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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS09554475Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL STA 1025-1060 RBL 60 EDGES & CORNERS DAMAGED. FABRICATED NEW MCD FLOOR PNL STA 1025-1060 RBL 60, PER SAMPLE IAW EO B757-5320-9692-F. MATERIAL P/N A402H-48Z144 MATERIAL BATCH 000 1333438.SDR UPS09554331Skin · damagedINSPECTION TYPE: C2 BS 477, S3L FUSELAGE HAS LIGHTNING STRIKE. REMOVED DAMAGED FASTENER, REPAIRED HOLE, INSTALLED NEW FASTENER IAW EO B757-5330-31827-A.SDR UPS09554365Support Bracket · crackedINSPECTION TYPE:C2 INBOARD SUPPORT BRACKET IS CRACKED AT AFT COMPRESSION ROD ON THE NR 2 ENGINE, 12 O'CLOCK POSITION PPS195. REMOVED AND REPLACED NR 2 ENG I/B AFT COMPRESSION ROD SUPPORT BRACKET IAW SRM 51-40-02.SDR UPS09554285Engine · vibrationEXCESSIVE VIBRATION NR 2 ENGINE. VIBRATION REGISTERED 5.0. CREW DECLARED EMERGENCY AND DIVERTED. FUMES EMINATED FROM OVERHEAD PANEL. NR 2 ENGINE PACK SHUTDOWN. INSPECTED INLET LP N1 BLADES, NOSE COWL AND EXHAUST AREA. NO DAMAGE OR OIL LEAKS FOUND. ACCOMP. FIMSDR UPS09554284Anti-Ice Valve · failedRT ENG ANTI-ICE VALVE FAILED IN THE CLOSED POSITION. 392171. DEFERRED PER MEL 30-21-1-1 ACCOMPLISHED DMP 30-21-1-1 PARTIALLY OPEN.SDR UPS09554277Floor Panel · dentedINSPECTION TYPE: N/A CENTER OF FLOOR PANEL AT POS 7/8 LT, 1 INCH DENT WITH CRACK IN TOP SHEET. REPAIRED IAW EO B757-5320-31573.SDR UPS09554275Skin · dentedDENT IN LOWER SURFACE PANEL NR113N2402. DENT MEASURES 1.250 INCHES IN DIA. X .060 INCH DEEP WITH .250 INCH HOLE AT CENTER OF DENT. AFTER CUTOUT OF DAMAGE RESULTS IN 1.5 INCHES DIA. CORE CUTOUT OF 1.5 DIA INCHES. REPAIRED IAW EO B757-5750-31769-B AND SRM 57SDR UPS09554366Support Angle · corrodedINSPECTION TYPE:C2 CORROSION ON THE CAPT'S RT RUDDER RACEWAY, RT SUPPORT ANGLE, P/N 253T 5518-1 BS 229, LBL 6, WL 200. REMOVED AND REPLACED SUPPORT ANGLE PER DWG 253T5518, SRM 51-40-05, AND SRM 51-20-01-0G.SDR UPS09554688Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1300 STR 26L. TRIM OUT DAMAGE AREA, DIM:L=0.530 INCH W=1.550 INCH IAW EA 757-5362-27-A1822 STEP1. HFEC INS TRIMMED AREA PER NTM51-00-19 PT6. NO CRACK IND NOTED. ENLARGED CUTOUT BY 0.04 INCH AS INS CUT IAW EA 757-5362-27-A1SDR UPS09554716Frame · dentedINSPECTION TYPE:C FRAME DENTED - BS 1320, BETWEEN STR 25-26R. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-07-2R STEP 1. HFEC INSPECTED TRIMMED AREA PER NTM 51-00-19 PT.6 NO CRACKS. TRIMMED OUT DAMAGED AREA IAW SRM 53-00-07-2R5 STEP 2. AFTER INSURANCE CUTOUT MEASDR UPS09554715Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1540 STR 25R. TRIMMED OUT DAMAGED AREA IAW B757-200 SRM 53-00-07-2R STEP 1 2. NDT HFEC INSPECTED TRIMMED AREA PER NTM 51-00-19 PT.6. NO CRACKS. PERFORMED AN INSURANCE CUTOUT .04 INCH AROUND TRIMMED OUT AREA IAW AFTER INSURASDR UPS09554713Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1380 STR 25L. TRIMMED DAMAGE AREA, MEASURES L=.900" W=1.05" IAW SRM 53-00-07-2R5 STEP 1. HFEC INSP TRIMMED AREA PER NTM 51-00-19 PT6, NO CRACK INDICATION NOTED. PERFORMED INS CUT BY 0.04" NEW DIMENSION L=.940" W=1.09". FABSDR UPS09554712Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1560 STR 25L. TRIMMED OUT DAMAGE MEASURES W=1.0",L=.600 IAW B757-200 SRM 53-00-07-2R STEP 1. HFEC INSP TRIMMED AREA PER NTM 51-00-19 PT6. NO CRACK INDICATIONS NOTED. PERFORMED INS CUT OF 0.04" AND AFFECTED AREA IAW B757-20SDR UPS09554711Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1540, STR 25R. TRIMMED OUT DAMAGED AREA IAW B757-200 SRM 53-00-07-2R, STEP 1. HFEC INSP TRIMMED AREA PER NTM51-00-19 PT6 NO CRACK INDICATION NOTED. PERFORMED INS CUTOUT OF .04 INCH AROUND TRIMMED OUT AREA IAW B757-200 SRM 5SDR UPS09554625Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1440, STR 26L. TRIM OUT THE DAMAGE AREA IAW SRM 53-00-07-2R5 STEP 1. HFEC INSPECTED AREA PER NTM 51-00-19 PT6. NO CRACK INDICATIONS NOTED. PERFORMED INSURANCE CUT, FINAL DIM OF THE CUTOUT ARE: L=.590" W= 1.290", IAW SRM 53SDR UPS09554623Frame · dentedINSPECTION TYPE:C FRAME DENTED-BX 1500, STR 26L. TRIMMED OUT DAMAGED AREA IAW B757-200 SRM 53-00-07-2R, STEP 1. NDT HFEC CUT OUT IAW 757 NDT 51-00-19&16 PT6. NO DEFECTS FOUND. PERFORMED AN INSURANCE CUT OF .04 INCH AROUND AFFECTED AREA IAW B757- 200 SRM 53SDR UPS09554621Frame · dentedINSPECTION TYPE:C FRAME DENTED BS 1480, STR 26L. TRIMMED OUT DAMAGED OF FR 1480, S26L IAW SRM 53-00-07-2RS, STEP 1. NDT HFEC INSPECTED TRIMMED AREA PER NTM51-00-19 PT6. NO CRACK INDICATIONS NOTED. PERFORMED INSURANCE CUT, FINAL CUT-OUT DIMENSIONS L=1.23" WSDR UPS09554620Frame · dentedINSPECTION TYPE:C FRAME DENTED-2PL-2.0 INCHES APART-BS 1500, STR 26L. TRIMMED DAMAGE AREA IAW SRM 53-00-07-2R FIG 201 SHT 1 STEP 1 2. HFEC INSPECTED TRIMMED AREA PER NTM51-00-19 PT6. NO CRACK INDICATION NOTED. TRIMMED OUT DAMAGE AREA BY .04 INCH AS AN INSUSDR UPS09554619Floor Support · deformedINSPECTION TYPE:C AFT PIT FLOOR SUPPORT AT STA 1300 LBL 3 DEFORMED. REMOVED DAMAGE SECTION OF FLOOR SUPPORT Z-ANGLE (54.12" LONG) IAW SRM 51-70-12-0G, FIG 1 SHT 1 STEP 1. W=1.4" X L=1.6" 2. LOCATED & DRILLED NEW SECTION OF EXTRUSION (Z-ANGLE) BAC1517-2226 70SDR UPS09554618Floor Support · deformedINSPECTION TYPE:C AFT PIT FLOOR SUPPORT AT STA 1380 RBL 3 DEFORMED. REMOVED DAMAGE SECTION OF FLOOR SUPPORT Z-ANGLE (75.12 INCH LONG) IAW SRM 51-70-12-06 FIG 1 SHT1 STEP 1. DAMAGE MEASURES 1.4"W X 2.0"L 2. LOCATED & DRILLED NEW SECTION OF EXTRUSION (Z-ANGLESDR UPS09554363Bracket · crackedINSPECTION TYPE:C1 NR 1 ENGINE NACELLE FWD SUPPORT ANGLE FOR ACCESS PANEL 435 AT LWR BRACKET CRACKED. REPLACED BRACKET PER SRM 51-40-02-0G.SDR UPS09554369Skin · damagedINSPECTION TYPE:C1 AOG RESPONSIBILITY, WHILE DRILLING OFF FASTENER HEAD ON CNTR TANK ACCESS PANEL 134AZ CAME OFF FASTENER AND CAUSED DAMAGE TO FUEL CELL CUT OUT EDGE. REPAIRED PER ATS ENGINEERING REPAIR 09-1026.SDR UPS09554368Panel · corrodedINSPECTION TYPE:C1 CORROSION ON AFT CARGO COMPARTMENT SIDE PANEL BS 1380 TO BS 1360 RBL 20 TO RBL 24 WL 147. REMOVED & REPLACED DAMAGED PART OF SIDE PANEL IAW SRM 53-0053-1A 51-40-02, 53-60-53-01, 51-30-01-0G, MM 51-31-01-2 & MM 25-00-00-7.SDR UPS09554364Seat Track · corrodedINSPECTION TYPE:C1 CORROSION ON CAPT'S O/B SEAT TRACK AT FWD MOUNT BOLT BS 233 LBL 26 WL 200.5. TRACK WAS REPLACED PER SOPM 20-50-01.SDR UPS09554362Web · corrodedINSPECTION TYPE:C1 CORROSION ON FLOOR AFT OF CAPTAINS RT RACEWAY AT BS 229 LBL 9 WL 200.5. REPAIRED PER SRM 51-70-13-0G.SDR UPS09554380Skin Panel · misrepairedINSPECTION TYPE:C1 WHILE WORKING EO B757-5100-30760A FOUND REPAIR AT BS 1224.5, 2.5 INCHES ABOVE STR 12L TO NOT MATCH SRM 53-00-01 FIG 208. REPAIR MISSING 12TH OUTER ROW FASTENER. REPAIR WAS REPLACED PER ATS ENGINEERING REPAIR 09-1027 DATED 15JAN2009.SDR UPS09554301Web · corrodedINSPECTION TYPE:C1 CORROSION ON FLOOR AFT OF CAPTAINS RT RACEWAY AT BS 229 LBL 9, WL 200.5. REPAIRED PER SRM 51-70-13-0G.SDR UPS09554375Strut · corrodedINSPECTION TYPE:C2 CORROSION ON THE NR 2 ENGINE CNA LWR STRUT 6 O'CLOCK POSITION PPS205. REPAIRED PER ATS ER 09-1052 DATED 12JAN09 AND UPS EO 757-7810-31855A.SDR UPS09554377Support Channel · chafedINSPECTION TYPE:C2 APU FIRE WIRE SUPPORT BRACKET RT APU ACCESS DOOR IS CHAFING ON APU FUEL LINE AT 4TH LATCH FROM THE FRONT. REMOVED SUPPORT CHANNEL, FABRICATED AND INSTALLED REPLACEMENT CHANNEL PER SRM 51-40-02SDR UPS09554376Fitting · gougedINSPECTION TYPE:C2 NR 1 ENGINE O/B T/R INNER SURFACE AFT LWR CORNER FITTING IS GOUGED. REMOVED AND REPLACED FITTING PER RR EM 70-42-28-300-05.SDR UPS09554374Seal Depressor · dentedINSPECTION TYPE:C2 DENT ON FWD CARGO DOOR AFT SEAL DEPRESSOR 20 INCHES FROM DOOR BOTTOM. REPAIRED PER ATS ENGINEERING REPAIR 09-1025.SDR UPS09554300Retainer · corrodedINSPECTION TYPE:C2 CORROSION ON NUT PLATE RETAINER ON THE BOTTOM OF THE FLOOR WEB BS 1715 RBL 4.5 WL 208. REMOVED, FABRICATED AND INSTALLED PLATE PER SRM 51-40-02.SDR UPS09554330Nut Plate · corrodedINSPECTION TYPE: C2 CORROSION, NUTPLATE RETAINER ON THE BOTTOM OF THE FLOOR WEB BS 1715 RBL 4.5 WL 208, REMOVED, FABRICATED AND INSTALLED PLATE IAW SRM 51-40-02.SDR UPS08554253Skin Panel · dentedINSPECTION TYPE:C D385560 LOWER VERTICAL STAB PANEL SKIN 175N2001-4 RT HAS SKIN DENT. REMOVED VERTICAL L/E PANEL 321BL TO FOM IAW MM 55-25-01-4. REMOVED DOUBLERS IAW SRM 51-70-10 PG 202 REPAIR 4 VERTICAL STA 172. SANDED AREA IAW SRM 51-70-10 PG 202 REPAIR 4SDR UPS08554233Indication Sys · malfunctionedINSPECTION TYPE:N/A EICAS MSG L FWD ENT DOOR DISPLAYED & ENTRY DOORS OPEN LIGHT ILLUMINATED WITH DOOR CLOSED. ***SDR FILED OPEN*** DEFERRED PER MEL 52-71-1 M-391356. VERIFIED L1 DOOR CLOSED & LOCKED. OK FOR SERVICE. DEFERRAL REMAINS.SDR UPS08554216Seal · leakingPBE VACUUM SEAL COMPROMISED. REMOVED AND REPLACED PBE.SDR UPS08554215Door · inoperativeINSPECTION TYPE:N/A ATB - AFTER TAKEOFF CREW REPORTED GEAR WOULD NOT RETRACT. GEAR DISAGREE & GEAR DOOR LIGHT ILLUMINATED (AIRFRAME VIBRATION) LEVEL OFF AT 5000. GEAR RETRACTS AT 5000 WITH LIGHTS EXTINGUISHED. GEAR DEPLOYED NORMALLY UPON LANDING. REPLACED SDR UPS08554207Roller · out of adjustINSPECTION TYPE:N/A L2 WINDOW WILL NOT OPEN. ADJUSTED LOWER AFT ROLLER. ACCOMPLISHED NR 2 WINDOW LATCHING SYS HANDLE ALL WORK PER MM 56-11-02-5. OK FOR SERVICE.SDR UPS08554201Floor Panel · damagedINSPECTION TYPE:N/A 3RD PANEL FROM RT SIDE DAMAGE 12 INCHES FROM AFT OF PANEL STA 440 SEC 43 8 INCH DIA AREA TOP SKIN AND CORE. REPLACED PANEL.SDR UPS08554200Floorboard · damagedINSPECTION TYPE:N/A LT MOST O/B FLOORBOARD 17 INCHES FROM AFT END OF PANEL POS 4 STA 440 SEC 4 43 DAMAGE 3 BY 1 INCHES TOP OF SKIN AND CORE. REPLACED PANEL.SDR UPS08554199Floor Panel · damagedINSPECTION TYPE:N/A 2ND PANEL FROM RT SIDE 17 INCHES FROM AFT OF PANEL STA 440 SEC 43 POS 4 DAMAGE CONSIDERED AS ONE 4 INCH DIA TOP SKIN AND CORE. REPLACED PANEL.SDR UPS08554190Skin · dentedINSPECTION TYPE:N/A DENT IN LWR FLAP SKIN LT INBOARD MAIN FLAP. REPAIRED IAW B757-5750-31130-B.SDR UPS08554197Window · bindingINSPECTION TYPE:N/A UNABLE TO OPEN CAPTAINS COCKPIT WINDOW. HANDLE MOVES AFT BUT WINDOW WILL NOT OPEN. CHECKED CAPTAINS C/P WINDOW WINDOW IAW MM 56-11-02-215-089. TESTS OK.SDR UPS08554188Flap · damagedINSPECTION TYPE:N/A LT OUTBOARD AFT FLAP T/E LWR SURFACE INTERIM REPAIR. REPAIRED FLAP PER B757-5750-31551-A.SDR UPS08554135Window · out of adjustINSPECTION TYPE:N/A L2 WINDOW HARD TO OPERATE. ADJUSTED L2 WINDOW PER MM 56-11-02-5.SDR UPS08554091Floor Panel · damagedINSPECTION TYPE:N/A MAIN DECK FLOOR PANEL POS 8 HAS HOLE. REPAIRED PER SRM 53-00-50-2R.SDR UPS08554083Engine · faultyINSPECTION TYPE:N/A RT PACK EXTREME ODOR/FUMES WHEN OPERATING SHUT DOWN RT PACK & FUMES EXTINGUISHED. ACCOMPLISHED NR 2 ENG PWR RUN PER MM 71-00-00-5. OIL FUMES EMITTED FROM NR 2 ENG WITH EITHER PACK L OR R SELECTED AND ENG ABOVE GRD IDLE. FUMES DISSIPATED SDR UPS08554029Unknown · odorINSPECTION TYPE:N/A AIR TURNBACK AT 1020Z DURING CLIMBOUT AT APPROX 15,000FT, NOTICED AN ODOR IN THE COCKPIT FOLLOWED A MINUTE OR TWO LATER BY THE PRESENCE OF A LIGHT HAZE. DURING THE SMOKE/FUMES CHECKLIST NOTICED THE RIGHT ENGINE OIL PRESSURE IN THE AMBER BASDR UPS08554051Unknown · odorINSPECTION TYPE:N/A NOTICED ODOR AND LIGHT HAZE IN COCKPIT DURING CLIMB. FOUND FUEL IN NR 2 ENGINE OIL SYSTEM. PER FIM CHANGED NR 2 ENGINE LOW PRESSURE AND HIGH PRESSURE FUEL PUMPS, FFG, FCOC AND FCOC BYPASS VALVE. ALSO PERFORMED DUCT BURNOUT OF PNEUMATIC DSDR UPS08553970Window · out of adjustINSPECTION TYPE:N/A CAPTAIN'S SIDE WINDOW HARD TO OPEN. ADJUSTED L2 WINDOW W/REF TO AMM 56-11-02-5. WINDOW HANDLE OPERATES NORMALLY.
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