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 FDEA202212172938Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MBF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222MBF IAW FEDEX DWG SRZ-25-005 REV R.SDR FDEA202212172937Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 221MAF IS DELAMINATED FABRICATED NEW FLOOR PANEL 221MAF IAW DWG SRZ-25-005 REV R.SDR FDEA202212172936Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MAF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222MAF IAW FEDEX DWG SRZ-25-005 REV RSDR FDEA202212172935Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MEF DELAMINATED. FABRICATED NEW FLOOR PANEL 222MEF IAW FEDEX DWG SRZ-25-005 REV R.SDR FDEA202212162933Handle · crackedFWD PIT CARGO DOOR EXTERIOR HANDLE IS CRACKED ON LOWER EDGE REMOVED AND REPLACED PER DWG 140N2789.SDR FDEA202212152916Cover Plate · bentINTERNAL FUSELAGE ABOVE WING CENTER SECTION UNDER MAIN CARGO FLOOR HAS LOOSE AND BENT FLOOR SUPPORT AT BS1020 RBL24.75-45.50 REMOVED, FABRICATED AND INSTALLED NEW COVER PLATE ON FLOOR SUPPORT IAW B757 DWG 114N5081 REV C AND DWG 114N5070 REV B.SDR FDEA202212152915Floor Support · damagedINTERNAL FUSELAGE ABOVE WING CENTER SECTION BELOW MAIN CARGO FLOOR HAS A DENT AND A CRACK ON FLOOR SUPPORT AT STA 900 LBL 24.75 REMOVED - FABRICATED AND INSTALLED NEW COVER PLATE ON FLOOR SUPPORT IAW DWG# 114N5081 REV C AND DWG 114N5070 REV ESDR FDEA202212152912Lamp · failedR1 DOOR SLIDE LIGHT INOP ON PREFLIGHT. REPLACED THE LAMP. OPS CHECKED GOOD IAW AMM 33-51-06-2-1.SDR FDEA202212142913Slide · damagedMDIS 770 52-10 6691 14DEC22 MEM OPEN U HUB REPORTS L1 DOOR ESCAPE SLIDE GREEN STATIC LINE PULLED OUT TO MAX EXTENSION ABOUT 6 FEET. SHGN 14DEC22 22:25 MEM U AMM: 25-56-01-4-0 UNABLE TO REINSTALL THE STATIC LINE, SECURED STATIC UNDER SLIDE SDR FDEA202212142909Rack · crackedE3-2 SHELF, SIDERAIL IS CRACKED AT ATTACHMENT HOLE REPAIRED E3-2 SHELF SIDERAIL ATTACHMENT HOLE IAW FEDEX DRAWING NUMBER SRZ-53-007, REV -.SDR FDEA202212142908Rack · crackedE2-3 SHELF, SIDERAIL IS CRACKED AT ATTACHMENT HOLE REPAIRED E2-3 SHELF SIDERAIL ATTACHMENT HOLE IAW FEDEX DRAWING NUMBER SRZ-53-007, REV-.SDR FDEA202212072883Floorboard · delaminatedZONE 220 FLOORBOARD 221MBF IS DELAMINATED. FABRICATED ZONE 220 FLOORBOARD 221MBF ON TRAVELER T22/1649009 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202211282850Floorbeam · crackedFWD PIT CEILING AREA STA 580 FLOOR BEAM UPPER CAP AFT SIDE FLANGE RADIUS HAS SUSPECTED CRACK, APPROX LBL 45. FLOOR BEAM WAS REPAIRED AND NEW ANGLE & RADIUS STRAP INSTALLED ON FWD PIT CEILING AREA STA 580 AT LBL 45 IAW DRAWING SR57-53-004 & SRM 51-40-02. MASDR FDEA202211212824Access Panel · corrodedLEFT WING FUEL TANK PANEL 541EB IS CORRODED. REPLACED FUEL TANK DOOR 541EB WITH NEW P/N 112N6101-5,SDR FDEA202211162800Floorbeam · crackedDOT(137-16) MAIN CABIN FLOOR BEAM AT STA 580 LBL 45 HAS CRACK. COMPLIED WITH EA # F-5310-T0371523 P1 FUSELAGE-MAINFRAME-FLOOR BEAM AT STA 580 AND LBL 45 CRACKED- REPAIR PER DRAWING SR57-53-004 WITH MINOR DEVIATION, MAJORSDR FDEA202211162799Deck Plate · corroded(DOT 38-38) MAIN CABIN AFT FLOOR STRUCTURE UPPER SKIN STA 1682 TO STA 1710 SURFACE CORROSION LBL 55 TO RBL55. REMOVED CORROSION, REPAIRED AREA IAW SRM 53-60-51-2R, RESTORED ACCESS, MAJOR REPAIR.SDR FDEA202211022715Attach Angle · cracked#2 PYLON AFT FAIRING O/B SIDE , FWD LOWER ATTACH CLIP IS CRACKED AT APPROX. NAC STA 206 REMOVED AND REPLACED CLIP AT #2 PYLON AFT FAIRING O/B SIDE , FWD LOWER AREA AT APPROX. NAC STA 206 IAW FEDEX EA : F-7120-T0371303 -P1SDR FDEA202211012705Sensor · failedLE SLAT ASYM MESSAGE ON DEPARTURE BETWEEN FLAPS 1 AND UP. RAN QRH AND COMPLIED WITH CHECKLIST. DECLARED EMERGENCY AND RETURNED TO MCI. REST OF FLIGHT WAS UNEVENTFUL. EMERGENCY DECLARED AMM: 27-81-41-4 REMOVED AND REPLACED LOSS SENSING SWITCH FOR THE ISDR FDEA202211012706Attach Angle · crackedRH WING MLG SUPPORT BEAM AFT SIDE, LOWER FIXED TRAILING EDGE PANEL ATTACH ANGLE IS CRACKED JUST ABOVE AFT MLG TRUNNION FITTING. FABRICATED AND REPLACED THE ATTACH ANGLE (BRACKET, P/N 113N1685-23) ON THE R/W LOWER FIXED T/E O/B SIDE, JUST ABOVE THE AFT MLG SDR FDEA202210312700Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251MXF HAS DELAMINATION ON LOWER SIDE REPAIRED DELAMINATION ON FLOOR PANEL 251MXF IAW B757 SRM 53-00-50-2R, REPAIR 1, PARA. 3.B. AND FIG. 201, SHEET 2. INSTALLED INSERTS IN REPAIR AREA IAW B757 SRM 53-00-50-2R, REPAIR 2, FIG. 201, SHSDR FDEA202210282689Battery Pack · no testMULTIPLE EMERGENCY EXIT LIGHTS FAIL TO TEST. ALL LIGHT ASSOCIATED WITH EMEGENCY LIGHTS POWER SUPPLY M730. REPLACED BATTERY PACK AT POWER SUPPLY M00730. RADIANT ILLUMINATION INC MPN 2013-1A S/N 18185. VERIFIED CHARGER OUTPUT GOOD. EMERGENCY LIGHT OPS CKS GOOSDR FDEA202210282687Stringer · crackedAFT CARGO COMPARTMENT STA 1680-1701 STR29R HAS CRACKED STINGER REMOVED CRACKED STINGER SECTION ON STA 1680 - 1701 STR29 R/H FABRICATED -1 HAT SECTION AND -2 FILLER INTALLED IAW B757 SRM 53-00-03-2RSDR FDEA202210282686Shim · corrodedNO. 2 ENGINE, INLET COWL, FWD PANEL LAND IS CORRODED BETWEEN 6 & 8 O'CLOCK POSITIONS REMOVED AND REPLACED 6 EA. SHIMS, NUMBER 2 ENGINE INLET COWL FWD LOWER LAND IAW BAC DWG 314N3010, REV. L AND B757 SRM 51-40-02-0G. CORROSION WAS FOUND TO BE ON PANEL LANSDR FDEA202210252663Plate · damagedEVALUATED PREVIOUS REPAIR FROM OPERATORS' RECORDS FOR CONFORMITY: EXISTING REPAIR LOCATED IN THE MAIN CABIN, AFT DECK WEB FILLER REPAIR, STA 1680-1690, RBL 45 TO RBL 60 EVALUATED EXISTING REPAIR LOCATED ON THE MAIN CABIN AFT DECK WEB, STA 1680-1690, RBL SDR FDEA202210252662Drag Fitting · crackedHOLES 3, 14, 17 ON #2 PYLON DRAG FTG HAVE CORROSION INDICATION. REPLACED RH WING UPPER OUTBD DRAG FITTING IAW FEDEX EA F-5730-T0371231-P1.SDR FDEA202210252661Drag Fitting · crackedHOLES #1 & #7 HAVE CRACK INDICATIONS IN THE BOTTOM OF FITTING. REPLACED RH WING UPPER INBD DRAG FITTING IAW EA F-5730-T0371231-P1.SDR FDEA202210252659Drag Fitting · crackedHOLE #3HAS CORROSION INDICATIONS IN FITTING, HOLE # 8 HAS CRACK INDICATION IN FITTING APPROX .0625" FROM BOTTOM OF HOLE AT THE 5-6 O'CLOCK POSITION LOOKING FORWARD, SIZE OF INDICATION APPROX .030. REPLACED LH WING, UPPER INBD DRAG FITTING IAW FEDEX EA # FSDR FDEA202210242654Floor Support · corrodedMAIN CABIN SEC 46 FLOOR SUPPORT STRUCTURE (CHANNEL) IS CORRODED AT 2EA NUT PLATES AT APPROX STA 1675 AT BL 0 REMOVED AND REPLACED FLOOR SUPPORT ( CHANNEL ) IAW BAC DWG 146N5230, REV BSDR FDEA202210242653Crease Beam · gougedDURING AGING AIRCRAFT INSPECTION, FOUND EXISTING CREASE BEAM WEB REPAIR WITH A GOUGE AT A FASTENER HOLE, STA 1397, RBL 69 REMOVED & REPLACED CREASE BEAM WEB IAW BAC DWG 146N5590, REV BSDR FDEA202210222643Fitting · corrodedLT WING PYLON DRAG LINK FITTING HAS CORROSION IN 5EA HOLES IN FITTING LAYER ONLY. HOLE NUMBERS 1,3,8,10, AND 15. COMPLIED WITH EA F-5730-T0370901 PT1 WINGS - PLATES AND SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS. THIS EA DEVIATES FROM EO F-5730-E034007SDR FDEA202210212635Floorboard · crackedMAIN CABIN SEC 46 FLOOR BOARD 251MJF IS CRACKED AT THE FWD OTBD CORNER RPEIARED MAIN CABIN FLOOR BOARD 251MJF IAW B757 SRM 53-00-50-2R, REPAIR 1. ORIG SUBMISSION DATE: 10/24/2022SDR FDEA202210212636Floorbeam · crackedVIEW FROM FWD CARGO COMPT. MAIN CARGO FLOOR BEAM AT BS 580 LBL 45 HAS CRACK. REPAIRED FLOOR BEAM AT STA 580 LBL 45 IAW EA TF-5310-T0370825 PT1. FUSELAGE - MAINFRAME- FLOOR BEAM AT STA 580 AND LBL 45 CRACKED - REPAIR PER DRAWING SR57-53- 004. MAJOR REPAIRSDR FDEA202210212634Floor Support · corrodedMAIN DECK FLOOR FS1681. FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION EXFILIATED BETWEEN WEB AND FLOOR BEAM APPROX LBL12. REPAIRED MAIN DECK FLORO FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION FROM LBL 3 TO LBL 20 IAW SRM 53-60-51-2R. CORROSION FOUND OUT OSDR FDEA202210212633Attach Fitting · corroded#2 ENGINE PYLON DRAG LINK ATTACHMENT FITTING HAS 8 HOLES WITH CORROSION. HOLES 2,3,5,7,10,14. AND 15 IN FITTING LAYER. HOLE 8 HAS CORROSION IN SKIN LAYER. COMPLIED WITH EA F-5730-T03700894 PT1 R/H WING UPPER SKIN AT DRAG FITTING CORROSION FINDINGS. THISSDR FDEA202210192623Floorboard · delaminatedZONE 20 FLOOR BOARD 222MAF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1638358 IAW DWG SRZ- 25-005 REV R. MAJOR REPAIRSDR FDEA202210192622Floorboard · delaminatedZONE 220 FLOOR BOARD 221MBF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1638356 IAW DWG SRZ-25-005 REV R. MAJOR REPAIRSDR FDEA202210192621Floorboard · delaminatedZONE 220 FLOOR BOARD 222AF IS DELIAMINATED FABRICATED ZONE 220 FLOOR BOARD 222AF ON VT MAE TRAVELER T22/1638359 IAW DWG SRZ- 25- 005 REV R. MAJOR REPAIRSDR FDEA202210192619Floorboard · delaminatedZONE 220 FLOOR BOARD 221AF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1638355 IAW DWG SRZ- 25- 005 REVISION R. MAJOR REPAIRSDR FDEA202210122752Light · failedON FINAL APPROCH WE SELECTED THE GEAR DOWN. RECEIVED 2 GREEN MAIN GEAR LIGHTS AND THE NOSE GEAR LIGHT REMAINED DARK. PRESSED TO TEST THE NOSE GEAR LIGHT AND HALF OF IT LIT UP GREEN. THIS LED TO THE GEAR DISAGREE CHECKLIST AND MANUALLY LOWERED THE GEAR. DSDR FDEA202210072514Wedge · delaminated#6 SLAT REQUIRES REPLACEMENT DUE TO T/E WEDGE DELAMINATION FOUND ON FEDEX E.O F- 5750-E0336930-P6 REPAIRED #6 SLAT T/E WEDGE IAW FEDEX EA# F-5750-T0370813-P1 - WINGS - FLIGHT SURFACES - #6 SLAT, TRAILING EDGE WEDGE, ISS 193, DELAMINATIONSDR FDEA202210062499Angle · cracked**PARTS RACK ITEM** R/W FLAP FAIRIG 672HB HAS A BENT FORWARD R/H CLOSEOUT ANGLE REPAIRED R/W, I/B FLAP FAIRING 672HB FORWARD R/H CLOSEOUT ANGLE IAW FEDEX EA # F-5720-T0370931- P1, TITLED "WING - SECONDARY WING STRCT - RH INBD FLAO FAIRING, 672HB, INBD AND OUTSDR FDEA202210042463Floor Support · corrodedMAIN CABIN, FLOOR SUPPORT AT STA 1640 TO 1660, LBL 55 HAS CORROSION AROUND NUT PLATES. BLENDED CORRODED AREAS IAW B757 SRM 51-10-02-0G. ORIGINAL MATERIAL THICKNESS OF .071" IAW B757 SRM 53-60-13-0I, FIG. 1, DETAIL VII. REMOVED .003" FOR REMAINING THICKNESSSDR FDEA202210022453Floorboard · delaminatedCOURIER AREA FLOOR BOARD 221MBF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VTMAE TRAVELER T22/1637405 IAW DWG. SRZ- 25-005 REV. R MAJOR REPAIR.SDR FDEA202210012439Floor Panel · crackedMAIN CABIN, FLOOR PANEL 251MVF IS CRACKED AND HAS AREAS OF DISBOND ON LOWER SIDE REPAIRED FLOOR PANEL 251MVF IAW BAC D6-55191, REV. C, AND B757 SRM 53-00-50-2R, REPAIR 2, FIG. 201, SHEET 1 AND PARA. 4.A., AND VT MAE DWG 11864182, REV. ASDR FDEA202209302420Shear Web · corrodedMAIN CABIN, AFT FLOOR, SHEAR WEB HAS SEVERAL, AREAS OF CORROSION, STA 1681 TO 1720, LBL 56 TO RBL 56 REPAIRED THE AFT MAIN CABIN SHEAR WEB (DECK PLATE), STA 1681 TO 1720, LBL 56 TO RBL 56, IAW FEDEX E.A. F-5310-T0370865-P1, RELEASE DATE: 29 SEPTEMBER, 2022SDR FDEA202209292396Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251MWF HAS AREA OF DISBON ON THE BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 251MWF IAW B757 SRM 53-00-50-1A REPAIR 2, BAC D6-55191 REV: CSDR FDEA202209292395Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252MVF HAS AREAS OF DISBOND ON BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5SDR FDEA202209292394Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252MVF HAS DELAMINATION ON TOP SIDE REPAIRED DELAMINATION ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5SDR FDEA202209292393Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 52MVF HAS AREAS OF DISBONDED ON THE BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5SDR FDEA202209262371Plate · crackedRIGHT WING T/E REAR SPAR LOWER CORD WIGGLE PLATE CRACK AT WSTA330 APPROX STREAMER ATTACHED CRACKED WIGGLE PLATE AT WS 330 RIGHT WING T/E REAR SPAR LOWER CHORD WAS REMOVED AS REQ IAW FEDEX B757 SRM 51-40-02-0G AND REPLACED WITH NEW WIGGLE PLATE P/N 113N16
Back to Boeing 757-222