Boeing 757-28A
Service difficulty reports · 2,000
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 = '75728A' 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 = '75728A' 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 NOCA01711Girt Bar · obstructedR1 DOOR SLIDE WILL NOT ARM. REMOVED DEBRIS FROM SLIDE GIRT BAR AREA, OPS CHECK NORMAL PER MM 25-66-11.SDR NOCA01611Idg · lowAIRCRAFT REJECTED TAKEOFF DUE TO GENERATOR DRIVE EICAS MSG AND WEATHER. PERFORMED BITE CHECK ON BPCU PER FIM 24-20-00 SERVICE IDG. NOTED, SERVICED IDG PER MM 12-13-03 ENGINE RUNS ACCOMPLISHED PER MM 71-00-00 NO FAULTS NOTED ALL PARMETERS NORMAL. ITEM NOW CLSDR FDEA201103070899Skin · misrepairedREPAIR BS 798 BETWEEN STR 15L-16L, INCORRECT SRM USED FOR INSTALLATION, REPAIRED IAW SRM 53-00-01, REPAIR 16 FIG 201 SHEET 1 THROUGH 6, CATEGORY "B" REPAIR RECURRENT INSPECTION IAW 53-00-01 FIG 201, TABLE V. MAJOR REPAIR.SDR NOCA01411Anti-Ice Valve · inoperativeEICAS MSG L ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI-ICE VALVE LIGHT REMAINED ILLUM. A/C DIVERSION TO JFK DUE TO ICING CONDITIONS AND PART AVAILABILITY. REPLACED LEFT ENGINE ANTI-ICE VALVE AS PER MM 30-21-03, OPS CHECK OK.SDR FDEA201103020824Frame · crackedAFT CARGO TA 1280 26R-25R FRAME HAS A CRACK. COMPLIED WITH E.A. F-5310-146259,8100-9 DATED MARCH 11, 2011- FIRST STAGE APPROVAL DTA 24 MONTHS. MAJOR REPAIRSDR FDEA201102250764Seat Track · damagedWHILE DRILLING P/N 11864182-21 AND -20 BL 0 AT STA 1438.0 SEAT TRACK SPLICES WERE MISDRILLED P/N 146N5178-1 AND 146N5185-U1. REPAIR ACCOMPLISHED IAW EA 757-5365-16-F3127 AND 8110-3 DATED JAN 30, 2011IN STMAE MOD CARD 118350557EZR07 REFERENCE EA F-5310-146387 SDR FDEA201102230700Frame · damagedMAIN CARGO DECK FRAME AT STA 1460 BETWEEN STR 2L TO 3L SEVERAL EXISTING TV MONITOR MOUNT AT HOLES DO NOT HAVE PROPER ED. REMOVED FRAME DAMAGE, FABRICATED NEW PARTS AND INSTALLED IAW SRM 53-00-07, FIG. 201. REPAIR NR 3 CAT "B" REPAIR WITH SUPPLEMENTAL INSSDR NOCA01011Circuit Breaker · openEICAS MSG EQ OVHT DISPLAY OVHT LIGHT ILLUMINATED. EICAS MSG EQ COOLING FAN DISPLAYED. OVHT LIGHT REMAINED ILLUMINATED WHEN ALT WAS SELECTED. T/S PER FIM 21-20-00 FIG 103, 105, FOUND AFT EXH EQ COOLING FAN 1 & 2 C/B OPEN. RESET SAME, OPS CHECK NORMAL PER AMSDR CA110215002O-Ring · damagedON FLIGHT THE ACFT EXPERIENCED A LARGE FUEL IMBALANCE IN CRUISE FLIGHT DUE TO A RT ENGINE FUEL LEAK. THE ACFT DECLARED AN EMERGENCY AND DIVERTED. WHEN THEY ARRIVED THE RT FUEL QUANTITY WAS 1500 KG LESS THAN THE LT. AN O-RING WAS FOUND LEAKING AT THE RT HP FSDR FDEA201102110546Skin · misrepairedREWORK OF SNRM N00090, REPAIR INSTALLED IAW INCORRECT SRM REPAIR REQUIRES REPLACEMENT. RT FUSELAGE EXT SKIN DENT AT STA 310 AND STR S23R. REMOVED EXT REPAIR AT STA 310 AND S23R IAW SRM 51-40-02, ACOMPLISHED REPAIR IAW SRM B757-200 SF 53-00-01. REPAIR 15,SDR FDEA201102110536Skin · misrepairedREPAIR INSTALLED IAW INCORRECT SRM. REPAIR REQUIRES REPLACEMENT. RT FUSELAGE EXTERNAL SKIN STA 520 BETWEEN S-24R TOS-25R. R & R REPAIR IAW SRM 53-00-01, REPAIR 15 B757-SF. OUTER ROW OF FASTNERS MUST BE INSPECTED EVERY 25,000 FC, CATEGORY "B" MAJOR REPAIR.SDR CA110211002Light · brokenFLIGHT CREW CONDUCTED A MISSED APPROACH AFTER THE RT MAIN GEAR DOWN AND LOCK GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR DOWN SELECTION. AN EMERGENCY WAS DECLARED AND ACFT LANDED WITHOUT FURTHER INCIDENT. MX FOUND THAT THE LIGHT WAS NOT TESTING AND CONCLUDED SDR FDEA201102080500Stringer · gougedSTA 278-270.5 S-23R HAS A GOUGE. NO ALLOWABLE DAMAGE FOR SPECIAL FREIGHTER EXIST. R & R S-23R AT STA 278-270.5 IAW SRM 51-40-02. FABRICATED STRINGER ON MAE TRAVELER T10/863577. CAT "A" MAJOR REPAIR.SDR FDEA201102040471Frame · misrepairedREWORK OF NR N01483, REWORK REQUIRED ON FRAME, STA 1280 BETWEEN S11R AND S13R DUE TO REPAIR INSTALLED IAW INCORRECT SRM. R & R REPAIR AT STA 1280, BETWEEN S11R AND S13R IAW SRM 53-00-07, FIG 201, DETAIL 1 REPAIR 3. MAJOR REPAIR.SDR FDEA201102040470Frame · misrepairedREWORK OF NR N01479, REWORK REQUIRED ON FRAME STA 1280 AT STRINGER 11L DUE TO REPAIR INSTALLED IAW INCORRECT SRM. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR SRM 53-00-07, FIG 201, DETAIL 1, REPAIR 3.SDR NOCA00911Landing Gear · damagedDUE TO SPEED TUG MALFUNCTION THE A/C NOSE GEAR SLIPPED OUT OF THE TOW UNIT. REPLACED NOSE GEAR AS PER JOB CARD 757-32-055-01.SDR NOCA00711Light · inoperativeEMERGENCY LIGHTS AREA LIGHT SEAT ROW 14D INOP. RELAMPED EMERGENCY LIGHT ROW 14D AS PER MM 33-51-05, OPS CHECK OK.SDR NOCA00611Bulb · burned outEMERGENCY EXIT LIGHT AT L2 DOOR INOP. REPLACED LIGHT AS PER MM 33-51-06, OPS CHECK OK.SDR NOCA00811Wire · looseADI CAPT'S BLANK SELECTING ALTN EFI DOES NOT CORRECT THE FAULT. T/S PER FIM TASK 34-22-00/ FIG 104. OPS NORMAL. INTERMITTENT FAILURE T/S PER WDM 34-22-16 CK'D CONDITION OF PINS CONNECTION BEHIND EADI & L SYM GEN PIN CONNECTIONS GOOD. REMOVED CAPT'S EADI & SDR NOCA00611AAdi · inoperativeACFT ABORTED TAKEOFF DUE TO LOST THE CAPT'S ADI (UPPER) DISPLAY.SDR NOCA00511Light · inoperativeINTERIOR EMERGENCY LIGHT ABOVE SEATS 1FD INOP. RELAMPED EMERGENCY LIGHT ABOVE SEAT 1FD OPS CHECK OK AMM 33-51-05.SDR NOCA00411Light · inoperativeRIGHT FWD PASS DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R1 DOOR EMERGENCY LIGHT OPS CHECK OK AMM 33-51-05.SDR NOCA0011Relay · defectiveAIR TURNBACK DUE TO EQUIPMENT OVERHEAT EICAS MSG DISPLAYED DURING TAKEOFF EICAS MSG EQPT OVHT DISPLAYED OVHT LIGHT ILLUMINATED. REPLACED EQUIPMENT VENT FAN RELAY K346 PER WDM. 21-58-21 OPS CHECK GOOD.SDR NOCA00111Relay · failedAIR TURNBACK , EICAS MESSAGE EQUIPMENT OVERHEAT DISPLAYED OVHT LGT ILLUMINATED, EICAS MESSAGE EQUIPMENT CLG FAN DISPLAYED. OVERHEAT LIGHT REMAINED ILLUMINATED WHEN ALTERNATE WAS SELECTED. EQUIPMENT CLG FLOW DISPLAYED ON GROUND. CIRCUIT BREAKERS FOR AFT EQUISDR FDEA201101040010Skin · gougedAFT CARGO DOOR, BELOW INTERNAL HANDLE, SKIN GOUGED. ACCOMPLISHED EA F-5230-146219, STEPS 1-8, AFT LOWER CARGO DOOR INNER SKIN GOUGED REPAIR, STA 1400, STR 25R. MAJOR REPAIR.SDR FDEA201101040009Tat Probe · failedIMMEDIATELY AFTER TAKE OFF, TAT PROBE, RT & LT ENG EEC EICAS MESSAGES. CHANGED RELAY K143, NR1 GROUND SENSE, R & R RELAY K-410, R & R K203 SYS 2 AIR/GROUND RELAY, VERIFIED NEW PROBE READS 26 OHMS. FOUND TAT PROBE READING OPEN. R & R TAT PROBE IAW MM 34-SDR NOCA07110Lamp · inoperativeL1 EMERGENCY LIGHT EXTERIOR INOP. RE-LAMPED EMERGENCY LIGHT, OPS CHECK OK PER AMM 33-51-00.SDR FDEA201012314787Skin · damagedLT WING NR 2 SLAT LOWER SURFACE FSS 635 WEDGE PUNCTURED REPAIRED NR2 SLAT LOWER WEDGE PUNCTURE IAW SRM 51-70-10, REPAIR 2. MAJOR REPAIR.SDR NOCA07410Brake Assy · lockedDURING REMOVAL NR 7 TIRE ASSY FOUND NR 7 BRAKE LOCKED. REPLACED NR 7 TIRE ASSY PER AMM 32-41-10-004-001 & REPLACED BRAKE PER 32-41-10-404-017 REF: FIM 32-42-00 FIG 110 SHEET 2 STEP 43. OPS CHECKS OK.SDR FDEA201012284759Frame · misrepairedSTA 1280, S-11L, FRAME REPAIR IS NOT IAW SRM INCOMING CONDITION. R & R FRAME IAW SRM 51-70-11, FIG 1 AND SRM 51-40-02. DTE REPAIR ASSESSMENT ON WO 00049137, N/R 00078. MAJOR REPAIRSDR FDEA201012284758Skin · dentedRT FUSELAGE EXT SKIN DENTED AT STA 1620 S-18R EVALUATED DENT AT STA 1620 S-18R A=.9 Y=.020 A/Y RATION 45. FOUND OUT OF LIMITS DUE TO PROXIMITY TO STR IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED DAMAGE IAW EA F-5330-146212. MAJOR REPAIR.SDR FDEA201012274754Frame · misrepairedFRAME REPAIR AT BS 1280 BETWEEN ST 11-13R NOT IAW SRM REQUIREMENTS. R & R FRAME IAW SRM 51-70-11 FIG 1 AND SRM 51-40-02. MAJOR REPAIRSDR NOCA07310Flashlight · inoperativeR2 F/A FLASHLIGHT INOP. REMOVED AND REPLACED R2 F/A FLASHLIGHT AS REQUIRED. OPS CHECK NORMAL.SDR FDEA201012214730Frame · damagedMAIN CARGO DECK FRAME AT STA 1360 STR S-2R, HAS EXISTING MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER ED'S. REMOVED FRAME FROM STA 1360 S6L TO S6R IAW SRM 51-40-02 RECIEVED THE REPAIR PARTS 1. PORTION OF FRAME TRAVLER T10/860856 2 CHANNEL T10/860858 2 CHANSDR FDEA201012214731Frame · damagedMAIN CARGO DECK FRAME AT STA 1360, STRINGER S-2L HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER ED'S. REMOVED FROME FROM 1360 S6L TO S6R IAW SRM 51-40-02 RECIEVED REPAIR PARTS 1 PORTION OF FRAME T10/860856 2 CHANNEL T10/960858 2 CHANNELS T10/86SDR FDEA201012214732Skin · dentedRT FUSELAGE EXT SKIN DENTED AT STA 231 BETWEEN S-23R TO S-24R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG III. REPAIRED DAMAGE AREA IAW EA F-5330-143238 DATED 12/14/10. FAA FORM 8100-9, DATED JAN 10, 2011, CATEGORY "B" MAJOR REPAIR.SDR CA101221006Heater · arced(CAN) DURING A FLIGHT, IN CRUISE AT FL350, ELECTRICAL ARCING WAS OBSERVED ALONG THE TOP OF THE R1 COCKPIT WINDOW HEATING ELEMENT (INTERNAL IN THE WINDOW). PER THE QRH THE WINDSHIELD HEAT WAS SELECTED OFF. APPROXIMATELY 2 MINUTES LATER THE OUTER (NON-STRUCTURALSDR FDEA201012154692Floor Support · corrodedCORROSION ON FLOOR MOUNT HOLES STA 1330 TO 1360, RBL62, MAIN CABIN. REMOVED CORROSION CHECK LIMITS ORIG MAT .070",L=2.0", W=0.80",D=.010" FOUND TO BE OUT OF LIMITS.REMOVED I/B CHORD, LOCATED DRILLED AND INSTALLED PART IAW SRM 51-40-02. MAJOR REPAIRSDR FDEA201012144662Crease Beam · corrodedCREASE WEG AT STA 1683, RBL 60 CORRODED ON UPPER SURFACE. CORROSION ON WEB AT STA 1683 RBL 60, BLENDED CORROSION AND CHECKED LIMITS IAW SRM 53-60-13, FIG 101,CORROSION FOUND TO BE OUT OF LIMITS. REMOVED WEB IAW SRM 51-40-02, RECEIVED NEW WEB PN 146N8723-2 ON SDR FDEA201012114635Skin · dentedRT FUSELAGE EXT SKIN DENT AT B STA 310 AND STRINGER S23R INSTALLED REPAIR DOUBLER AT STA 310, S23R DENT WAS OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. DOUBLER WAS FABBED FROM .071 2024-T3 BATCH NR 1941519. FILLER WAS .063 2024-T3, BATCH NR 1905681 SDR FDEA201012104630Floorbeam · corrodedCABIN FLOORBEAM BS 720 TOP SURFACE IS CORRODED ADJACENT TO L-2 DOOR SILL. ACCOMPLISHED STEP 1-7 OF EA -5310-143217 COMPLIANCE WITH FAA FORM 8110-3. MAJOR REPAIR.SDR FDEA201012094625Gate · chafedNR4 RT DOOR LOWER GATE SEAL SUPPORT STRUCTURE BOTH ENDS HAS CHAFED. BLENDED AREAIAW SRM 51-10-02 ,CHECKED LIMITS L=1.5,W=1,D=.060, FOUND TO BE OUT LIMITS IAW SRM 52-10-02 DETAIL V FIG 101. REMOVED DOOR GATE IAW SRM 51-40-02, RECEIVED NEW LOWER GATE P/N 146N6SDR FDEA201012074608Frame · damagedMAIN CARGO DECK FRAME AT STA 418 BETWEEN STRINGER S-1R HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER EDS. REPLACED FRAME AT STA 418 FROM RBL 2.5 TO TO LBL 2.5 IAW EA 757-5312-16-F3027. MAJOR REPAIR.SDR FDEA201012074607Frame · damagedMAIN CARGO DECK FRAME AT STA 1100, STRINGER S-2L HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE EDS. REMOVED AND INSTALLED STRINGER CLIP AT S-2L IAW SRM 51-40-02. CUT OUT FRAME FROM STR 1 TO STR 5L, IAW SRM 53-00-07, FOR SPECIAL FREIGHTER AND REPAIRESDR FDEA201012074606Frame · damagedMAIN CARGO DECK FRAME AT STA 1100, STRINGER S-2R HAS EXISTING TV MONITOR MOUNT HOLES THAT DOES NOT HAVE PROPER EDS. R & R STRINGER CLIP S2R IAW SRM 51-40-02. CUT OUT FRAME FROM STR 2R TO STR 5R, IAW SRM 53-00-07 FOR SPECIAL FREIGHTER AND REPAIRED IAW SRM 53-SDR CA101206015Panel · missingON ARRIVAL AFTER A FLIGHT, IT WAS NOTICED THAT INSP PANEL 443BR ON THE OTBD SIDE OF THE NR 2 ENGINE PYLON WAS MISSING. PANEL PN 311N5049-139, IPC 54-53-01-05, ITEM 175. THE PANEL WAS REPLACED. ACFT TSN 46089, CSN 14630. THIS IS THE SECOND PANEL TO GO MISSINGSDR FDEA201012044577Skin · dentedRT FUSELAGE EXTERNAL SKIN DENT BS 520 BETWEEN STRINGER 24R-25R. FABRICATED, INSTALLED DOUBLER & FILLER 2024-T3 BATCH 0001928869 .063 &2024-T3 .056 BATCH 0001383027 IAW SRM 53-00-01 REPAIR 2 THRESHOLD INSPECTION OF REPAIR DOULBER TO OCCUR ON OR BEFORE 37,50SDR FDEA201012014533Seat Track · corrodedSEAT TRACK CROWN AT LBL 45 STA1080-1180 HAS SEVERALAREAS OF CORROSION AND GOUGES. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. ORIGINAL MATERIAL .550 MATERIAL REMOVED .050 MATERIAL REMAINING .500 .FOSDR FDEA201012014532Seat Track · corrodedSEAT TRACK CROWN AT RBL 45, STA 1080-1180 HAS SEVERAL AREAS OF CORROSION AND GOUGES FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101, FABRICATED NEW SEAT TRACK P/N BAC 1520-792 IAW SRM 53-40-02, LOCATED AND DRILLED IAW SRM 51-40- 05,SDR CA101202003Panel · missingON ARRIVAL AFTER A POSITIONING FLIGHT FROM MANCHESTER, UK, IT WAS NOTICED THAT INSPECTION PANEL 443HL ON THE INBOARD SIDE OF THE NR 2 ENGINE PYLON WAS MISSING. PANEL P/N 311N5049-155, IPC 54-53-01-05, ITEM 208. THE PANEL WAS REPLACED. AIRCRAFT TSN 46050, CS
Back to Boeing 757-28A