Boeing 757-2T7
Service difficulty reports · 666
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 = '7572T7' 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 = '7572T7' 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 FDEA202610131587Indication Sys · malfunctionedDURING CLIMB OUT, GOT RT HYD SYS PRESSURE EICAS & ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE & NORMAL QUANTITY. EMERGENCY DECLARED. IAW CHAPTER 6, AMM 26-18-00-5, AMM 29-11-00-5, AMM 28-22-00-5, AMM 75-32-01-2, AMM 73-2SDR FDEA202610131564Wire · shortedDURING CLIMB OUT GOT R HYD SYS PRESS EICAS AND ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE AND NORMAL QUANTITY. EMERGENCY DECLARED. FOUND WIRE W5200-0073-20 SHORTED TO GROUND. REMOVED CONTACTS 2 & 3 OF C/P D3064 & SHORT TSDR FDEA202609181374Eec · failedL EEC EICAS DURING TAKEOFF ROLL AND 4X IN FLIGHT ALL WITH ASSOCIATED AUTOTHROTTLES EICAS. NOTABLE YAW IN FLIGHT WHEN IT WOULD OCCUR. COMPLIED WITH QRH. FIM: 73-21 FAULT TREE 822 ON HIGH POWER RUN FOUND LH EEC WENT TO OFF AS THROTTLES WERE INCREASED. PERSDR FDEA202609141333Gust Lock · failedWHILE CLOSING THE L-1 DOOR, RAMP WAS UNABLE TO RELEASE THE GUST LOCK. FOUND HOLD OPEN DOOR COLLAR DAMAGED AND WILL REQUIRE REPLACEMENT. PART NIS AT FLL. AMM 52-11-08-8 REMOVED AND REPLACED L1 DOOR HOLD OPEN SPLIT COLLAR ASSY IAW AMM 52-11-08-8. L1 DOORSDR FDEA202607231013Beam · corrodedNOSE WHEEL WELL STRUCTURE BS 310.5 LOWER AREA INTERNAL BEAM WITH CORROSION REMOVED VERTICAL BEAM OUT OF LIMITS AT NOSE WEEL STRUCTURE BS 310.5 LBL 20.05 LOWER AREA INTERNAL IAW B757 51-40-02-0G; TRIMED LOCATED, DRILLED AND INSTALLED NEW VERTICAL BEAM REPLASDR FDEA202607200955Strap · corrodedAPU INLET DUCT ATTACHMENTS AT THE AFT FRAME WITH CORROSION CORRSION OUT OF LIMITS AT APU INLET DUCT ATTACHMENTS ON THE AFT FRAME (MIDDLE STRAP) IAW B-757 SRM 53-80-15-1A WAS REPAIRED IAW B-757 SRM 53-80-15-2R REPAIR 1SDR FDEA202607200954Crease Beam · corrodedMCC CREASE BEAM SIDE LH BSTA 1620 TO BSTA 1370 IT HAS CORROSION SPOTS MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1430 TO 1530 LBL 64.40 IAW B-757 SRM 53-60-13-1A, WAS REPAIRED IAW B-757 SRM 53-00-13-2R REPAIR 1SDR FDEA202607200953Crease Beam · corrodedMCC SIDE LH BETWEEN BS 1080 TO BS 1100 CREASE BEAM WITH CORROSION MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1040 TO STA 1100 IAW B-757 SRM 53-40-13-1A WAS REPAIRED IAW B-757 SRM 53-40-13-1A, WAS REPAIRED IAW B-757 SRM 53-00-13-2R RSDR FDEA202607150928Floorbeam · corrodedMCC BL 0 TO LBL 24.75 BS 1200 FLOOR BEAM WITH CORROSION AREA WITH CORROSION OUT OF LIMITS AT FLOOR BEAM BS 1200 LBL 8 TO LBL 14 WAS REPAIRED IAW B757 SRM 53-00-51-2R REPAIR 5SDR FDEA202607150927Collar · brokenL1 DOOR GUST LOCK FOUND BROKEN DURING POST FLIGHT CHECK UPON FLIGHT ARRIVAL. REINSTALLED NEW AND SERVICEABLE GUST LOCK AS REQUIRED, OPS CHECK GOOD IAW AMM 52-11-08-8.SDR FDEA202607100893Skin Panel · dentedUPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I.A.W B757 SRM 53-80-01-1A, TABLE I, NOTE 'C', FIG 101, SHEET 2 AND SRM 51-70-10-2R REP '4'SDR FDEA202607100892Access Panel · crackedLH WING #3 SLAT LOWER SKIN ACCESS PANEL 523GB AREA WITH 02 EA CRACK. 2EA CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523GB AREA WERE REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4SDR FDEA202607100890Access Panel · crackedLH WING #3 SLAT LOWER SKIN ACCESS PANEL 523FB AREA WITH 01EA CRACK. CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523FB AREA WAS REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4.SDR FDEA202605280640Gust Lock · damagedL1 DOOR HOLD OPEN LOCK IS BROKEN. TROUBLESHOOTING REQUIRED PRIOR TO INSTALLING IPC EFFECTIVITY VERIFICATION IS ALSO REQUIRED. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR AND OPS CHKD GOOD IAW AMM 52-11-08-4.SDR FDEA202601060008Skin · corrodedENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA IS WITH CORROSION AREA WITH CORROSION AT ENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA WAS REPAIRED PER FEDEX E.A. #: F-5430-T0385801 P1 WITH TITLE: NACELLES / PYLONS - - SKIN / SDR FDEA202601060007Crease Beam · crackedRH LOBE INTERIOR BETWEEN BS 1720 AND STR 17 HAS CREASE BEAM WITH CRACK 2 INCH APROX. ACCOMPLISHED REPAIR ON ADDITIONAL DAMAGE FOUND: CRACK IN THE HOLE AT AFT PRESSURE BULKHEAD STA 1720 PER FEDEX E.A.#: F-5310-T0385818 P1 WITH TITLE: FUSELAGE - MAINFRAME - SDR FDEA202512302297Skin · corrodedNR 1 ENGINE NACELLE STRUT PP STA 174.30 R/H FWD BULKHEAD INTERNAL SIDE SKIN WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A.#: F - 5430 - T0385806 P1 WITH TITLE: NACELLES/PYLONS - SKIN/PLATES/PANELS - RN 1 PYLON INBD SIDE SKIN INNER SURFACE CORROSSDR FDEA202512302296Skin · corrodedNR 1 ENGINE NACELLE STRUT ACCESS PANEL 433JR CUTOUT WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A F- 5430 - T0385806 P1SDR FDEA202512292295Stringer · corrodedMEC BETWEEN BS 418 - 440, S24R CORRODED. PERMANENTLY REPAIRED STRINGER 24R IAW SRM 53-00-03-2R, REP 2, FIG 201.SDR FDEA202512272292Skin · corrodedNO 1 ENGINE NACELLE BETWEEN ACCESS PANEL 433 HR AND 433 JR INTERNAL SKIN WITH CORROSION. JOBS FOR NR W/O 91519, N00437 AND N00438 WAS INCLUDED AND ACCOMPLISHED UNDER FEDEX EA F-5430-T0385806 P1SDR FDEA202512222284Crease Beam · corrodedMAIN CABIN. CREASE BEAM. (RH) STA 1200 CORRODED. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT CREASE BEAM INBOARD CHORD AT STA 1200 RBL 64 WAS REPAIRED IAW B-757 SRM 53-00-13-2RSDR FDEA202512222283Crease Beam · corrodedMCC FLOOR BTWN STA 440 - 460 (RH CREASE BEAM) RBL 64.5 APROX WAS FOUND ON LOCATION WITH CORROSION. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT, CREASE BEAM INBOARD CHORD BTW STA 440-460 RBL 64.40 WAS REPAIRED IAW B-757 SRM 53-00-13-2RSDR FDEA202512222282Crease Beam · corrodedMAIN CARGO BAY, FLOOR INBOARD CHORD HAS SURFACE CORROSION AROUND NUTS PLATE BETWEEN BS 860 AND 879 CORROSION OUT OF LIMITS AT MAIN CARGO BAY CREASE BEAM INBOARD CHORD BTW STA 860 - 879 RBL 64 WAS REPAIRED IAW SRM 53-00-13-2R.SDR FDEA202512192264Skin · corrodedENG NR 2 NACELLE STRUT FWD ACCESS PANEL 443AR INSIDE SKIN IS WITH CORROSION. (INNER AREA.) ENG. NR 2 NACELLE STRUT OTBD SIDE FWD ACCESS PANEL 443AR SKIN OUT OF LIMITS WAS REPLACED IAW SRM 51-41-02-0G AND DWG 311N5041 REV. K.SDR FDEA202512172260Deck Plate · corrodedPOINTS NR 2 AND 3 WITH CORROSION OUT OF LIMITS AT DECK PLATE AREA, BS 1681, BTW RBL 13 - 23, OUT OF LIMITS AT CABIN DECK PLATE. REPAIRED IAW SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE II.SDR FDEA202512172259Skin · corrodedNR 2 NACELLE STRUT FWD ACCESS PANEL 443GL INSIDE SKIN AREA IS WITH CORROSION. NR 2 NACELLE STRUT INBD SIDE FWD ACCESS PANEL 443GL SKIN OUT OF LIMITS WAS REPLACED IAW SRM 51-41-02-0G AND DWG 311N5041, REV. KSDR FDEA202512122247Shear Web · corrodedCABIN FLOOR SHEAR WEB HAD MULTIPLES SPOTS OF CORROSION, BS 1680 - 1720, AREA OUT OF LIMITS. BS 1697, LBL 08 IAW SRM 53-60-51-1A. REPAIRED IAW SRM 53-60-51-2R, REPAIR 2, ALTERNATIVE II.SDR FDEA202512122246Seat Track · corrodedMAIN CARGO BAY SEAT TRACK 45.50 RBL BETWEEN BS 1100 -1140 HAS MULTIPLE AREAS WITH CORROSION. REMOVED SEAT TRACK BS 1076 TO 1180, RBL 45.50 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 51-40-05-0G, SRM 51SDR FDEA202512122245Seat Track · corrodedMAIN CARGO BAY, SEAT TRACK 45.50 LBL BETWEEN BS 1180 - 1200 WITH CORROSION IN MULTIPLES AREAS. REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 1180 TO 1240, LBL 45.50 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED NEW SEAT TRACK REPLACSDR FDEA202512122244Seat Track · corrodedMAIN CARGO BAY FLOOR SEAT TRACK HAS SURFACE CORROSION BETWEEN BS 680 & 720, RBL 58.22. REMOVED SEAT TRACK SECTION OUT LIMITS AT MAIN CARGO BS BS 640 - 880, RBL 58.22 IAW SRM 51-40-02-0G. TRIMED, LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-05SDR FDEA202512122243Seat Track · corrodedMAIN CABIN. SEAT TRACK, RBL 58.22 BTW BS 1180 TO 1200 CORRODED REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT BS 1180 TO 1420 RBL 58.22 IAW SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED & INSTALLED A NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 5SDR FDEA202512122242Seat Track · corrodedMAIN CARGO BAY SEAT TRACK LBL 58.22, BS 1180 - 1420 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION IAW SRM 51-40-02-0G. TRIMMED, LOCATED, DRILLED AND INSTALLED A NEW SEAT TRACK REPLACEMENT SECTION IAW SRM 51-40-05-0G, SRM 51-40-08-0G, SRMSDR FDEA202512122241Seat Track · corrodedMAIN CARGO COMPARMENT SEAT TRACK LBL BETWEEN BS 1180 - 900 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 900 - 1180, LBL 58.22 IAW SRM 51-40-02-0G; TRIMMED, LOCATED, DRILLED AND INSTALLED A NEW SEAT TRACSDR FDEA202512122240Skin · delaminatedLEFT WING OTBD MAIN FLAP T/E UPPER SURFACE HAD POSSIBLE DELAMINATION. APPLIED PERMANENT REPAIR ON AREAS WITH DELAMINATION AT LT WING OTBD MAIN FLAP T/E UPPER SURFACE BTW WBL 471 - WBL 501 IAW SRM 57-53-01-2R, TABLE III, AND SRM 51-70-07-0G.SDR FDEA202512112237Crease Beam · corrodedMAIN CARGO BAY FLOOR CREASE BEAM HAS SURFACE CORROSION BETWEEN BS 760 AND 780. REMOVED CREASE BEAM INBD CHORD SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT LBL 64.20 BS 760 TO 900 IAW B757 SRM 51-40-02-0G; TRIMED, LOCATED, DRILLED AND INSTALLED NEW CREASE SDR FDEA202512102230Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN HAD REPAIR DAMAGE AT LOWER INTERNAL SURFACE, HSS 104.248 & 128.248, DENT WITH DELAMINATION AT LT HORIZONTAL STAB UPPER SKIN ON LOWER INTERNAL SURFACE WAS APPLIED PERMANENT REPAIR IAW SRM 55-10-01-1A, TABLE 1, NOTE I, & SRM 51-SDR FDEA202512102229Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN HAD FIVE DENTS BETWEEN HSS 81.249 AND 104.248, APPLIED PERMANENT REPAIR AT LT HORIZONTAL STAB UPPER SKIN IAW SRM 55-10-01-1A, TABLE I NOTE I & SRM 51-70-10-2RSDR FDEA202506060850Gust Lock · inoperativeL1 DOOR GUST LOCK FOUND DAMAGED/BROKEN ON WALKAROUND. AMM: 52-11-08-8 INSTALLED NEW SPLIT COLLAR IRW AMM 52-11-08-8.SDR FDEA202408301193Transmission · dirtyTE FLAP DISAGREE ON APPROACH. FLAPS STUCK BETWEEN 20-25 DEGREES. EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING PER FIM. FOUND FAULT CODE 305 (FLAP DISAGREE) ON FSEU-1. PERFORMED VISUAL INSPECTION OF ALL FLAP DRIVE TRANSMISSIONS AND JACKSCREWS. FOUND FLAP #5SDR FDEA202408171144Stringer · corrodedFORWARD CARGO LSTR 19-22 STA 760 FRAME HAS AREAS OF CORROSION AT SKIN ATTACHMENT POINTS AND STR EVALUATED CORROSION AT SKIN ATTACHMENT POINTS S-19L, 21L, AND 22L NO CORROSION NOTED. REPAIRED STRINGER WITH SPLICE, SHEAR TIE, AND FILLER BETWEEN S-19L TO 20L SDR FDEA202406280877Battery · no testLEFT SIDE EMERGENCY LIGHTS DO NOT TEST. R & R LT EMERGENCY LIGHTS POWER SUPPLY REF 757 AMM 33-51-07-2. OPS CHECK GOOD, OK FOR SERVICE.SDR FDEA202406120794Battery · no testDURING EMERGENCY EXIT LIGHT TEST R/H EXIT LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. R/H EXIT LIGHT OPS CHK SERVICEABLE. OK TO CONTINUE.SDR FDEA202403300423Battery Pack · inoperativeTHROUGHOUT MAINTANENCE DAILY CHECK FOUND L1 EMER EXIT SIGN DOOR 1 LT, FLT DECK DOME EMER LT MODULE, SLIDE LT DR 1 EMER INOP. SHGN 30MAR24 05:49 BNA WDM: CH 33-51-12 PG 13.1 SHEET 1FX1 PERFORMED T/S PROCEDURES TO EMERGENCY LIGHTS FORWAR LEFT SIDE L1 DSDR FDEA202403160300Girt Bar · out of alignmentL1 DOOR ESCAPE SLIDE BEGAN TO FALL OUT WHEN DOOR WAS OPENED FOR CREW STAIR MATING. DURING TROUBLESHOOTING FOUND LH DOOR AFT FLOOR FITTING MISALIGNED. RE-ALIGNED FITTING IAW AMM 25-66-10-2. REINSTALLED GIRT BAR ON LT DOOR AND OPS CHECKED PER THE ABOVE MANUALSDR FDEA202402210206Fitting · damagedDURING ACCOMPLISHED W/C EF-5730-E0340076 P11 STEP #3 PAGE 5 OF 13. FOUND #8 HOLE 2ND OVERSIZED. REMOVED & REINSTALLED #1 ENG IB & OB FAN COWLS, #1 PYLON BULLNOSE, IB TORQUE TUBE BTWN SLAT 4 & 5, Y-DUCT, LUBE FITTING, FUEL SUPPLY LINE & UPPER LINK IAW B757SDR FDEA202401240105Skin · dentedDENT FOUND AT FUSELAGE SKIN BTW STA 480-500, STR 22-R TO 23R. EVALUATED DENT ON FUSELAGE SKIN BETWEEN STA 480-500, STR 22R TO 23R FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-01-1A, FIG 101 DETIAL III, CUT DAMAGED AREA IAW B757 SRM 53-00- 01-2R PAR 4 D, PERSDR FDEA202401230102Skin · gougedMAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 497 1 1/8" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND IN LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINATINSDR FDEA202401230101Skin · gougedMAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 490 0.787" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND OUT OF LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINSDR FDEA202401190091Floor Panel · dentedMAIN CABIN FOUND DENTS ON FLOORBOARD PANEL #232 MJF BETWEEN STA 560 TO STA 680 RBL 58.22 TO RBL 63.5.SDR FDEA202208071908Frame · delaminatedLEFT ELEVATOR O/B UPPER SURFACE CONDUCTIVE FRAME IS DELAMINATED. REMOVED & REPLACED -7 ADAPTER PLATE IAW DWG 183N2003 REV G, -5 SPLICE PLATE & CONDUCTIVE FRAME IAW SRM 51-40-02 & DWG 183N2003 REV G & AMM 55-29-00-8.
Back to Boeing 757-2T7