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 IPXA09555028Floorbeam · corrodedINSPECTION TYPE:C3 FLOORBEAM AT STA 1681.8 EVIDENCE OF CORROSION FROM RBL 30 TO 53 BULGING BETWEEN ANGLE AND SKIN. REPAIRED DAMAGED AREAS IAW ER 09-1586.SDR IPXA09555024Support Beam · damagedINSPECTION TYPE:C3 UPON REMOVAL, FOUND NR 2 PYLON FAN COWL SUPPORT BEAM O/B RAIL EDGE DAMAGE APPROXIMATELY INCHES FROM AFT END. REPAIRED FAN COWL SUPPORT BEAM O/B RAIL IAW ER 09-1804.SDR IPXA09555023Support Beam · crackedINSPECTION TYPE:C3 NR 2 PYLON FWD RT FAN COWL SUPPORT BEAM O/B RAIL CRACKED 8 INCHES FROM FRONT END. REPAIRED FAN COWL SUPPORT BEAM RAIL IAW ER 09-1804.SDR IPXA09555022Floorbeam · corrodedINSPECTION TYPE:C3 FLOORBEAM AT STA 1681.8 EVIDENCE OF CORROSION FROM RBL 20 TO 53 BULGING BETWEEN ANGLE AND SKIN. REPAIRED DAMAGED AREA IAW ER 09-1586.SDR IPXA09555021Skin · dentedINSPECTION TYPE:C1 EMPENNAGE, FILLER MISSING IS DENT AT B 1957.2 RT, UPPER SURFACE (REQUIRES REPAIR PER SRM, AS DOCUMENTED ON CARD 796286). WORK PERFORMED IAW SRM 51-70-10-2R AND ER 09-1932.SDR IPXA09555027Skin · dentedINSPECTION TYPE:C1 DENT IN FUSELAGE BELLY SKIN BS 217 RBL 17. REPAIRED DENTED AREA IAW ER 09-1803 AND SRM 53-00-01-1A-1.SDR IPXA09555043Window · damagedR2 WINDOW DELAMINATION & CRACKS. REMOVED AND REPLACED NR 2 RT COCKPIT WINDOW ASSY AS PER MM 56-11-02-4.SDR IPXA09555019Skin · wornINSPECTION TYPE:C1 LT WING NR 2 SLAT HAS WEAR ON T/E WEDGE LOWER SURFACE 14 INCHES FROM O/B END AT T/E. ALL WORK ACCOMPLISHED PER SRM 51-70-10-2R, RECEIVED APPROVAL FOR RCD SECT 2, AND ER 09-1919.SDR IPXA09555007Skin · dentedINSPECTION TYPE:C1 DENT IN FUSELAGE BELLY SKIN BS 217 RBL 17. REPAIRED DENTED AREA IAW ER 09-1803 AND SRM 53-00-01-1A-1.SDR IPXA09554994Handle · out of positionINSPECTION TYPE:N/A CAPT'S SLIDING WINDOW HANDLE, CRANK OPEN CAME OFF. FOUND CRANK HANDLE BOLT MISSING. REPLACED CRANK HANDLE CLAMP UP BOLT ASSY PER M/M 56-11-04-4. OPEN AND CLOSED WINDOW 3 TIMES WITH NO DEFECTS. P/N ON ABC7313, NO P/N OFF.SDR IPXA09555106Wedge · chafedINSPECTION TYPE:C2 NR 8 SLAT LWR T/E WEDGE HAS OUT OF LIMITS, CHAFED AREA JUST ABOVE I/B MAIN TRACK. REPAIRED PER SRM 51-70-10-2R-4.SDR IPXA09554976Frame · damagedINSPECTION TYPE:C3 LT BS 1580 FRAME I/B FLANGE SCREW STARTS 11 PLACES - MARKED. REPAIRED 11 SCREW STARTS IAW SRM ADDENDUM B757-5310-19952C.SDR IPXA09555112Wedge · dentedINSPECTION TYPE:C2 REPAIR NR 5 SLAT DENTS (2 EACH ) LOCATED ON THE T/E WEDGE FWD SURFACE 66.5 INCHES AND 70 INCHES FROM I/B END OUT OF LIMITS DUE TO THE PROXIMITY TO EACH OTHER. FABRICATED REPAIR DOUBLERS, FILLED DENTS & INSTALLED DOUBLERS SEALED & REFINISHEDSDR IPXA09554982Floor Panel · puncturedINSPECTION TYPE:C2 FLOOR PANEL BS 900-1020 RBL 24-45 WL 208 PUNCTURED ON BOTTOM BS 942. FABRICATED REPLACEMENT PANEL PER EO B757-5320-9692-F.SDR IPXA09554981Floor Panel · puncturedINSPECTION TYPE:C2 FLOOR PANEL BS 1100-1200 RBL 24-45 WL 208 PUNCTURED ON BOTTOM BS 1150. FABRICATED REPLACEMENT PANEL PER EO B757-5320-9692-F.SDR IPXA09554978Frame · damagedINSPECTION TYPE:C3 BS 1580 FRAME HAS DAMAGE AT STR 14L. REPAIRED BS 1580 FRAME AT STR 14L IAW SRM 51-00-07, SRM 53-00-07-2R.SDR IPXA09555107Threshold · corrodedINSPECTION TYPE:C2 CORROSION ON FWD CARGO DOOR THRESHOLD BS 560-620 RBL 21.5. BLENDED AND TREATED PER ATS ER 09-1916 DATED 18MAR09.SDR IPXA09554961Structure · dentedDENT ON NR 1 CARGO DOOR - REPAIR REF. EO B757-5230-3260 WILL REQUIRE REPETITIVE LFEC INSP PER EO EO.SDR IPXA09555313Door Frame · damagedINSPECTION TYPE:C ("04 ITEM") FWD CARGO DOOR JAM AT STA 620 HAS 2EA MISDRILLED HOLES HOLES IN WEB & CHORD. REMOVED DAMAGED BRACKET PER SRM 51-40-02. DIM OF DAMAGE HOLES: A UPPER HOL .330" ORIG HOLE .250 B LWR HOLE .315 IRUG GIKE .250 PER DRW NT143N8522. REMSDR IPXA09554980Seal Depressor · dentedINSPECTION TYPE:C2 FORWARD CARGO DOOR UPPER AFT SEAL DEPRESSOR IS DENTED. REMOVED AND INSTALLED NEW SEAL DEPRESSOR PER SRM 51-20-05, SRM 51-40-02.SDR IPXA09554907Lavatory · odorINSPECTION TYPE:N/A AIRCRAFT COCKPIT HAS FOUL ODOR LIKE LAV MAY NEED SERVICE. SERVICED LAVATORY PER AMM 12-17-01-3. ODOR NO LONGER PRESENT.SDR IPXA09554894Skin Panel · gougedINSPECTION TYPE:N/A LT WING T/E OUTBOARD FLAP UPPER SKIN HAS 5 EACH GOUGES. PANEL REMOVED AND ROUTED TO S/M SHOP. REMOVED DAMAGE, FABRICATED REPAIR FILLER, DOUBLER AND CORE SPLICE, PRIMERED AREA.SDR IPXA09554886Skin · dentedINSPECTION TYPE:N/A DENT IN FUSELAGE AT STA 480 STR 22R. REMOVED DAMAGE AND REPAIRED IAW EO B757-5330-32333-A.SDR IPXA09554870Skin · dentedINSPECTION TYPE:N/A DENT IN FUSELAGE SKIN AFT OF LOWER AFT CARGO DOOR SKIN AT STA 1556. REMOVED DAMAGE AND REPAIRED IAW EO B757-5330-32511-A.SDR IPXA09555032Skin · dentedINSPECTION TYPE:C1 DENT IN SKIN BS 1602, STR 4R. REPAIRED PER EA 09-1807.SDR IPXA09555031Skin · dentedINSPECTION TYPE:C1 DENT IN FUSELAGE SKIN BS 1593, STR 4R. REPAIRED PER EA 09-1807.SDR IPXA09555008Angle · crackedINSPECTION TYPE:C1 L-ANGLE CRACKED ON OUTBOARD SIDE OF THE NR 2 ENGINE PYLON, NAS 246, COMMON TO THE AFT LOWER CORNER OF PANEL 445AR CUTOUT. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-06 AND SRM 51-40-05-0G.SDR IPXA09554979Angle · crackedINSPECTION TYPE:C1 L-ANGLE CRACKED RT SIDE NR 2 PYLON NAS 209. REMOVED AND REPLACED ANGLE PER SRM 51-40-02.SDR IPXA09555020Skin · puncturedINSPECTION TYPE:C1 PUNCTURE AT RIGHT WING INBOARD MAIN FLAP TRAILING EDGE, LOWER SURFACE 9 INCHES FROM THE TRAILING EDGE, 12 INCHES OUTBOARD OF THE CENTER AFT FLAP TRACK. REPAIRED PER SRM 51-70-07.SDR IPXA09555017Flap · delaminatedINSPECTION TYPE:C1 DELAMINATION AT THE RIGHT WING OUTBOARD AFT FLAP LOWER TRAILING EDGE, 24 INCHES OUTBOARD OF THE INBOARD CENTER AFT FLAP TRACK. REPAIRED PER SRM 51-70-04-0G.SDR IPXA09554856Seat Track · corrodedINSPECTION TYPE:C4 CORROSION MAIN CABIN SEAT TRACK BS 1184, LBL 61, WL 208. REPAIRED PER ATS ENGINEERING ORDER 09-1601.SDR IPXA09555006Support · chafedINSPECTION TYPE:C1 FAIRING SUPPORT CHAFED 4 INCHES FWD OF MLG DOOR TANG DOOR CUTOUT. REPAIRED IAW SRM 51-70-11-0G.SDR IPXA09554831Seal · leakingINSPECTION TYPE:N/A DIVERSION - L2 WINDOW AIR LEAK IN FLIGHT. T/S PER FIM 56-11-53-4 TO L2 WINDOW. R&R L2 WINDOW SEAL PER MM 56-11-53-4 UP TO AND INCLUDING STEP 4(J) PAGE 2 NEEDS STEPS 4K THROUGH M. COMPLETED INSTALLATION PER MM 56-11-53-4.SDR IPXA09555156Structure · chafedINSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER EO 535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE CSDR IPXA09555155Structure · chafedINSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER E0535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE COSDR IPXA09555047Structure · chafedINSPECTION TYPE:C NR 2 ENGINE V-BAND GROOVE HAS CHAFED MARK AT 1'OCLOCK POSITION. HAND BLENDED CHAFED AREA IAW EO535-7230-32641P4 APP Z PG 1, 2 ST 1 PER SPM TASK 70-42-11-300-001. HFEC REWORK AREA IAW NTM51-00-19PT6 PER EO 535-7230-32641 P1, NO CRACK FOUND. SDR IPXA09555046Structure · chafedINSPECTION TYPE:C NR 2 ENG V-BAND GROOVE HAS CHAFED MARK AT 1 O'CLOCK POSITION. HAND BLND CHAFED AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 STP1 PER SPM TASK70-42-11-300-001. HFEC REWRK IAW NTM51-00-19PT6 PER EO535-7230- 32641P1, NO CRACK FOUND. APPLIED CSDR IPXA09554832Landing Gear · inoperativeLANDING DISAGREE MSG, GEAR WOULD NOT RETRACT. OK TO CONTINUE IAW MEL 32-30-1. LANDING GEAR RETRACT SYSTEM INOP DMP 32-30-1 C/W.SDR IPXA09555048Frame · dentedINSPECTION TYPE:C FRAME DENTED AT STA 1340 STR 25L. FOUND DAMAGE OUT OF LIMIT IAW SRM 53-00-07-1A1, FIG 101 SHT 1, NO DENT ALLOWED. DAMAGE IS .9"LX.6"WX.009"D. TRIMMED OUT DENT DAMAGE IAW SRM 53-00-07-2R, FIG 201 STEP 1. TRIMMED OUT AREA .905"L, 1.3"W. HFSDR IPXA09554969Frame · dentedINSPECTION TYPE:C DENT AT FWD CARGO COMP FUSELAGE FRAME STA 700 S24R. DENT IS D=.015 W=.310 L=.520. TRIMMED OUT DENT DAMAGE IAW SRM 53-00-07- 2R, FIG 201 SHT 1, STEP 1. SIZE OF TRIM OUT IS L=.650" W=1.2". PERFORMED HFEC IAW NTM51-00-19PT6 OF DAMAGE CONTENTSDR IPXA09554968Frame · dentedINSPECTION TYPE:C DENT AT FWD CARGO FUSELAGE FRAME STA 720, S23R-S24R. DENT IS W=.450 L=.620 D=.0250. TRIM OUT DENT DAMAGE IAW SRM 53-00-07- 2R FIG201 SHT 1 STEP 1 SIZE OF TRIM OUT L=.70" W=1.30". PERFORMED HFEC IAW NTM 51-00-19 PT6 OF DMG CUTOUT AREA. NO SDR IPXA09555130Skin · gougedINSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS 2 (EA) EVENLY SPACED GOUGES LOCATED BEHIND NR 3 SPOILER ACTUATOR 25 INCHES FWD OF T/E PER E.0. B757-5100-30760-B APPENDIX 'C' CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMITS SRM 57-53-01-1A. REMSDR IPXA09555129Skin · gougedINSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS A GOUGE REPAIR LOCATE 35.0 INCHES FROM I/B EDGE 25 INCHES FWD OF T/E PER EO B757-5100-30760-B APPEN 'C', CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMIT SRM 57-53-01-1A (2) REMOVED PREV REPAIR SRSDR IPXA09554945Frame Splice · damagedINSPECTION TYPE: C3 MAIN CARGO COMPARTMENT BS 365, STR 14L HAS MECHANICAL DAMAGE ON THE FR FRAME SPLICE. FRAME SPLICE WAS REPLACED PER SRM 51-40-02SDR IPXA09555044Frame · dentedINSPECTION TYPE:C FRAME STATION 1300 HAS A DENT BETWEEN S22R TO S23R. DNT L=.991W=.490DPTH=.039. TRIM OUT DENT DAMAGE IAW EA757-5362-27-A1836 STP1 PRELIM2 TRM SZ:W=1.5"X L=1.09". REMOVED FASTENERS CMMN TO REPAIR FOR HFEC INSP IAW SRM 51-40-02, EA757-5362-27SDR UPS09554743Skin · delaminatedRIGHT AILERON HAS DELAMINATION. R & R RIGHT AILERON ASSY PER MM 27-11-21-4. CHECKS NORMAL.SDR UPS09554736Door · delaminatedINSPECTION TYPE:N/A LT MLG DOOR L/E DELAMINATED. DAMAGE MEASURES 12.750 INCHES LONG FROM LEADING EDGE, AND 18 INCHES IN WIDTH DEP. INSTALLED NEW HEAT SHIELD AND STARTED CURE PER EO B757-5280-8537. CURE COMPLETED, REPAIR PERFORMED PER EO B757-5280-8537.SDR IPXA09554946Seat Track · corrodedINSPECTION TYPE:C3 SEAT TRACK CORRODED ON O/B FLANGE, REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, PER SRM 51-40-02-0GSDR UPS09554730Floor Panel · damagedINSPECTION TYPE:N/A FLOOR PANEL POS 5 DAMAGED 5 INCHES I/B EDGE 30 INCHES FROM AFT EDGE. REPAIRED PER EO B757-5320-32306-B.SDR UPS09554729Floor Panel · damagedINSPECTION TYPE:N/A SECTION 43 RIGHT O/B FLOOR PANEL DAMAGED. REPAIRED PER EO B757-5320-9692-F.
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