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 FDEA202204271070Floor Panel · noneMAIN CABIN FLOOR, PANEL 242VFF IS DAMAGED, STA 1013, RBL 83 REPAIRED DAMAGE ON FLOOR PANEL 242VFF STA 1013, RBL 83 IAW B767 SRM 53-00-50-2R, PARA. 4.C.SDR FDEA202204271069Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 242SFF IS DAMAGED IN 3 PLACES, STA 1023-1068, RBL 30 REPAIRED 3EA DAMAGE LOCATIONS ON FLOOR PANEL 242SFF IAW B767 SRM 53-00-50-2R, PARA. 4.C.SDR FDEA202204271068Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 241KFF IS DAMAGED 2 PLACES, STA 885-889, LBL 80-85 REPAIRED 2EA DAMAGE LOCATIONS ON FLOOR PANEL 241KFF, STA 885-889, LBL 80-85 IAW B767 SRM 53-00-50-2R, PARA. 4.D.SDR FDEA202204271067Floor Panel · delaminatedMAIN CABIN FLOOR, PANEL 241HFF IS DAMAGED 2 PLACES, STA 835-870, LBL 56-63 REPAIRED 2EA DAMAGE LOCATIONS ON FLOOR PANEL 241HFF, STA 835-870, LBL 56-63 IAW B767 SRM 53-00-50-2R, PARA. 4.BSDR FDEA202204271066Floor Panel · unknownMAIN CABIN FLOOR, PANEL 241GFF IS DAMAGED 2 PLACES, STA 836-847, LBL 35-43 REPAIRED 2EA DAMAGE LOCATIONS ON FLOOR PANEL 241GFF IAW B767 SRM 53-00-50-2R, PARA. 4.B.SDR FDEA202204271065Floor Panel · unknownMAIN CARGO DECK FLOOR PANEL 241ZFF HAS PATCH THAT IS DISBONDED REPAIRED DAMAGE ON FLOOR PANEL 241ZFF IAW B767 SRM 53-00-50-2R, PARA. 4.C.SDR FDEA202204271063Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL 241YFA IS CRACKED REPAIRED CRACK ON FLOOR PANEL 241YFA IAW B767 SRM 53-00-50-2R, PARA 4.D.SDR FDEA202204271061Slat · dentedLEFT WING SLAT 4 WITH DENT T/E WEDGE LH WING SLAT #4 WEDGE AT POSITION OSS(648.9-657) UPPER SKIN WAS REPAIRED IAW SRM 57- 43-02-2R PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 149, 159-163 FIG. 202 REV. 82 DEC15/2021SDR FDEA202204261073Slat · faultedDURING APPROACH WHEN SELECTING FLAPS TO 25 GOT LE SLAT DISAGREE. EXECUTED A GO AROUND AND COMPLIED WITH QRH. EMERGENCY WAS DECLARED. PERFORMED T/S IAW FIM 27-51 FAULT TREE 809. BITE TEST SHOWED NO CURRENT FAULTS. CYCLED FLAPS AND SLATS FULL UP & DOWN SEVSDR FDEA202204261058Flap · gougedLEFT INBD AFT FLAP LOWER SURFACE CHIPPED INBD SIDE. REPAIRED L/W I/B FLAP LOWER SURFACE NOTED AREA IAW B767 SRM 5753-01-2R FIG 201 SHEET 4 AND 51-70-03-OG FIG 20 SHEET 1.SDR FDEA202204261056Skin · delaminatedRIGHT WING O/B FLAP I/B SIDE L/E AREA DELAM. REPAIRED DELAM ON RW O/B FLAP L/E WITH FIBERGLASS DOUBLER AND CORE REPAIR IAW B767 SRM 57-53-01-2R FIG 201 SHEET 5, 57-53-01-0I, 51-70-05, 51-40-02 AND NDTM PT 1 51-01-01.SDR FDEA202204251053Splice Plate · crackedFIXED LEADING EDGE SPLICE PLATE AT APPROX LS FLE OSS 520 IS CRACKED (MWT)
FIXED LEADING EDGE SPLICE PLATE AT APPROX LS FLE OSS 520 IS CRACKED (MWT) REPLACED CRACKED SPLICE PLATE. REF E.A. T-5720-T0368182 P1SDR FDEA202204251047Former · crackedL/H WING AT STATION .441 L/E FORMER IS CRACKED P/N: 114T2170-5 REPAIR PER SRM/EASDR FDEA202204241090Panel · crackedRH WING WIGGLE PLATES BROKEN AT JACK POINT 0000280794 : SHAEFFER, DAVID C - 25-APR-2022 00:15 REPLACED DAMAGED PANELS REF B767 SRM 57-51-02-2R FIG 201, SHT 1-3 REPAIR 5SDR FDEA202204241050Former · crackedR/H WING AT STATION .441 L/E FORMER IS CRACKED P/N: 114T2170-6 REMOVED AND REPLACED RH WING LEADING EDGE NOSE FORMER(114T2170-6), ANGLE (114T2171-4), AND LOOSE FASTNERS AT OSS 441.596 IN REF. TO EA# T H-5720-T0368175 P1SDR FDEA202204241044Former · crackedRH WING LEADING EDGE CRACKED FORMER AND LOOSE FASTNERSAT RS OSS 441.596 REMOVED & REPLACED FORMER, AND FASTNERS IN REF. TO E.A H-5720-T0368164 P1SDR FDEA202204241043Former · crackedLH WING LEADING EDGE CRACKED FORMER AND LOOSE FASTNERSAT LS OSS 441.596 REMOVED & REPLACED FORMER, AND FASTNERS IN REF. TO E.A H-5720-T0368164 P1SDR FDEA202204231089Former · crackedCRACKED FORMER AND LOOSE FASTENERS AT LS OSS 441.596 0000355851 : MITROVICH, DAVID T - 24-APR-2022 05:34 REMOVED & REPLACED FORMER & FASTENERS REF: E.A TH5720-T0368164 P1.SDR FDEA202204231088Former · crackedCRACKED FORMER AND LOOSE FASTENERS AT RS OSS 441.596 0000355851 : MITROVICH, DAVID T - 24-APR-2022 05:33 REMOVED & REPLACED FORMER & FASTENERS REF: E.A TH5720-T0368164 P1.SDR FDEA202204221027Former · crackedNR 12 441 AT RS FLE OSS 441 CRACKED FORMER 114T2170-6 WITH ANGLE 114T2171-3, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REPLACED WITH B67-57-002-02 FORMER & B67-57-003-02 ANGLE REFERENCE EA H-5720-T0368124 P1SDR FDEA202204221026Former · crackedNR 8 AT LS FLE OSS 441 CRACKED FORMER 114T2170-5 WITH ANGLE 114T2171-4, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION REPLACED WITH B67-57-002-01 FORMER & B67-57-003-01 ANGLE REFERENCE EA H-5720-T0368124 P1SDR FDEA202204211025Former · crackedAT RS FLE OSS 565 CRACKED FORMER 114T2512-14 WITH ANGLE 114T2512-12, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. 0000553921 : DAVIES, ANDREW M - 22-APR-2022 10:11 REMOVED AND REPLACED CRACKED FORMER REF E.A. H-5720-T0368124 P1SDR FDEA202204211024Former · crackedAT RS FLE OSS 499 CRACKED FORMER 114T2511-14 WITH ANGLE 114T2511-12, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REMOVED AND REPLACED CRACKED FORMER REF E.A H-5720-T0368124 P1SDR FDEA202204211023Former · crackedAT LS FLE OSS 565 CRACKED FORMER 114T2512-13 WITH ANGLE 114T2512-11, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REMOVED AND REPLACED CRACKED FORMER REF E.A. H-5720-T0368124 P1SDR FDEA202204211022Former · crackedAT LS FLE OSS 499 CRACKED FORMER 114T2511-13 WITH ANGLE 114T2511-11, ALONG WITH LOOSE/DAMAGED FASTENERS AT THIS LOCATION. REMOVED AND REPLACED CRACKED FORMER REF E.A, H-5720-T0368124 P1SDR FDEA202204190991Printer · failedSTRONG AND RAPID ONSET OF FUMES IN THE COCKPIT. ODOR UNIDENTIFIED. CREW RESPONDED WITH OXYGEN MASKS, QRC, FOLLOWED BY QRH THEN DIVERT TO SHV. ***EMERGENCY DECLARED*** T/S PER FIM 21-00-21-3. PERFORMED EXTERNAL INSP OF RT AND LEFT ENGINES.NO LEAKS NOTED, INSSDR FDEA202204170981None · noneLH WING LE AT STA OSS441 FORMER CRACKED P/N 114T2170-5 C/W WITH EA H-5720-T0368062P1SDR FDEA202204160975Unknown · unknownDURING APPROACH RECEIVED A TRAILING EDGE FLAPS DISAGREE EICAS MESSAGE UPON CONFIGURING TO FLAPS 5. DISCONTINUED THE APPROACH AND COMPLIED WITH QRH. RETURNED TO FOR A UNEVENTFUL FLAPS 20 LANDING. SDR FDEA202204090907Former · crackedCRAKED FORMER 114T2170-5 ALONG WITH LOOSE/DAMAGED FASTENERS LOCATED AT LS FLE OSS 441. 0000301922 : VERNON, JAMES L - 09-APR-2022 23:11 REPLACED FORMER AND ATTACH BRACKET REF E.A. TH-5720-T0367929 P2SDR FDEA202204080895None · crackedRW LWR T/E PANEL AT WS 685 ATTACH ROD AFT ATTACH BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW BAC DWG 113T1681 SHEET 3, REVISION A, AND FEDEX EA H-5720-T0367856-P1 RELEASED APR 05, 2022, TITLED "WING - SECONDARY WING STRCT - RH WING, LOWER TRAILING EDSDR FDEA202204070888None · delaminatedRH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL: 435. RH WING OUTBOARD FLAP LOWER SKIN WITH DENT AT WBL 435 THAT WAS REPAIRED IAW SRM 57- 53-01-2R FIG. 201 PAGE 1-6 TABLE II AND SRM 51-70-17-0G-0 FIG. 10 PAGE 1, 24, 25, 36, 48 PARA. 4.A. REV. 82 DEC15/20SDR FDEA202204060882None · gougedLEFT WING #6 SPOILER LOWER SURFACE HAS HOLE APROXIMATELY 1"X1". ACCOMPLISHED PERMANET REPAIR OF PUNCTURE ON L/W #6 SPOILER LOWER SURFACE IAW FEDEX B767 SRM 57-70-01-2RFIG 201 SHEET 4 AND 51-70-05-2RSDR FDEA202204060881None · gougedRIGHT WING #9 SLAT UPPER TRAILING EDGE WEDGE LOWER SURFACE IS GOUGED IB OF IB MAIN TRACK. REPAIRED RIGHT WING #9 SLAT UPPER TRAILING EDGE WEDGE LOWER SURFACE GOUGE I/B OF I/B MAIN TRACK IAW B767-SRM-57-43-02-2R REPAIR 1 FIG 201 SHEET 1 AND 2.SDR FDEA202204060877Bracket · cracked#1 ENGINE PYLON, OTBD SIDE DRAIN TUBE ATTACH BRACKET IS CRACKED JUST BELOW PANEL 437BL CRACKED BRACKET ON #1 ENGINE PYLON, OUTBD DRAIN TUBE REMOVED & REPLACED WITH NEW BRACKET IAW BAC DWG 313T2380, REV-SDR FDEA202204050869None · noneRH WING LE AT STA OSS-565 RIVETS ARE LOOSE. COMPLIED WITH E.A. TH-5720-T0367852 P2 PER STEP 4. WRI 57203540SDR FDEA202204050868None · noneRH WING LE AT STA OSS-499 RIVETS ARE LOOSE COMPLIED WITH E.A TH-5720-T0367852 P2 AS REFERENCED IN STEP 3.. IN SEQ 000145SDR FDEA202204050862None · noneLH WING LE AT STA OSS441 RIVETS LOOSE REPLACED FASTENERS REF B767 SRM 51-40-02 AND E.A. TH-5750-T0367852 P1SDR FDEA202204050861None · noneRH WING LE AT STA OSS-441 RIVETS ARE LOOSE COMPLIED WITH E.A TH-5720-T0367852 P2 AS REFERENCED IN STEP 2.. IN SEQ 000145SDR FDEA202204050860None · noneRH WING LE AT STA OSS-437 RIVETS ARE LOOSE COMPLIED WITH E.A TH-5720-T0367852 P2 AS REFERENCED IN STEP 1.. IN SEQ 000145SDR FDEA202204050853Former · failedLH WING LE AT STA OSS437 RIVETS LOOSE COMPLIED WITH EA H-5720-T0367852P1SDR FDEA202204050851Frame · cracked#2 PYLON, 447BR, HYDRAULIC BAY, MID FRAME IS CRACKED REPAIRED MID-SPAR FRAME IAW FEDEX EA H-5450-T0367830-P1, RELEASED APR04, 2022, TITLED "NACELLES / PYLON - WING PYLON / STRUT - #2 PYLON, NAC STA 329, FAIRING, FRAME, SRM REPAIR DEVIATIONSDR FDEA202204050850Frame · cracked#1 ENGINE, INBD SIDE, MID PYLON FRAME UNDER THE LATCH BEAM IS CRACKED REPAIRED MID-SPAR FRAME IAW FEDEX EA H-5450-T0367836-P1, RELEASED APR 04, 2022, TITLED " NACELLES / PYLON - WING PYLON / STRUT - #1 PYLON, NAC STA 329, FAIRING, FRAME, SRM REPAIR DEVIATSDR FDEA202204040836Floor Support · crackedAREA AFT OF BULK CARGO, MAIN CABIN FLOOR, , SUPPORT STRUCTURE SPLICE IS CRACKED BETWEEN STA 1562 AND 1582 AT APPROX LBL80 REMOVED AND REPLACED CRACKED SPLICE ANGLE WITH NEW ANGLE IAW BAC DWG 146T5650, REV. CSDR FDEA202204040832Skin · gougedRIGHT WING #8 SLAT LOWER TRAILING EDGE AFT WEDGE IS GOUGED OB OF MAIN TRACK. REPAIRED GOUGE ON R/W #8 SLAT T/E WEDGE LOWER SKIN AT O/B OF MAIN TRACK WITH 250 DEGREE CORE AND DOUBLER REPAIR IAW B767 SRM 57-43-02-2RFIG 201 REPAIR1 SHEET 1, 51- 70-10-2R REPAIRSDR FDEA202204030857None · noneLH WING LE AT STA OSS441 RIVETS LOOSE AND FORMER CRACKED P/N 114T2170-5. INSTALLED NEW FORMER REF: E.A. H-5720-T0367810. SEQ:146. W/O:82588.SDR FDEA202204030856None · noneL/H WING L/E #5 SLAT GOUGED STA 499. 0000452710 : ROSNER, DANIEL D - 05-APR-2022 02:00 SEQ 152.. TH-5750-T0367838 P1 N/R 23 L/H WING L/E #5 SLAT GOUGED STA 499. REMOVED DAMAGE MATERIAL AND BONDED IN NEW REPAIRS SEALED AND PAINTED. REF B-767 SRM 57-43-02-2SDR FDEA202204030855None · noneL/H WING L/E #5 SLAT GOUGED STA 441. 0000452710 : ROSNER, DANIEL D - 05-APR-2022 02:02 SEQ 151.. TH-5750-T0367837 P1 N/R 22 L/H WING L/E #5 SLAT GOUGED STA 441. REMOVED DAMAGE MATERIAL AND BONDED IN NEW REPAIRS, SEALED AND PAINTED. REF B-767 SRM 57-43-02-SDR FDEA202204030826Floor Support · crackedAREA AFT OF BULK CARGO, MAIN CABIN FLOOR SUPPORT STRUCTURE, OTBD SPLICE IS CRACKED BETWEEN STA 1562 AND 1582 AT APPROX LBL82 REMOVED ANGLE AND REPLACED WITH NEW ANGLE IAW B767 SRM 51-40-02-0G AND BAC DWG 146T5650, REV. C.SDR FDEA202204030825Skin · gougedRIGHT WING #8 SLAT LOWER TRAILING EDGE AFT WEDGE IS GOUGED OB OF IB AUX TRACK. REPAIRED GOUGE ON R/W #8 SLAT T/E WEDGE LOWER SKIN AT O/B OF I/B AUX TRACKWITH 250 DEGREE CORE AND DOUBLER REPAIR IAW B767 SRM 57-43-02-2RFIG 201 REPAIR 1 SHEET 1, 51- 70-10-2R, SDR FDEA202204030824Skin · gougedLW #5 SLAT INBD T/E LWR SURFACE IS GOUGED. REPAIRED GOUGE ON L/W #5 SLAT T/E LOWER SURFACE WITH 250 DEGREE CORE AND DOUBLER REPAIR IAW B767 SRM 57-43-02-2RFIG 201 REPAIR 1 SHEET 1, 51-70-10-2R, 57-43-01- 0I, 51-20-05 AND B767 AMM 51-21-01/701, B767 NDTM PAR
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