G 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554597Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15R BS 1140. REPAIRED DAMAGE IAW UPS EO B757-5310-19952C AND B757 SRM 51-40-09-0G, 51-20-01-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554473Frame · damagedINSPECTION TYPE:C3 FRAME DAMAGE INBOARD FLANGE AT STR 15L BS 1140. REPAIRED DAMAGE IAW UPS EO B757-5310-19952-C AND 51-40-07-0G 51-20-01-0G, 51-40-02-0G.Jan 27, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554432Oil System · overservicedINSPECTION TYPE:N/A DURING LANDING ROLL OUT, WHILE USING REVERSE THRUST, THE CREW SMELLED SMOKE IN THE COCKPIT. DURING TAXI IN, THE SMOKE SMELL APPEARED TO DISSIPATE. NO EMERGENCY DECLARED. PER FIM 21-00-01, 1.C. (1) (B) DETERMINED RT ENGINE OIL QTY OVER SEJan 27, 2009 · N416UP · Boeing 75724APF · Turbine Engine Oil SystemSDR UPS09554425Frame · dentedINSPECTION TYPE:N/A DENT IN INNER CORD FUSELAGE FRAME AT BS 720 AT STR 23L. REPAIRED PER EO B757-5310-31723-C.Jan 25, 2009 · N432UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554705Frame · damagedINSPECTION TYPE:C3 FRAME AT STA 440 HAS MECHANIC DAMAGE BETWEEN STR 7L-15L. BLENDED DAMAGE, CUTOUT IS OUT OF LIMITS AREA, INSTALLED DOUBLER IAW ER 09-1306.Jan 24, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554726Frame · damagedINSPECTION TYPE:C3 MECHANICAL DAMAGE ON FRAME BS 365.25 BETWEEN STR 6R TO 15RT. REPAIR PER ATS ER 09-1309.Jan 23, 2009 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554692Frame · damagedINSPECTION TYPE:C3 BODY STATION 345 FRAME RIGHT SIDE HAS MECHANICAL DAMAGE BETWEEN STRINGER 8R AND 15R (7 PLACES). ALL REFERENCE AND REPAIR PROCEDURES ACCOMPLISHED PER SRM ADDENDUM AMM B757-5310-32189A AND ER 09-1307.Jan 23, 2009 · N417UP · Boeing 75724APF · Fuselage Main, Frame
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