Boeing 757-24APF

Service difficulty reports · 16,067

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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 IPXA09555604Floor Panel · delaminatedINSPECTION TYPE:C4 MAIN CABIN 44 SECTION, FLOOR PANEL BETWEEN STA 1100 AND 1200 LBL45.5 TO 60 HAS DELAMED FWD AND AFT INBD CORNERS. REMOVED AND REPLACED FLOOR PANEL IAW EO B757-5320-9692-F.Apr 14, 2009 · N444UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA09555727Frame · dentedINSPECTION TYPE:C4 AFT CARGO COMPARTMENT RT FRAME IS DENTED AT BS 1280 RBL 32 WL 150. INSTALLED REPAIR DOUBLER IAW EO B757-5310-33317A.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555726Frame · dentedINSPECTION TYPE:C4 AFT CARGO COMPARTMENT RT FRAME IS DENTED AT BS 1300 RBL 34 WL 149. INSTALLED REPAIR DOUBLER IAW EO B757-5310-33307A.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555694Skin · puncturedINSPECTION TYPE:C4 NR 2 SLAT LWR SURFACE SKIN IS PUNCTURED 28 INCHES FROM I/B END 4 INCHES FROM T/E. REMOVED DAMAGED POTTED REPAIR, BONDED DOUBLER PER SRM 51-70-10-2R.Apr 13, 2009 · N444UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA09555693Frame · dentedINSPECTION TYPE:C4 BULK CARGO COMPARTMENT LT FRAME IS DENTED AT BS 1480 LBL 35 WL 153. REPAIRED FRAME PER SRM 53-00-07-2R5.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555692Skin · gougedINSPECTION TYPE:C4 GOUGE IN FUSELAGE SKIN BS 485 STR 25R. REPAIR PER ATS ER 09-2367 DATED 23APR09.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09555691Filler · chafedINSPECTION TYPE:C4 PREVIOUS REPAIR EFN 44420051001 ON IPXA MRCSSR BS1807 S-17L HAS FURTHER CHAFING ON FILLER OF PREVIOUS REPAIR. ACCOMPLISHED REPAIR PER ATS ER 09-2324 DATED APR17,2009 PRIOR TO FURTHER FLIGHT.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09555690Bracket · damagedINSPECTION TYPE:C4 NR 1 ENGINE INBOARD T/R AFT CASCADE RING LWR ATTACH FITTING BOLT HOLE IS ELONGATED. REMOVED AND REPLACED BKT PER RR EM78-31-50-000-000.Apr 13, 2009 · N444UP · Boeing 75724APF · Engine Thrust ReverserSDR IPXA09555689Floor Panel · corrodedINSPECTION TYPE:C4 CORROSION ON AFT CARGO NR 1 FLOOR PANEL RT SIDE UNDER CARGO HANDLING SYSTEM. FABRICATED FLOOR PANEL PER SRM 51-40-05-06, SRM 53-60-53-01.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA09555602Support · crackedINSPECTION TYPE:C4 NR 1 ENGINE CNA OTBD COMPRESSION ROD SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT PER AMM 20-11-00-2.Apr 13, 2009 · N444UP · Boeing 75724APF · Engine Thrust ReverserSDR IPXA09555601Support · crackedINSPECTION TYPE:C4 NR 1 ENGINE CNA, INBD COMPRESSION ROD SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT PER AMM 20-11-00-2.Apr 13, 2009 · N444UP · Boeing 75724APF · Engine Thrust ReverserSDR IPXA09555600Swivel · looseINSPECTION TYPE:C4 NR 2 NACELLE STRUT PANEL NR 444AL HOLD OPEN ROD SWIVEL IS LOOSE AND WORN. REMOVED AND REPLACED BASE PER SRM 51-40-02.Apr 13, 2009 · N444UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA09555599Floor Panel · corrodedINSPECTION TYPE:C4 CORROSION ON AFT CARGO NR 4 FLOOR PANEL RT SIDE UNDER CARGO HANDLING SYSTEM. REMOVED AND REPLACED FLOOR PANEL.Apr 13, 2009 · N444UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA09555688Web · chafedINSPECTION TYPE:C4 ENGINE NR 2 NACELLE STRUT FAIRING LOWER WEB IS CHAFED I/B LOWER SURFACE AT PPS 262. REMOVED DAMAGED AND FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-13-0G AND SRM 51-30-01-0G.Apr 12, 2009 · N444UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA09555598Threshold · corrodedINSPECTION TYPE:C4 CORROSION ON AFT CARGO LOWER THRESHOLD NUT PLATE RETAINING STRIP BS1386, 1393 AND 1406, RBL 24 WL143. REPLACED THRESHOLD NUT PLATE RETAINING STRIP.Apr 12, 2009 · N444UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA09555597Fairing · chafedINSPECTION TYPE:C4 NACELLE STRUT AFT FAIRING NR 443FR IS CHAFED ON INNER SURFACE ACCESS PANEL WAS REPLACED IAW SRM 51-40-02.Apr 12, 2009 · N444UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA09555596Swivel · looseINSPECTION TYPE:C4 NR 1 ENGINE LEFT NACELLE STRUT PANEL NR 434AL HOLD OPEN ROD SWIVEL IS LOOSE AND WORN. REMOVED AND REPLACED BASE AND SWIVEL PER SRM 51-40-02.Apr 12, 2009 · N444UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA09555588Panel · damagedINSPECTION TYPE:C2 LOWER FUSELAGE AFT KEEL BEAM PANEL SUPPORT HAS 4 ELONGATED HOLES AT STA 1140 REPLACED KEEL BEAM PANEL SUPPORT (BAFFLE) IAW SRM 51-40-05-0G, SRM 51-40-06-0G.Apr 12, 2009 · N402UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09555687Skin · misrepairedINSPECTION TYPE:C2 FOUND A FORWARD CARGO DOOR SKIN REPAIR THAT APPEARS TO MEET ALL THE REQUIREMENTS OF THE SRM 52-30-01-01-2R EXCEPT THE DOUBLER THICKNESS IS 0.080 INCH. REMOVED THE CURRENT REPAIR DOUBLER THAT DOES NOT MEET THE REQUIREMENTS OF THE SRM REPAIR Apr 10, 2009 · N402UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA09555686Carriage · chafedINSPECTION TYPE:C2 OUTBOARD MAIN FLAP NR 1 FLAP CARRIAGE FWD PANEL 666BR IS CHAFED ON INNER SURFACE. REMOVED CHAFING DAMAGE AND COMPLIED WITH ALL STEPS IN ER 09-2305 DATED 4-21-09 AND SRM 57-53-01-1-A1.Apr 10, 2009 · N402UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA09555779Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1480, BETWEEN S-26R + S-27R. DENT AT STA 1480 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101. REMOVED TRANSIT PANEL IAW 51-40-02. CUT OUT DAMAGE IAW SRM 53-00-07-2R5. HFEC AT CUTOUTApr 9, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555760Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1520, S23L. DENT AT STA 1520 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101. REMOVED CLIP IAW SRM 51-40-02. CUT OUT DAMAGE IAW SRM 53-00-07-2R5. HFEC AT CUTOUT IAW NTM51-00-19PT6, NApr 9, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555759Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1500, S-25R TO S- 27R. DENT AT STA 1500 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101. CUT OUT DAMAGE IAW 53-00-07-2R5. HFEC AT CUTOUT + HOLES IAW NTM51- 00-19PT6, NO CRACKS FOUND. Apr 9, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555758Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1500, S-25R+S-26R. DENT AT STA 1500 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101. CUT OUT DAMAGE IAW SRM 53-00-07-2R5. HFEC AT CUTOUT + HOLES IAW 757 NTM 51-00-19PT6. FAB PARTS ONApr 9, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555754Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME, STA1500, S-25L. DENT AT STA 1500 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A FIG 101. REMOVED SPLICE IAW SRM 53-40-02 AND EA757-5362-27-A1862. CUT OUT DAMAGE AREA IAW EA757-5362-27-A1862Apr 9, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555753Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1500, S25L &26L. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 SHT 1. REMOVED 2 STRINGER CLIPS STA 1500 LT S25L & 26L IAW SRM 53-40-02. CUT OUT DENT AREA IAW EA 757-53-A1862. Apr 9, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555761Frame · dentedINSPECTION TYPE:C DENT AT BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1520, S-25L + S-26L. DENT AT STA 1520 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101. CUT OUT DAMAGE IAW SRM 53-00-07-2R5. HFEC AT CUT OUT IAW NTM51 -00-19PT6, NO CRACKS FOUND. FAB Apr 8, 2009 · N441UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555685Floor Support · chafedINSPECTION TYPE:C2 FWD CARGO COMPARTMENT A/C MIX BAY FLOOR SUPPORT AT BS 845 LBL 17 WL 200 IS CHAFED. REMOVED SUPPORT, FABRICATED REPLACEMENT AND INSTALLED PER SRM 51-40-2.Apr 8, 2009 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA09555684Floor Support · chafedINSPECTION TYPE:C2 FWD CARGO COMPARTMENT A/C MIX BAY FLOOR SUPPORT AT BS 845 RBL 17 WL 200 IS CHAFED. REMOVED SUPPORT, FABRICATED AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-40-02.Apr 8, 2009 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA09555595Skin · tornINSPECTION TYPE:C2 RT WING FIXED LE UPPER SURFACE IS TORN BETWEEN NR 7 AND NR 8 LE SLATS. REPAIRED RT WING FIXED LE UPPER SURFACE BETWEEN NR 7 AND NR 8 SLATS IAW STANDARD REPAIR MANUAL EO B757-5740-11855-D.Apr 8, 2009 · N402UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA09555594Wedge · dentedINSPECTION TYPE:C2 R/W OTBD AFT FLAP UPPER T/E WEDGE HAS A DENT 28 INCH OTBD OF INBD END (SRM 57-53-01-01 REFERS TO TREAT AS A HOLE OR PUNCTURE) AFT FLAP WAS REPAIRED PER SRM51-70-04.Apr 8, 2009 · N402UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA09555593Plate · crackedINSPECTION TYPE:C2 CRACKED WIGGLE PLATE STA 330.0 R/W. REPLACED PER B757-5750-5622-A.Apr 8, 2009 · N402UP · Boeing 75724APF · Wing Miscellaneous StructureSDR IPXA09555592Floorbeam · corrodedINSPECTION TYPE:C2 CORROSION ON LONGITUDINAL BEAM BS 1012, LBL26 WL208 REPAIRED PER ER 09-2275.Apr 8, 2009 · N402UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA09555591Floorbeam · corrodedINSPECTION TYPE:C2 CORROSION AROUND SCREW HOLE AT BS 1055 LBL10-15, WL208 ON PANEL SUPPORT. REPLACED PANEL SUPPORT TEE IAW SRM 53-00-51-1A, SRM51-40-05-0G.Apr 8, 2009 · N402UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA09555590Floorbeam · corrodedINSPECTION TYPE:C2, CORROSION AROUND SCREW HOLE AT BS 1048, LBL45, WL208 ON LONGITUDINAL BEAM. BEAM SECTION WAS REPLACED PER SRM 51-40-02.Apr 8, 2009 · N402UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA09555589Support Channel · crackedINSPECTION TYPE:C2, RT MLG BODY DOOR CUTOUT FED. BULB SEAL SUPPORT CHANNEL OTBD SUPPORT ANGLE CRACKED. REMOVED AND REPLACED CRACKED BRACKET IAW SRM51-40-02-0G, AMM 32-12-51-4 STEP 3C 1-5.Apr 8, 2009 · N402UP · Boeing 75724APF · Landing Gear DoorsSDR IPXA09555683Stiffener · chafedINSPECTION TYPE:C2 LONGITUDINAL STIFFENER BELOW PANEL 445AR FWD EDGE IS CHAFING ONE FASTENER. STIFFENER WAS REPAIRED PER ATS ENGINEERING REPAIR 09-2329 DATED 24APR09.Apr 7, 2009 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA09555682Stiffener · chafedINSPECTION TYPE:C2 LONGITUDINAL STIFFENER BELOW PANEL 445AL FWD EDGE IS CHAFING VERTICAL STIFFENER AND ONE FASTENER. STIFFENER WAS REPLACED PER ATS ENGINEERING REPAIR 09-2329 DATED 24APR09.Apr 7, 2009 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA09555681Support Bracket · crackedINSPECTION TYPE:C2 FUSE & WING STRUCTURE UNDER LT AFT SUPPORT STRUCTURE IS CRACKED BS 109.2 LBL 74 WL 64. REMOVED, FABRICATED AND INSTALLED SUPPORT STRUCTURE BRACKET PER SRM 51-40-02-0G, SRM 51-30-01-09.Apr 7, 2009 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA09555587Panel · damagedINSPECTION TYPE:C2 LOWER FUSELAGE AFT KEEL BEAM PANEL SUPPORT HAS 4 ELONGATED HOLES AT STA 1100. REPLACED KEEL BEAM PANEL SUPPORT (BAFFLE) IAW SRM 51-40-06-0G, SRM51-40-05-0G.Apr 7, 2009 · N402UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09555680Plate · chafedINSPECTION TYPE:C2 NR 2 ENGINE I/B CORE COWL HAS CHAFED DEFLECTOR PLATE AT UPPER AFT INNER SURFACE. REPLACED DEFLECTOR PLATE IAW SRM 51-40-05-0G, 51-40-02-0G.Apr 6, 2009 · N402UP · Boeing 75724APF · Engine Cowling SystemSDR IPXA09555361Seat Track · corrodedINSPECTION TYPE:C3 CORROSION ON SEAT TRACK I/B FLANGE BS 1675 RBL 44 WL 208. ALL WORK ACCOMPLISH IAW SRM 51-40-05 & 51-40-08.Apr 4, 2009 · N418UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA09555661Floorbeam · corrodedINSPECTION TYPE:C CORROSION ON MAIN DECK FLOORBEAM AT STA 1200 BETWEEN LBL 3.6 AND 5.6 CORROSION IS OUT OF LIMITS. REMOVED CORROSION. FOUND OUT OF LIMITS IAW SRM 53-00-51-1A1 DETAIL II. REMOVED CEILING PNL PER SRM 51-40-02. REMOVED CLIP FWD FLOORBEAM. FABMar 30, 2009 · N439UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA09555465Floor Panel · brokenINSPECTION TYPE:C MAIN CARGO DECK FLOOR PANEL STA 900-1020 LBL 72 - 104 HAS A BROKEN FASTENER HOLE. FAB NEW MAIN CARGO FLOOR PNL STA 900-1020 LBL 72-104 ON MAE TRAVELER T9/787460 USING A402H-48X144, BATCH 1333430.Mar 28, 2009 · N439UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA09555464Floor Panel · brokenINSPECTION TYPE:C MAIN CARGO FLOOR PANEL STA 900-1020 RBL IS BROKEN AT MID AREA. FABRICATED NEW MAIN CARGO FLOOR PNL STA 900-1020 ON MAE TRAVLER T9/ 787458 USING A4024-48X144, BATCH 1333430.Mar 28, 2009 · N439UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA09555248Skin · damagedINSPECTION TYPE:N/A LT SIDE FUSELAGE HAS LIGHTNING STRIKE LOCATED 1.5 INCH FROM FWD RADIO ALT ANTENNA. REPAIR ACCOMPLISHED PER EO B757-5330-32920-A.Mar 28, 2009 · N406UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA09555196Compressor · stalledATB - RT ENG COMPRESSOR STALL AT 1000FT ON DEPARTURE. EMERGENCY DECLARED. REMOVED AND REPLACED RT ENGINE PER ENGINEERING REQUEST PER TC 5001. OPS TEST C/W PER TC 5002. SATISFACTORY AMM 71-00-00-5.Mar 28, 2009 · N454UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA09555565Skin · delaminatedINSPECTION TYPE:C RT OTBD AFT FLAP LOWER SURFACE HAS DELAMINATED 36 INCH FROM OTBD EDGE AND 7.0 INCH FWD OF THE T/E. FOUND TO BE OUT OF LIMITS PER SRM 57-53-01-1A. SANDED CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 51-70-05 PARG 5. PREP PLIES WITH GRAFIT BTMar 26, 2009 · N439UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA09555564Skin · delaminatedINSPECTION TYPE:CRH, OTBD/B AFT FLAP LOWER SURFACE HAS DELAMINATED 36 INCHES FROM OTBD EDGE AND 7.0 INCH FWD OF THE T/E. FOUND TO BE OUT OF LIMITS PER SRM 57-53-01-1A. SANDED CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 51-70-05 PARG 5. PREP PLIES WITH GRAP Mar 26, 2009 · N439UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA09555562Skin · gougedINSPECTION TYPE:C LT OTBD MAIN FLAP INBD UPPER SKIN PANEL HAS 3 SMALL GOUGES IN SKIN OF EXISTING REPAIR. FOUND OUT OF LIMITS PER SRM 57-53-01-1A 2. REMOVED SKIN PANEL IAW SRM 51-40 -02 3, SANDED AND REMOVED UPPER SKIN FOR REPAIR IAW SRM 51-70-10-2R4 4. REMOMar 26, 2009 · N439UP · Boeing 75724APF · Trailing Edge Flaps
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