Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA202010062423Strap · crackedCOURIER AREA STA 350 LBL 25 LOWER SUPPORT STRAP LOWER SURFACE IS CRACKED. REMOVED EXISTING STABILIZATION STRAP REPAIR BETWEEN STA 345 TO STA 377 LBL 25, IAW B757 SRM 51-40-02-OG. FABRICATED AND INSTALLED NEW STABILIZATION STRAP REPAIR AND FILLER SECTION, IAWSDR FDEA202010062422Strap · crackedUPON REMOVE LOWER STRAP (STABILIZATION) FOUND INTERCOSTAL PREVIOUS REPAIR CRACKED BETWEEN BS 350 TO BS 365.5 ON LBL 24.750. REMOVED INTERCOSTAL BETWEEN STA 350 TO STA 365.5 LBL 24.75, IAW B 757 SRM 51-40-02-OG. FABRICATED AND INSTALLED NEW INTERCOSTAL, IAW BSDR FDEA202010052420Floorbeam · damagedMAIN CABIN FLOOR PANEL SUPPORT HAS PULLED RIVETS THRU UPPER SHIM AT BS 1055 LBL 24.75 TO 45.5. REMOVED AND FABRICATED, INSTALLED NEW FLOOR SUPPORT (PLATE) AT STA 1055 BETWEEN LBL 24.75-LBL 45.5, IAW B 757 SRM 51-40-02-OG, 51-40-05-OG AND BOEING DWG 144N5070 RSDR FDEA202010052419Floorbeam · crackedMAIN DECK STA 900 BETWEEN LBL 24.75-LBL 44.5 FLOOR SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT (PLATE) STA 900 BETWEEN LBL 24.75-LBL 44.5, IAW B 757 SRM 51-40-02-OG, 51-40-05-OG AND BOEING DWG 144N5070 REV W AND REV B.SDR FDEA202010042414Crease Beam · corrodedMAIN DECK BETWEEN STA 1020-1040 RT CREASE BEAM CORRODED. REMOVED CORROSION AT CREASE BEAM STA 1020-1040 RT SIDE, IAW B 757 SRM 51-10-02-OG, ORIGINAL MAT .070", MINIMUN REMAINING .022". MAT LOSS .048" FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG SDR FDEA202010022400Slide · unwanted deployAFTER BLOCK IN, 1R DOOR SLIDE DEPLOYED WHEN GROUND CREW OPENED DOOR. INSTALLED NEW SLIDER ON GIRTBAR AND TARGET, IN REF TO 757 AMM 25-66-01-4. OPERATIONS CHECK DOOR ARM LIGHT IS GOOD.SDR FDEA202010012384Frame · crackedHFEC SURFACE INDICATION OF DEFECT(CRACK)NOTED AND MARKED IN RED SHARPIE ON FUSELAGE MAIN FRAME 1640RIGHT HAND SIDE INNER CHORD FWD RETURN FLANGE RADIUS INLINE WITH STRINGER 14R. INDICATION RUNS FROM EDGE OF FLANGE UNDER STRAP TO SINGLE FASTENER ATTACHED SDR FDEA202009172238Skin · delaminatedLT WING OUTBOARD FLAP UPPER TRAILING EDGE PANEL HAS DELAMINATED AREA AT WS 495.SDR FDEA202009172240Skin · delaminatedRT WING OB MAIN FLAP EXTERNAL AREA T/E HAS ONE DENT. UPON FURTHER EVAL FOUND 1/2" DENT DELAMINATED, IAW B757 SRM 51-10-06-2R. ACCOMPLISHED REPAIR ON RT WING O/B MAIN FLAP EXTERNAL AREA T/E AT WS 560-565, IAW B757 SRM 57-53-01-2R REP 1 TABLE III SRM 51-70-07-SDR FDEA202009172239Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 475. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III AND B757 SRM 51-70-07-06 PARAG 5B AND B757 SRM 51-70-17-0G PARAG 3G AT WS 475.SDR FDEA202009172237Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 495. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III SRM 51-70-07-0G PAR 5B AND SRM 51-70-17-0G PAR 3G AT WS 495.SDR FDEA202009172236Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 595. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III SRM 51-70-07-0G PAR 5B AND SRM 51-70-17-0G PAR 3G AT WS 595.SDR FDEA202009142210Skin · crackedMAIN CARGO DOOR FWD VENT DOOR BOX INTERIOR SKIN HAS PROTUDING DENT WITH VISUAL CRACK. REMOVED, FABRICATED, AND REPLACED PANEL ON MAIN CARGO DOOR FWD VENT DOOR BOX INTERIOR SKIN (PANEL), IAW B757 SRM 51-40-02-0G AND B DWG 65-49309, REV D AND REV H.SDR FDEA202009122187Seat Track · corrodedMAIN DECK STA 1180 RBL 24.75 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION ON SEAT TRACK FLANGE AT STA 1180, RBL 24.75 IAW B757 SRM 51-10- 02-0G. EVALUATED DAMAGED AREA, ORIG. MAT=.070", REM. MAT= .032" MAT LOSS= .038" FOUND TO BE OUT OF LIMITS, IAW B757 SSDR FDEA2020091422188Light · inoperativeNO NOSE GEAR LIGHT AFTER GEAR WAS IN DOWN PISITION. R & R NOSE GEAR POSITION INDICATION MODULE, REF SMP'S AND IPC 33-14-70-03 & 32-61-51-01. MANUFACTURER KORRY P/N 674-1043-3205. OPS CHECK NORMAL. AC OK FOR SERVICE.SDR FDEA2020090952126Nozzle · crackedNR 2 ENGINE EXHAUST NOZZLE 9 O'CLOCK POSITION MOUNT FLANGE CRACKED. REPAIRED NR 2 ENGINE EXHAUST NOZZLE 9 O'CLOCK POSITION MOUNT FLANGE, PER CMM 78-11-01 REP 2-1.SDR FDEA202009092066Fairing · crackedTAIL SECTION LT LOWER HORIZONTAL STAB SEAL FAIRING DENTED/CRACKED. REPAIRED TAIL SECTION LT LOWER HORIZONTAL STAB SEAL FAIRING, IAW FEDEX EA NR F-5350- T0356088-P1 FUSELAGE-AERODYNAMIC FAIRINGS-LT HORIZONTAL STABILIZER TO BODY LWR BLADE ASSY DAM.SDR FDEA2020083192068Floor Support · corrodedCORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER FLANGE , APPROX BS.738 RBL.7.5 DOT 129-047 REMOVED CORR ON INTERCOASTAL APPROX STA 738 RBL7.5 IAW B757 SRM 51-10-02-0G. UPON EVAL FOUND INTERCOASTAL TO BE WRONG MATERIAL IAW BOEING DWG 143N5367 REVSDR FDEA2020083192066Fairing · crackedTAIL SECTION L/H LOWER HORIZONTAL STAB. SEAL FAIRING DENTED/ CRACKED. REPAIRED TAIL SECTION L/H LOWER HORIZONTAL STAB SEAL FAIRING IAW FEDEX EA# F-5350- T0356088SDR FDEA202008272044Angle · crackedNR 2 PYLON 445BL HAS A CRACKED CLIP. REMOVED, FABBED, AND REPLACED NEW CLIP IAW BOEING DWG 313N5022 REV AB.SDR FDEA202008272043Barrier · crackedNR 2 ENGINE INBOARD UPPER PYLON FWD AREA JUST ABOVE THE INBOARD T/R PLASTIC SHIELD IS CRACKED IN TWO PLACES. REPAIRED NR 2 ENGINE INBOARD AFT FLUID BARRIER ON 2 EA AREAS, IAW FEDEX EA F-5450-T0356144-P1, NACELLES/PYLON - WING PYLON/STRUT NR #2 (RT) PYLON INBOSDR FDEA202008262035Bracket · crackedRT WING FUEL DOOR SWITCH BRACKET CRACKED STREAMER ATTACHED. REMOVED AND REPLACED BRACKET PER BOEING DWG NR 284N1138 AND B757 SRM 51-40-02.SDR FDEA202008252021Floorbeam · corrodedCABIN FLOOR BEAM CORRODED BS 375, BL354L. REMOVED CORROSION IAW B757 SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A. ACCOMPLISHED FLOOR BEAM REPAIR IAW FEDEX EA "F-5310-T0356115-P1. FUSELAGE-MAINFRAME, MAIN CABIN FLOOR BEAM STA 377SDR FDEA202008252019Seat Track · corrodedCABIN SEAT TRACK CORRODED BS 342- BS 372, BL 7L REMOVED CORROSION AS REQUIRED IAW B757 SRM 51-10-02. MAX ALLOWABLE MAT REMOVAL .020, REMOVED .030. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DET "I". FABRICATED NEW SEAT TRACK AND INSTALLED ISDR FDEA202008252020Seat Track · corrodedCABIN SEAT TRACK CORRODED BS 365, BL 44R - BL 47R. ACCOMPLISHED EA# F-5310-T0356090-P1 FUSELAGE - MAINFRAME - SEAT TRACK - STA 365 - RBL 45.50 - CORROSION.SDR FDEA202008221981Battery Pack · failedDURING PREFLIGHT FOUND R1 EMERGENCY EXIT EXTERIOR LIGHT INOPERABLE. REMOVED & REPLACED BATTERY ASSEMBLY, AS REQUIRED. R1 DOOR EMERGENCY EXIT LIGHTS GROUNND CHECKK NORMAL, REF 757 AMM 33-51-07.SDR FDEA2020082621983Floorbeam · corrodedFLOOR BEAM NUTPLATE IS CORRODED BS 1681-RBL47. REMOVED NUTPLATE BRACKET IAW B757 SRM 51-40-02. MAT ID 7075-T6 ALUMINIUM SHEET PO NR 964704.1, IAW BOEING PL 146N5693 REV C AND BOEING DWG 146N5693 REV B. FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV B.SDR FDEA2020082521981Battery Pack · inoperativeDURING PREFLIGHT FOUND R1 EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED & REPLACED BATTERY ASSY AS REQUIRED, R1 DOOR EMERGENCY EXIT LIGHTS GRND CK NORMAL IAW AMM 33-51-07.SDR FDEA202008211964Lamp · inoperativeCOCKPIT EMERGENCY LIGHT INOP. REPLACED LAMP AND TESTED GOOD IAW AMM: 33-51-09-3 REPLACED LAMP AND TESTED GOOD IAW AMM: 33-51-09-3 LAMP P/N 1317SDR FDEA202008201947Seal · cracked#1 ENG EXHAUST NOZZLE O/B UPPER SPRING LEAF CRACKED REMOVED AND REPLACED SPRING LEAF PER B757 SRM 51-40-02-0G AND REF IPC 78-11-01-03SDR FDEA2020082091939Bulkhead · cracked#2 PYLON HYDRAULIC BAY,AFT OF BULKHEAD THE OTBD LWR FWD CORNER ATTACH CLIP IS CRACKED REMOVED AND REPLACED CLIP PER BOEING DWG #313N3052SDR FDEA202008181925Transmitter · failedTE FLAP ASYM EICAS MESSAGE. TE FLAPS STOPPED AT 2.5 DEGREES. COMPLIED WITH QRH IAW AMM 27-58-01-5. R & R THE RT TRAILING EDGE FLAP POSITION TRANSMITTER, OPS CHECKED OK, ALL INDICATIONS CHECKED NORMAL. NO HISTORY.SDR FDEA2020080711743Intercostal · damagedFUSELAGE SKIN BULGED FROM BS 1420 TO 1440, AT INTERCOSTAL BETWEEN STRINGERS 28R AND 29R. REMOVED, FABRICATED, AND INSTALLED THE NEW INTERCOSTAL IAW DWG 146N5398, REV P, A , DWG 146N5425 REV -, AND SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN SDR FDEA2020080511743Intercostal · unknownFUSELAGE SKIN BULGE FROM BS1420 TO BS1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P , A , SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE INTERCOSDR FDEA2020080311743Intercostal · damagedFUSELAGE SKIN BULGE FROM BS 1420 TO BS 1440 AT INTERCOSTAL BETWEEN S-29R AND S-28R. REMOVED FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS1420-1440 STR28R-29R IAW DWG 149N5398 REV P , A , B757 SRM 51-40-02-0G. EVALUATED AREA OF DAMAGE AND FOUND HOLES IN THE SDR FDEA2020072761663Attach Angle · crackedLEFT LOWER SIDEWALL ATTACH ANGLE AT BS 640 CRACKED. REMOVED AND REPLACED THE ANGLE IAW DWG 453N1131 AND SRM 51-40-02.SDR FDEA2020072751649Battery Pack · failedEMERGENCY BATTERY PACK DOES NOT HOLD CHARGE. REMOVED, REPLACED, AND OPS CHEC KED GOOD EMERGENCY LIGHT BATTERY PACK M730 PER B757 AMM 33-51- 07-2.SDR FDEA2020072431635Bracket · crackedLEFT PYLON,UNDER PANEL 435AR FWD LOWER CORNER HAS BRACKET CRACKED REMOVED AND REPLACED ATTACH ANGLE PER B757 SRM 51-40-02 AND DWG #313N3052 REV BSDR FDEA202007211612Rivet · wrong partDURING AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR ON LEFT WING OUTBOARD MAIN FLAP LEADING EDGE SKIN DOES NOT MEET CURRENT SRM STANDARDS DUE TO INCORRECT RIVET SPACING,CUTOUT ORIENTATION,AND REPAIR PARTS USEDSDR FDEA2020072311603Seat Track · corrodedMAIN CABIN, FWD RIGHT WET AREA, SEAT TRACK CORRODED BS 365 - 377 RBL 45 COMPLIED WITH EA F-5310-T0355330.SDR FDEA202007211610Seat Track · corrodedMAIN CABIN, FWD L/H WET AREA, LBL7 SEAT TRACK CORRODED TAPED AREAS ON SIDE OF TRACK 345 - 379 REMOVED CORROSION, ORIGINAL THICKNESS .072" MATERIAL REMOVED .018", REMAINING .054", OUT OF LIMITS OF B757 SRM 53-10-52-01, FABRICATED SEAT TRACK IAW VENTURA SDR FDEA202007201587Plate · corrodedMAIN CABIN, FWD RT WET AREA, CORROSION AT O2 LINE FEED THROUGH BS 375, RBL 37. REMOVED O2 LINE IAW AMM 53-11-00-2 & 20-11-00-2. REMOVED O2 PLATE IAW SRM 51-40-02. FABRICATED A NEW O2 PLATE IAW DWG 3516, REV -. INSTALLED THE NEW O2 PLATE IAW DWG 3516 REV - &SDR FDEA2020072301587Line · corrodedMAIN CABIN, FWD RT WET AREA, CORROSION AT O2 LINE FEED THROUGH STA 375 RBL 37 REMOVED O2 LINE IAW AMM 53-11-00-2 AND 20-11-00-2. REMOVED O2 PLATE IAW SRM 51-40- 02. FABRICATED NEW O2 PLATE IAW DWG 3516 REV -. INSTALLED NEW O2 PLATE IAW DWG 3516 REV - AND SRM SDR FDEA2020072391584Bracket · crackedR/H PYLON PANEL O/B INSIDE PANEL 445BR BRACKET FOR CONDUIT CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 313N3033 REV D AND B757 SRM 51-40-02SDR FDEA202007191583Bracket · crackedR/H PYLON I/B PANEL 445AL CONDUIT INSIDE FWD BRACKET CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 313N3053 REV E AND SRM 51-40-02SDR FDEA202007171569Nut Plate · corrodedMAIN CABIN, FWD R/H WET AREA, FLOOR BAEM CORRODED AT NUT PLATES STA 325 RBL 35-58 REMOVED CORROSION ORIGINAL THICKNESS .120 REMOVED .011 NEW THICKNESS .109 WICH IS FOUND TO BE WITHIN LIMITS WICH IS FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-10-08-1A AND BOESDR FDEA202007171568Seat Track · corrodedMAIN CABIN, FWD RT WET AREA HAD CORROSION ON THE SEAT TRACK, BS 365 - 379, RBL 25. REMOVED CORROSION, ORIGINAL THICKNESS .070, REMOVED MATERIAL .009, REMAINING .061 FOUND WITHIN LIMITS IAW SRM 53-00-52--1A, DETAIL 7, DWG 1520- 792 AND SRM 53-10-52-01,SDR FDEA202007171566Skin · puncturedLEFT HORIZONTAL STAB LOWER SURFACE SKIN WAS A PUNCTURED APPROX. 5 INCHES LONG, APPROX. 5 INCHES FROM THE LEADING EDGE. REPAIRED HORIZONTAL STAB LOWER SKIN BY REMOVING DAMAGE, LAYING UP CORE PLUG AND EXT. DOUBLER REPAIR AND CURED IAW SRM 55-10-01 AND SRM 51SDR FDEA202007161533Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8 LBL 4. REMOVED AND REPLACED FLOOR BEAM LOWER NUTPLATE STRIP AT BS 1681.8 LBL 4, IAW FEDEX B757 SRM 51-40-02 AND DWG 146N5693 REV C.SDR FDEA2020072461538Seat Track · corrodedRH SEAT TRACK RBL 58.22 LIGHT SURFACE CORROSION AROUND NUT PLATES AT FS 1180R. REMOVED CORROSION AT SEAT TRACK RBL 58.22 STA. 1180 AND STA. 1300 AND FOUND TO BE OUT OF LIMITS IN BOTH LOCATIONS IAW B757 SRM 53-00-52-1A FIG 101 DET VII AND DET I, CUT OUT SEC
Back to Boeing 757-222