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 FDEA201412104098Strap · chafedCABIN STATION 1654 R4 DOOR UPPER SILL INBD CHORD FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 113 & FOUND MATERIAL LOSS MORE THAN 50%.. CHORD STRAP FABRICATED IAW DWG 146N8721 SHT 1 REV H. CHORD STRAP REMOVED IAW SRM 51-40-02 REV 113 & REPLACED IAW DWG 146N87SDR FDEA201412104097Strap · chafedCABIN STATION 1655 - 1667 L4 DOOR UPPER SILL INBD CHORD FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 113 & FOUND MATERIAL LOSS OF MORE THAN 50% CHORD STRAP. FABRICATED IAW DWG 146N8721 SHT 1 REV H. CHORD STRAP REMOVED IAW SRM 51-40-02 REV 113 & REPLACED BY FASDR FDEA201412054067Skin · corrodedTHE APU CUT OUT AT BS 1825 FROM STRINGERS 3 - 6R CORRODED. FOUND OUT OF LIMITS IAW SRM 53-80-15 FIG 101 TABLE 101 REV 113 AND REPAIRED IAW SRM 53-80-15 FIG 202 DETAIL 1 REPAIR 1 REV 113 REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412054066Skin · damagedLIGHTNING STRIKE AT BS 1000 - 1020 BETWEEN STRINGER 1 - 2 FUSELAGE EXTERIOR SKIN RT SIDE. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 113. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412054065Bracket · corrodedLEFT AFT EMERGENCY HATCH, INBD BRACKET CORRODED. REPAIRED. MINOR REPAIR.SDR FDEA201412054086Doubler · gougedEXISTING REPAIR FINDINGS, THERE IS A GOUGE ON THE EXISTING REPAIR DOUBLER AT STATION 340 STRINGER 23R. REPAIR REMOVED IAW SRM 51-40-02 REV 113. REPAIRED IAW EA F-5330-T0314168 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR CALA2014120892797Warning System · false activation20 MIN AFTER DEPARTURE LE SLAT DISAGREE RETRACTING FLAPS FROM 1 TO 0, DIVERTED. ACCOMPLISHED FAULT ISOLATION FOR, LE SLAT DISAGREE, 27-81 FAULT TREE 803, ACCOMPLISHED LE SLAT ROTARY ACTUATOR INSPECTION CHECK, RESET 3, 5 & 10 RA. FLAP OPERATIONS CHECKED MULTISDR FDEA201412054069Strap · chafedCABIN BS 355 STRINGER 7R, R1 DOOR CUT OUT UPPER SILL INNER CHORD FOUND CHAFED AT EDGE. CHAFE REMOVED IAW SRM 51-10-02 REV 113. FOUND OUT OF LIMITS IAW SRM 53-10-15 ALLOWABLE DAMAGE 1 FIG 101 REV 113. R & R BY FABRICATION OF PART IAW DWG 141N8421 SHEET SDR FDEA201412044062Slide · unserviceableR1 DOOR SLIDE PRESS BELOW LIMIT. RELEASED FOR SERVICE IAW MEL 52-11-01-B CATEGORY B. IDENTIFY L1 & R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. R & R R1 DOOR SLIDE IAW 75 MM 25-66-01-4. OK TO CONTINUESDR FDEA201412044058Frame · chafedFRAME BS 760 STRINGER 8 - 9R INNER SURFACE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 113. FOUND OUT OF LIMITS IAW SRM 53-00-07 ALLOWABLE DAMAGE 2 FIG 101 REV 113. REPAIRED IAW SRM 53-00-07 REPAIR 3 REV 113. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412034045Doubler · chafedEXISTING REPAIR FINDINGS, THERE ARE CHAFING MARKS ON THE EXISTING REPAIR DOUBLER AT NR 2 PYLON OTBD SIDE, RT OF THE FAN COWL SUPPORT WEB AFT SIDE AT NAC STATION 102. DAMAGED REPAIR DOUBLER REMOVED & NEW REPAIR CARRIED OUT IAW SRM 54-51-02 FIG 201 REPAIR 1 REVSDR FDEA201412034055Skin · damagedFUSELAGE EXTERIOR SKIN THERE ARE NICKS & SCRATCHES AT BS 1000 - 1020, STRINGERS 1 - 2R. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113 AND REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 113. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412034054Skin · damagedFUSELAGE EXTERIOR SKIN THERE ARE NICKS & SCRATCHES AT BS 1100 - 1120 STRINGERS 6 - 7L. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113 AND REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 113. REPAIR CLASSIFIED AS MAJOR.SDR CALA2014120592796Frame · corrodedAFT PIT, BILGE AREA, FRAME CORROSION STATION 1300, STRINGER 30L. REMOVED DAMAGE & INSTALL REPAIR IAW REO-G18514 REV A & ECRA 5310-06329.SDR CALA2014120592793Socket · damagedNUMBER 2 R-H DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED, NO HELP. SLAVED IN NEW POWER SUPPLY M732, NO HELP. REPAIRED LIGHT SOCKET ASSEMBLY IAW IPC 33-51-06-051. OPERATIONS CHECKED GOOD.SDR FDEA201412024031Skin · delaminatedRIGHT INBD FLAP, OTBD LOWER END, INNER SKIN DISBONDED. REPAIRED RT INBD FLAP, OTBD LOWER END SKIN IAW SRM 51-70-10. IAW EA F-5710-T0313603 FOR RSC TRACKING. MAJOR REPAIR.SDR FDEA201412024030Skin · damagedAFT CARGO DOOR SKIN AT LOWER AFT CORNER, NOTED EDGE WITH PREVIOUS BLEND. PREVIOUS BLEND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01 PG 104 DETAIL 4. MATERIAL LOSS .017 INCHES OF ORIGINAL .063 INCHES. REPAIR DOUBLER, INSTALLED TO REPAIR DAMAGE IAW SRM 52-30- SDR FDEA201412024028Sensor · trippedRIGHT WING SLIDE DISPLAYED ON EICAS DURING APPROACH. DISAPPEARED AFTER LANDING. PRESSURIZATION WAS NORMAL. SMP CHECK TARGET ON RT WING SLIDE DOOR S10374 NO DEFECTS NOTED. CLEANED SAME, CHECKED PSEU FOUND SENSOR S10374 TRIPPED, RESET SAME. OPERATIONAL CHESDR FDEA201412013995Support · corrodedEMPENNAGE RT SIDE THE APU INLET STRUCTURE FROM BS 1790 - 1825 ALONG STRINGER 6 HAS CORROSION. FOUND OUT OF LIMIT IAW SRM 51-10-02 REV 113. CORRODED SUPPORT REMOVED AND REPLACED IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412013986Beam · gougedFORWARD CARGO DOOR AT BS 591 LOWER EDGE BEAM GOUGED. R & R IAW DWG 143N6603 SHT 1 REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412013998Strap · corrodedEMPENNAGE RT SIDE THE APU INLET STRUCTURE FROM STRINGER 3 TO 6 AT BS 1790. FOUND OUT OF LIMIT IAW SRM 51-10-02 REV 113. REMOVED & NEW STRAP FABRICATED IAW DWG NR 148N3138 SHT 1 REV C & INSTALLED IAW DWG NR 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201412013997Support · corrodedEMPENNAGE RT SIDE THE APU INLET STRUCTURE FROM BS 1790 - 1825, ALONG STRINGER 3 IS CORRODED. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 113. CORRODED SUPPORT REMOVED & NEW SUPPORT FABRICATED IAW DWG 148N3152 SHT 1 REV & INSTALLED IAW DWG NR 148N3105 SHT 1 REV SDR FDEA201412013996Skin · damagedFUSELAGE EXTERIOR SKIN THERE ARE NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26L & 26R BS 600 T0 620. NICKS & SCRATCHES REMOVED, FOUND OUT OF LIMITS AT IAW SRM 53-00-01 FIG 101 DETAIL II REV 113. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 15 RVE 113. REPAIR SDR FDEA201411293977Crease Beam · corrodedBS 940 - 960 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 113 & FOUND OUT OF LIMITS. CREASE BEAM FABRICATED IAW DWG 144N5140 SHT 03 REV D, REMOVED IAW SRM 51-40-02 REV 113 & REPLACED IAW DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFISDR FDEA201411293976Crease Beam · corrodedBS 1120 - 1140 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 113 & FOUND OUT OF LIMITS. CREASE BEAM FABRICATED IAW DWG 144N5210 SHT 01 REV, REMOVED IAW SRM 51-40-02 REV 113 & REPLACED IAW 144N5200 SHT 2 REV B. REPAIR CLASSIFIEDSDR FDEA201411293975Crease Beam · corrodedBS 1421 RT CREASE BEAM WEB FOUND CORROSION. CREASE BEAM FABRICATED IAW DWG 146N5590 SHT 04 REV E, REMOVED IAW SRM 51-40-02 REV 113 & REPLACED IAW DWG 146N5590 SHT 4 REV E. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201411293974Crease Beam · corrodedCABIN STATION 1020 - 1040 LT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 113 & FOUND MATERIAL LOSS OF MORE THAN 50%. CREASE BEAM WEB FABRICATED IAW DWG 144N5140 SHT 4 REV A. CREASE BEAM R & R BY FABRICATED PART IAW DWG 4N5140 SHTSDR FDEA201411293973Crease Beam · corrodedCABIN STATION 960 - 984 LT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 113 & FOUND MATERIAL LOSS OF MORE THAN 50%. CREASE BEAM WEB FABRICATED IAW DWG 144N5140 SHT 3 REV D. CREASE BEAM R & R BY FABRICATED PART IAW DWG 144N5140 SHTSDR CALA2014120292757Frame · corrodedAFT PIT FRAME HAS EXFOLIATION CORROSION STATION 1480, STRINGER 25 - 26R. REMOVED DAMAGED SECTION OF RIB STATION 1480, STRINGER 26 - 25R. INSTALLED NEW SECTION IAW SRM 530-00 -07 REPAIR 5. SPLICE PLATES & J ANGLE REPAIR.SDR FDEA201411273916Web · chafedCHAFES ON THE REPAIR DOUBLER AT NR 1 PYLON INBD SIDE, RT OF THE FAN COWL SUPPORT WEB, AFT SIDE AT NAC STATION 102. REPAIRED IAW SRM 54-51- 02 FIG 201 REPAIR 1 REV 113. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201411273915Web · chafedTHERE ARE CHAFING MARKS ON THE EXISTING REPAIR DOUBLER AT NR 2 PYLON INBD SIDE, LEFT OF THE FAN COWL SUPPORT WEB AFT SIDE AT NAC STATION 102. REPAIRED IAW EA F-5450-T0314118 P 1. TITLE, NACELLES & PYLON, WING PYLON & STRUT, RT STRUT FAN COWL SUPPORT BEAM ASSSDR FDEA201411273914Skate Angle · crackedNUMBER 2 PYLON AFT FAIRING OTBD AFT SKATE ANGLE, WING SIDE, TE CRACKED. REPLACED BY FABRICATION & INSTALLATION IAW DWG 112N4601 SHT 02 REV C EA F-5400-T0315070 PT 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201411263899Sliding Window · out of adjustCAPTAIN'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED CAPTAIN`S SLIDING WINDOW IAW AMM 56-11-02-5. OPERATIONS CHECKED GOOD.SDR IXXA20141124034Bracket · brokenFLASHLIGHT BRACKET BROKEN. REPLACED HARDWARE IAW AMM 25-64-00.SDR FDEA201411223863Pin · bentLEADING EDGE SLAT LIGHT CAME & FLAP NEEDLE WENT TO INTERMEDIATE POSITION BETWEEN 0 & 1 DEGREE. 38,000 FT SLOWED TO 220 KTS DESCENDED BELOW 20,000 FT FOR TROUBLESHOOTING. UNABLE TO CORRECT, RTB TO TROUBLESHOOT. FOUND PIN 29 BENT & SHORTED TO PIN 14 OF CONNECSDR FDEA201411213840Doubler · chafedCHAFING ON THE EXISTING REPAIR DOUBLER AT NR 2 PYLON INBD SIDE OF THE AFT BULKHEAD AT NAC STATION 203. REPAIRED IAW EA F-5450-T0314203 P 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201411193799Skin · gougedSTATION 1440 STRINGER 23R - 24R SKIN EDGE HAS GOUGE MARKS. SKIN EDGE GOUGE MARKS COMPLIED WITH EA F-5330-T0312777 PART 1. TITLE FUSELAGE PLATES & SKINS EXISTING TRIM OUT LOCATIONS ON FUSELAGE SKIN AT BS 1440 BETWEEN STRINGERS 23R & 25R. REPAIR CLASSIFIED ASSDR FDEA201411193798Skin · damagedFUSELAGE SKIN AT STATION 1440 STRINGER 24R - 25R EDGE HAS EXISTING BLEND OFF. EXISTING BLEND OFF COMPLIED WITH EA F-5330-T0312777 PART 1. TITLE FUSELAGE PLATES & SKINS EXISTING TRIM OUT LOCATIONS ON FUSELAGE SKIN AT BS 1440 BETWEEN STRINGERS 23R & 25R. REPASDR FDEA201411193797Doubler · corrodedAFT CARGO COMPARTMENT BS 1460 - 1479 STRINGER 29 RT TO 30 ANTENNA RETAINER DOUBLER CORROSION FOUND AFTER ACCESS IAW SNRM NOO186. CORRODED ANTENNA RETAINER DOUBLER, RADIUS FILLER, REPLACED WITH NEW FABRICATED RADIUS FILLER IAW DWG 140N2058 SHT 1 REV A & EA F-5SDR FDEA201411183796Frame · mechanic errorMAIN CABIN, LT AT BS 960 FWD EMER WINDOW CUT OUT JUST BELOW STRINGER 9L DOUBLE DRILLED HOLE IN FRAME. FUSELAGE FRAME REPAIR AT STATION 960 BELOW STRINGER 9L WAS ACCOMPLISHED DUE TO EFFECTING THE PTF CONVERSION ON EA 757-5342-16-F4770 REV DATED NOV 7 2014 & NRSDR FDEA201411183745Floorbeam · damagedAIRCRAFT INSPECTION FLOORBEAM BS 310, RBL 42, UPPER CHORD OF FLOORBEAM, FOUR EACH FASTENER COUNTERSINKS ARE TOO DEEP. LOCK FASTENER HEADS PULLING THROUGH UPPER SURFACE OF CHORD. FLOORBEAM UPPER T CHORD AT STATION 310 REMOVED IAW SRM 51-40-02 REV 113. NEW T SDR FDEA201411173715Floorbeam · corrodedAGEING ACFT, ACFT INSPECTION FLOORBEAM BS 1640, LBL 10 TO RT FRAME UPPER CHORD, LOWER SURFACE OF FLOORBEAM HAS MANY AREAS OF CORROSION AROUND NUTPLATE HOLES, REF N01875. FLOORBEAM AT STATION 1640 LBL 70 TO RBL 70 WAS R & R WITH NEW FABRICATED FLOORBEAM IAW DWSDR FDEA201411163707Skin · chafedEMPENNAGE EXTERIOR SKIN THERE ARE NICKS & SCRATCHES AT STATION 1825 - 1844, STRINGER 5L - 6L. REMOVED & TREATED IAW SRM 51-10-02 & 51-20-01 REV 113, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET II ALLOWABLE DAMAGE 1 REV 113. REPAIR CARRIED OUT IAW PART 1SDR FDEA201411143688Support Beam · chafedNUMBER 2 STRUT FAN COWL SUPPORT BEAM OTBD RAIL FOUND CHAFE MARK AT NAC STATION 98. REPAIRED IAW EA F-5450-T0312965 PART 1 TITLE NACELLES & PYLON, PYLON STRUCTURES NR 2 STRUT LT & RT FAN COWL SUPPORT BEAM RAIL GOUGE BLEND OUT REPAIR. REPAIR CLASSIFIED AS MAJORSDR FDEA201411143687Support Beam · chafedNUMBER 2 STRUT FAN COWL SUPPORT BEAM INBD RAIL FOUND CHAFE MARK AT NAC STATION 98.5. REPAIRED IAW EA F-5450-T0312965 PART 1 TITLE NACELLES & PYLON, PYLON STRUCTURE NR 2 STRUT. LT & RT FAN COWL SUPPORT BEAM RAIL GOUGE BLEND OUT, REPAIRED. REPAIR CLASSIFIED ASDR FDEA201411133669Skin · dentedFUSELAGE EXTERIOR SKIN BS 1595 AT STRINGER 17R DENTED. REPAIRED IAW EA F-5330-T0313250 PART 1. REPAIR CALSSIFIED AS MAJOR.SDR FDEA201411113628Skin · chafedFWD E & E BAY DOOR EXTERNAL SKIN CHAFED. REPAIRED IAW EA F-5310-T0313047. REPAIR CLASSIFIED AS MAJORSDR FDEA201411063538Stringer · crackedAT STATION 1675 - 1695 RT SIDE A CRACK WAS FOUND IN STRINGER 18 WHILE INSTALLING FLOORBEAM. R & R PN FX146N3820-89 FABRICATED ON T14 1089757 IAW SRM 51-40-02 & DWG 146N3820, STINGER SECTION. MAJOR REPAIR.SDR FDEA201411053511Skin · corrodedAFTER REMOVAL OF AFT DRAIN MAST, FUSELAGE SKIN EXTERIOR SURFACE FOUND CORRODED BETWEEN STRINGER 25 & 26R BS 1660 & 1680. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113. REPAIRED IAW EA F-5330- T0312967 PART 1. REPAISDR FDEA201411053530Door · damagedMAIN CARGO DOOR LOWER FWD CORNER DAMAGED. ACCOMPLISHED EA F-5230-T0312949 DOORS & CARGO DOOR & HYD SYS MAIN CARGO DOOR CORNER DAMAGED. MAJOR REPAIR.
Back to Boeing 757-222