Boeing 767-300
Service difficulty reports · 2,161
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 = '767300' 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 = '767300' 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 IXXA2022051904Vertical Beam · delaminatedDELAMINATED AREA ON RIGHT HAND VERTICAL STABILIZER LEADING EDGE AT APPROX FSS 245.0 INNER SKIN.SDR IXXA2022051903Vertical Beam · delaminatedDELAMINATED AREA ON RIGHT HAND SIDE OF VERTICAL STABILIZER AT APPROX FSS 270.784.SDR IXXA2022051902Bracket · brokenR/H MAIN LANDING GEAR SUPPORT BEAM ACCESS PANEL SUPPORT BRACKET JUST ABOVE STRUT DOOR AFT SIDE IS BROKEN.SDR IXXA2022051901Skin Panel · corrodedAREA OF BULGING SKIN ON LEFT HAND WING I/B FLAP LOWER SURFACE AROUND MID FLAP.SDR FDEA202205161223Skin · noneFUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 632/654 AND STG 2/3 RH FUSELAGE SKIN BETWEEN STA 632/654 AND STG 2/3 RH WAS REPAIRED. SRM 53-00-01-2R REV 82 DEC 15,2021SDR FDEA202205161222Skin · noneFUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 220.5 / AND STG 30LH / BL0 FUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 220.5 / AND STGR 30LH WAS REPAIRED IAW E.A # M-5330-T0368423SDR FDEA202205161221Former · crackedRIGHT WING FIXED L/E FORMER CRACKED AT #8 SLAT OTBD ROTORY ACTUATOR REMOVED AND REPLACED THE RIGHT WING FIXED L/E NOSE FORMER AT #8 SLAT OTBD ROTORY ACTUATOR, STA OSS 499 IAW FEDEX E.A. H-5720-T0368429-P1, RELEASE DATE: MAY 11, 2022, TITLE: WING - SECONDARSDR FDEA202205161220Web · crackedLEFT WING, OUTBOARD FIXED LEADING EDGE NOSE BEAM WEB IS CRACKED AT OSS 679 REPAIRED CRACK IN L/H WING FIXED L/E NOSE BEAM WEB AT OSS 679 IAW B767 SRM 57-41-13- 2R, REPAIR 3SDR IXXA2022051601Tie Clip · crackedCRACKED ANGLE SUPPORT BETWEEN AFT AND MID TORQUE BOX #1 ENG.SDR FDEA202205161218Skin · dentedL/H WING #^ SPOILER HAS 2 EA DENTS ON UPPER SURFACE OF SPOILER( NEAR OUTBD END OF SPOILER. ACCOMPLISHED PERMANENT REPAIR OF DENTS ON L/H WING #6 SPOILER UPPER SURFACE IAW B767 SRM 57-70-01-2R FIG 201 SHEET 4 AND 51-70-05-0G. REMOVED AND REINSTALLED SPOILSDR FDEA202205161217Web · crackedRIGHT WING L/E WEB CRACKED AT REFULE PANEL REPAIRED THE RIGHT WING LEADING EDGE NOSE BEAM WEB AT STA OSS 679 IAW B767 SRM 57- 41-13-2R, REPAIR 3.SDR IXXA2022051502Tie Clip · crackedCRACKED ANGLE SUPPORT MID TORQUE BOX #1 ENG.SDR IXXA2022051501Pylon · crackedCRACK VERTICAL EXTRUSION UPPER SURFSCE IN MID TORQUE BOX #1 ENG PYLON LOOKING IN OUTBD MOON PANEL.SDR UIEA2022051400469Cowling · installedENGINE #1 REINSTALL ALL ENGINE COWLS DUE TO ENGINE CHANGE CANCELATION. INSTALL INLET COWL ON ENGINE #1 AS PER B767-300 AMM 71-11-01. INSTALLED FAN COWL ( LEFT RIGHT ) ON ENGINE # AS PER B767-300 AMM 71-11-04. INSTALLED LEFT AND RIGHT CORE COWLS ON ENGINSDR UIEA2022051400470Engine · installedREINSTALL ALL REMOVED HYDRAULIC, PNEMAUTIC AND ELECTRIAL CONNECTORS AND LINKS DUE TO #1 ENGINE CHANGE CANCELATION. REINSTALLED ALL; HYDRAULIC; PNEUMATIC AND ELECTRICAL CONNECTORS AS PER 71-00-02. PENDING ENGINE RUN UP LEAK CHECK .PERFORMED IDLE ;LEAK CHSDR UIEA2022051400472Cartridge · out of dateENG 2 OB SQUIB OUT OF DATE(<P>IN ACCORDANCE WITH W/O 94430 WAS REMOVED AND REPLACED CARTRIDGE OUTBOARD B767 AMM 26-21-03</P>)SDR UIEA2022051400473Squib · installedCARGO FIRE EXTINGUISHER BOTTLE SQUIB P/N 30903889 S/N 03608 DUE FOR REPLACEMENT IN ACCORDANCE WITH W/O 94430 WAS REMOVED AND REPLACED CARTRIDGE CARGO FIRE AS PER B767 26-011-00SDR UIEA2022051400474Blade · nickedFAN BLADE MARKED # 8 HAS A NICK AT L/E AREA D .BLENDED OUT # 1 ENG. FAN BLADE # 8 AT L/E AREA; FOUND WITHIN LIMITS PER B767-300 SRM 72-31-02-308-045-H000. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSP OF THE AREA NO NICK ON CRACK IND NOTED REF. AMM 70-11-SDR UIEA2022051400475Blade · nickedFAN BLADE MARKED # 1 HAS A NICK AT L/E AREA D. BLENDED OUT #1 ENG. FAN BLADE #1 AT L/E; AREA; FOUND WITHIN LIMITS PER B767-300 AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION. NO NICK ON CRACK IND NOTED AT THIS TIME. AMM 70-11SDR UIEA2022051400476Blade · nickedFAN BLADE MARKED # 10 HAS A NICK AT L/E AREA D .BLENDED OUT # 1 ENG. FAN BLADE # 10 AT LEADING EDGE AREA FOUND WITHIN LIMITS PER B767-300&; AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION. NO NICK ON CRACK IND NOTED. REF. AMSDR UIEA2022051400477Blade · dentedFAN BLADE MARKED # 11 HAS A DENT AT L/E AREA D .BLENDED OUT ENG. # 1; FAN BLADE # 11 AT LEADING EDGE; AREA FOUND WITHIN LIMITS PER B767-300 & AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION IN AREA NO CRACK OR INDICATION NOTSDR UIEA2022051400478Blade · nickedFAN BLADE MARKED # 31 HAS A NICK AT L/E AREA D . BLENDED OUT # 1 ENG. FAN BLADE # 31 AT LEADING EDGE; AREA FOUND WITHIN; LIMITS PER B767-300; AMM 72-31-02-308-045-H00. PERFORMED NDT; SPOT &;FLOURESCENT PENETRANT INSPECTION NO NICK; ON CRACK IND NOTED RESDR FDEA202205141206Fitting · failedDURING LSY CHECK AT INDY, THE LH MLG DOOR STOP SHIMS (FORWARD STOP) WERE IDENTIFIED AS LOOSE AND THE STOP PAD ON THE MLG DOOR HAS GOUGING ABOUT 0.020 DEEP. THE HELICOIL INSERTS IN THE AIRCRAFT SIDE STOP FITTING ARE LOOSE AND NOT HOLDING RETENTION OF THE SCRSDR FDEA202205141205Insert · failedFOUND RH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIM FASTENER HOLES TO BE ELONGATED. REMOVED INSERTS FROM RH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-T0368483P1 AND REPLACED SHIMS REF 767 SRM 51-20-11 AND 51-20-12.SDR FDEA202205141204Insert · failedFOUND LH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIMS TO HAVE MIGRATED. REMOVED INSERTS FROM LH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-T0368483P1 AND REPLACED SHIMS REF 767 SRM 51-20-11 AND 51-20-12.SDR CALA2022051601241Stiffener · crackedSUPPORT TASK : EA 5310-07143 REV D OP 001 (AD 2017-17-16) LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK AS MARKED TRANSFER REF HXWO 779672 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BSDR CALA2022051601240Stiffener · crackedSUPPORT TASK : EA 5310-07143 REV D OP 002 (AD 2017-17-16) RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK AS MARKED TRANSFER REF HXWO 779691 AND ORIGINATED BY EMP V914372 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BSDR CALA2022051301232Stiffener · crackedSUPPORT TASK : EA 5310-07143 REV D OP 001 (AD 2017-17-16) LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK AS MARKED TRANSFER REF HXWO 779672 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BSDR CALA2022051301231Stiffener · crackedSUPPORT TASK : EA 5310-07143 REV D OP 002 (AD 2017-17-16) RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 159 TO 185 FOUND 1EA CRACK AS MARKED TRANSFER REF HXWO 779691 AND ORIGINATED BY EMP V914372 RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BSDR FDEA202205121192Frame · cracked#2 PYLON AFT FAIRING MID FRAME FITTING AT APPROX NAC STA 330 IS CRACKED ON UPPER INBD SIDE REPAIRED THE #2 PYLON AFT FAIRING MID FRAME FITTING I/B SIDE AT NAC STA 329 IAW B767 SRM 54-52-71-2R, REPAIR 4 AND FEDEX EA H5450-T0368448-P1, RELEASE DATE: MAY 12, SDR FDEA202205121191Frame · cracked#1 PYLON HYD BAY MID FRAME CRACKED REPAIRED THE #1 PYLON HYDRAULIC BAY MID FRAME O/B SIDE IAW B767 SRM 54-52-71-2R, REPAIR 4 AND FEDEX EA H-5450-T0368446-P1, RELEASE DATE: MAY 12, 2022, TITLE: NACELLES/PYLON - WING PYLON/STRUT - #1 PYLON, NAC STA 329, FAIRSDR FDEA202205121189Bracket · cracked#2 PYLON AFT FAIRING OUTBD SIDE, 1EA HYD RESERVOIR PRESSURIZATION LINE CLAMP ATTACH BRACKET IS CRACKED AT APPROX NAC STA 327 REMOVED & REPLACED #2 PYLON AFT FAIRING OUTBD SIDE, 1EA HYD RESERVOIR PRESSURIZATION LINE CLAMP ATTACH BRACKET IAW B767 SRM 51-40-0SDR FDEA202205121188Shear Tie · cracked#1 PYLON HYD BAY FORWARD INBOARD UNDER PANEL437BR HAS CRACKED L-CLIP REMOVED & REPLACED CLIP IAW BAC DWG 313T2310 REV-SDR FDEA202205121187Angle · cracked#1 PYLON HYD BAY AFT OUTBOARD UNDER PANEL 437BL HAS CRACKED CLIP REMOVED & REPLACED CLIP IAW BAC DWG 313T2303, REV -SDR FDEA202205111180Shear Tie · cracked#2 PYLON AFT BULKHEAD, UPPER ATTACH CLIP ON INBD SIDE AT APPROX NAC STA 295 IS CRACKED REMOVED & REPLACED #2 PYLON AFT BULKHEAD, UPPER ATTACH CLIP ON INBD SIDE AT APPROX NAC STA 295 IAW B767 SRM 51-40-02 AND BOEING DWG NO. 313T2310 REV-, SHEET 95SDR CALA2022050401127Generator · leakingL GEN DRIVE LIGHT. DISCONNECTED GEN PER QRC PER FIM 24-22-00, BITE OF BPCU SHOWED MSG ''SERVICE IDG'' FOR LEFT APPROX 1 GAL AND INSPECTED IDG OIL AND SCAVENGE FILTER WITH NO NOT EXTENDED. RECONNECTED LEFT GEN AND PERF IDLE RUN AND LEAK GEN. ON INSPECTION OF LSDR FDEA202205021100None · noneAFTER LANDING RWY 15 PANC CLEARED RUNWAY AND COULD NOT STEER AIRCRAFT. STOPPED AIRCRAFT AND CALLED MX. MX CHECKED NOSE GEAR AND CLEARED US TO TAXI TO GATE. STEERING NORMAL TO GATE. HYDRAULIC PRESSURE NORMAL. INSPECTED NOSE WHEEL SYSTEM COMPONENTS FOR SECSDR FDEA202205021099None · noneLE SLAT ASYM EICAS ALERT ON FINAL @ 1300 MSL WHEN FLAPS SELECTED TO 25 DEGREES . EXECUTED MISSED APPROACH @ 700 . LEVELED AT 2000 CLEANED AIRCRAFT TO FLAPS 5 AND NOTICED LE SLAT ASYM EICAS EXTINGUISHED WHEN FLAPS RETRACT TO 20. REATTEMPED FLAP EXTENSIOSDR FDEA202204301096None · crackedLEFT WING L/E FORMER CRACKED AT #5 SLAT INBD AUX TRACK REMOVED AND REPLACED THE L/W L/E NOSE FORMER AND ATTACH ANGLE AT #5 SLAT INBD AUX TRACK, STA. OSS 441 IAW FEDEX E.A. H-5720-T0368117-P1, RELEASE DATE: 29APR2022, TITLE: WING - SECONDARY WING STRCT - FISDR FDEA202204301095None · crackedLEFT WING L/E FORMER CRACKED AT #5 SLAT OTBD ROTARY ACTUATOR REMOVED AND REPLACED THE L/W L/E NOSE FORMER AND ATTACH ANGLE AT #5 SLAT OTBD ROTARY ACTUATOR, STA. OSS 499 IAW FEDEX E.A. H-5720-T0368117-P1, RELEASE DATE: 29APR2022, TITLE: WING - SECONDARY WINSDR FDEA202204301094None · crackedLEFT WING L/E FORMER CRACKED AT #4 SLAT INBD ROTARY ACTUATOR REMOVED AND REPLACED THE L/W L/E NOSE FORMER AND ATTACH ANGLE AT #4 SLAT INBD ROTARY ACTUATOR, STA. OSS 565 IAW FEDEX E.A. H-5720-T0368117-P1, RELEASE DATE: 29APR2022, TITLE: WING - SECONDARY WINSDR FDEA202204301093None · crackedRIGHT WING L/E CAVITY SUPPORT BRACKET CRACKED AT OFSS 487 REMOVED AND REPLACED THE R/W L/E NOSE FORMER (CURTAIN SUPPORT BRACKET) AND ATTACH ANGLE AT OSS 499 (OFSS 487) IAW FEDEX E.A. H-5720-T0368117-P1, RELEASE DATE: 29APR2022, TITLE: WING - SECONDARY WINGSDR FDEA202204301092None · crackedRIGHT WING L/E CAVITY CURTAIN SUPPORT BRACKET CRACKED AT OFSS 559 REMOVED AND REPLACED THE R/W L/E NOSE FORMER (CURTAIN SUPPORT BRACKET) AND ATTACH ANGLE AT OSS 565 (OFSS 559) IAW FEDEX E.A. H-5720-T0368117-P1, RELEASE DATE: 29APR2022, TITLE: WING - SECONDSDR FDEA202204291083Web · crackedLEFT WNG L/E INSIDE REFUEL PANEL NOSE BEAM WEB CRACKED REPAIRED LEFT WING NOSSE BEAM WEB IAW B767 SRM 57-41-13-2R, FIGURE 201, REPAIR 3SDR FDEA202204291082Splice Plate · crackedRIGHT WING L/E CAVITY SKIN SPLICE PLATE CRACKED AT OFSS 502 REMOVED AND REPLACED R/H WING L/E SKIN SPLICE PLATE AT OFSS 502 IAW B767 SRM 51-40-02 AND BAC DWG 114T2800, REV. G.SDR FDEA202204281084Panel · delaminatedLH WING - LEADING EDGE STRUCTURE UPPER SURFACE SKIN PANELS AT LOCATION OF ENGINE PYLON HAS AN AREA OF THE INBOARD PANEL WITH THE SKIN DELAMINATED. REPLACED PANEL USING BOEING DRW 114T6104 AND 767 SRM 51-40-03-0G-0.SDR FDEA202204281078Former · crackedR/H WING LEADING EDGE AT WS 499 (SLAT # 8) HAS A CRACKED FORMER. REPLACED CRACKED FORMER REF E.A. H-5720-T0368255 P1.SDR FDEA202204281077None · damagedRIGHT WING I/B MAIN FLAP AND AFT FLAP LOWER SKIN HAS DEBRIS IMPACT. EVALUATED RW MAIN FLAP LOWER SURFACE AND FOUND ONLY DAMAGE TO SURFACE FINISH NO DENTS GOUGES OR DELAMINATION IAW B767 SRM 57-53--01-1A. AFT FLAP HAD DAMAGE TO ROCK SHIELD. REPAIRED ROCK SDR FDEA202204271072Floor Panel · noneMAIN CABIN FLOOR, PANEL 242UFF HAS AN AREA OF DAMAGE, STA 975, RBL 59 REPAIRED DAMAGE ON FLOOR PANEL 242UFF, STA 975, RBL 59 IAW B767 SRM 53-00-50-2R, PARA. 4.B.SDR FDEA202204271071Floor Panel · noneMAIN CABIN FLOOR, PANEL 241AGF IS DAMAGED, STA 1008, LBL 82 REPAIRED DAMAGE ON FLOOR PANEL 241AGF, STA 1008, LBL 82 IAW B767 SRM 53-00-50-2R, PARA. 4.D.
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