Boeing 767-3S2F
Service difficulty reports · 2,378
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 = '7673S2F' 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 = '7673S2F' 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 FDEA202402090139Skin · crackedRH WING, SLAT NR 10 SURFACE OUTERSIDE AREA LEADING EDGE CRACKED. RH WING, SLAT NO. 10 SURFACE OUTER SIDE AREA LEADING EDGE SKIN , CRACK WAS REPAIRED. I.A.W. SRM 57-43-01-2R FIG.201 REPAIR 2 SHET 1-3 REV 88.SDR FDEA202402030134Skin · dentedLEFT INBOARD FLAP, AFT FLAP, LOWER SURFACE, BTW FLAP TRACK FAIRINGS, DENTS. LEFT INBOARD FLAP, AFT FLAP, LOWER SURFACE, BTW FLAP TRACK FAIRINGS WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 AND SRM 51-70-03-0G PAR 5.L FIG 16 PAG 27,52 REV 88 DEC 15/2023SDR FDEA202401310126Skin · crackedLH OUTBOARD ELEVATOR LOWER SKIN WITH HOLE AT 42" FROM ELEVATOR EDGE INTERIOR AND 10" FROM L.E. LH OUTBOARD ELEVATOR LOWER SKIN AT 42" FROM ELEVATOR EDGE INTERIOR AND 10" FROM L.E. WAS REPAIRED IAW E.A. # : H-5520-T0377675 RELEASE DATE : JAN 30,24SDR FDEA202401260114Circuit Card · inoperativeSPEED BRAKES SEGMENT LIGHT & SPREED BRAKES EXT EICAS MESSAGE ILLUMINATED AFTER TAKEOFF BELOW 1000FT. AFTER ARRIVAL, ACFT CAUTION MSG EICAS & SPEED BRAKES ANNUNCIATOR LIGHT ILLUM. R & R LANDING CONFIG WARNING CARD (M983) OPS TEST OK IAW AMM 31-51-04-4. CONSDR FDEA202401240108Skin · wornLH WING SLAT 5 TRAILING EDGE WEDGE WITH WEAR MARK OSS 44160 LH WING SLAT 5 TRAILING EDGE WEDGE AT OSS 441.60 WAS REPAIRED IAW B767 SRM 57-43--02-2R FIG 201 SHEET 1-2 AND SRM 51-70-10-2R REP 4 FIG 202 SHEET 8 PAGE 150,163,164. REV 88 DEC 15/2023SDR FDEA202401120072Skin · delaminatedLH WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION AT OTEF STA 72 LH WING OUTBOARD FLAP LEADING EDGE AT OTEF STA 72 WAS REPAIRED IAW B767 SRM 57-53-01- 2R REP 1 FIG 201 SHEET 1-3-5-6 PAGE 1-6 AND SRM 51-70-03-0G PAR 5A FIG 5 PAGE 19-36. REV 88 DEC 15/ 202SDR FDEA202401090156Skin · dentedFOUND DENT ON #11 SLAT AFT EDGE AT APPROX WS 887, MEASURING 14" X 5.5". COMPLIED WITH (EA# H-5740-T 0378114 P 1 REPAIRED LH WING L/E # 11 SLAT TRAINLING EDGE WEDGE AT WS OSS 887 IN REF TO 767 SRM 57-43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, AND SDR FDEA202312071921Carbon Seal · leakingAT 34,000 FT AND CRUISE MODE, OIL QUANTITY OF LEFT ENGINE WAS NOTICED TO BE AT ZERO WITH NO OTHER ABNORMAL ALERTS. OIL PRESSURE WAS AT 35-37 WHICH WAS ABOUT 20 PSI LESS THAN THE RIGHT ENGINE. THE PRESSURE SLOWLY CONTINUED TO DROP UNTIL RED LINE AT ABOUT SDR FDEA202301290174Valve · malfunctionedPOSSIBLE FUEL LEAK ASSOCIATED WITH THE LEFT TANK AND ENGINE, LEFT SIDE DROPPED AN EXTRA 1000 LBS EVERY 10 MINS. AFTER 30 MINS OF FLT, WERE 3500 POUNDS SHORT ON FUEL AT TINGS INTERSECTION. ENGINE FUEL BURNS WERE NORMAL AND EVEN. ACFT ARRIVAL W/ NO VISUAL EXTERNSDR FDEA202301230158Skin · dentedSLAT 5 WITH DENT AT UPPER SKIN, TRAILING EDGE WEDGE. LH WING SLAT #5 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG. 1-2 FIG. 201 AND B767 SRM 51-70-10-2R FIG. 201 REV. 85 15-DEC-22SDR FDEA2023012320155Skin · wornRH WING, OUTBOARD SLAT (8), TRAILING EDGE, LOWER SURFACE WITH WEAR (TWO POINTS) RH WING, OUTBOARD SLAT 8 TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW SRM 57-43- 02-2R PAG. 1-2 FIG. 201, AND SRM 51-70-10-2R FIG. 201 REV. 85 15-DEC-22SDR FDEA202301170126Transmitter · failedRT SYS PRESS EICAS ON DEPARTURE. UNABLE TO RESTORE SYSTEM PRESSURE VIA QRH. DECLARED EMERGENCY AND RTB TO CAN. EMERGENCY DECLARED. CONSULTED WITH FLIGHT CREW JUST R HYD SYS LIGHT ILLUMINATED AND R SYS PRESS EICAS, ELEC PUMP LOW PRESS LIGHT AND EDP LOW PSDR FDEA202301150114Pump · misinstalledCREW REPORT ON DEBRIEF THAT C HYD PRIM 2 MESSAGE MOMENTALLY CAME ON WITH GEAR OPERATION. REMOVEDAND REPLACED CENTER HYD PRIM NR 2 PUMP IAW AMM 29-11-02-4. LEAK AND OPS CHECKED GOOD. WAS INFORMED THAT WHILE REPLACING THE HYD PUMP THEY NOTICED THAT THE PUMP WSDR FDEA202301110070Exhaust Fan · failedCOMING THROUGH 10,000 FT ON ARRIVAL HAD A SMELL OF AN ELECTRIC MOTOR GOING OUT IN THE COCKPIT. UPON SHUTDOWN HAD AN EICAS MESSAGE FOR FWD EQ EXH FAN. REMOVED AND REPLACED FWD EXHAUST FAN EQUIP NR B12 IAW AMM 21-58-06-4. OPS CHECKED GOOD.SDR FDEA202301090058Skin · wornRH WING, SLAT # 8, TRAILING EDGE WEDGE, BOTTOM SKIN WITH WEAR. RH WING, SLAT #8, TRAILING EDGE WEDGE BOTTOM SKIN WAS REPAIRED IAW SRM 51-70-10-2R PAG. 163, FIG. 202 REV. 85 DEC15/2022 AND SRM 57-43-02-2R FIG. 201, (SHEET 1) REV. 85 .SDR FDEA202212172944Beam · damagedAFTER OPENING PYLON PANEL 437BL (#1 ENGINE OTBD) FOUND BOTH AFT DOOR HINGE FITTINGS WITH EXCESSIVE PLAY AND HINGE BOLTS WEARING INTO PYLON FITTINGS. ITEM REPAIRED PER E.A. H-5451-T0372182 P1.SDR FDEA202211172811Skin · wornRH WING SLAT #8 INNER SKIN WEDGE AREA TWO PREVIUS REPAIR WITH WEAR. RH WING SLAT #8 T/E WEDGE INNER SKIN, ONE PREVIOUS REPAIR WAS REPLACED AND ONE FILLER WAS REPLACED IAW B767 SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 AND SRM 51-70-10-2R REP. 4 PAG. 10, 11,SDR FDEA202211172810Skin · wornLEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WITH WEAR (LOWER SURFACE). LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R REPAIR 4 FIG. 202 SHEET 8 AND SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 REV. 84 15-AUG-2022SDR FDEA202211122762Skin · damagedLH WING - OUTBOARD FLAP ASSY LEADING EDGE STRUCTURE IS DAMAGED AT LOCATION ADJACENT TO THE INBOARD SIDE OF THE OUTBOARD FLAP TRACK FAIRING. REPAIRED USING 767 SRM 57-53-01-2R.SDR FDEA202211112759Skin · gougedR/H WING SLAT #8 HAS GOUGE DAMAGE REPAIRED USING 767 SRM 51-70-10-2R; EA H-5750-T0371624 CREATED FOR TRACKING ONLYSDR FDEA202211102763Skin · damagedLH WING - OUTBOARD FLAP ASSY LEADING EDGE STRUCTURE IS DAMAGED AT LOCATION ADJACENT TO THE INBOARD SIDE OF THE OUTBOARD FLAP TRACK FAIRING,MWT. REPAIRED BIRD STRIKE DAMAGE TO LH OB FLAP LEADING EDGE PER EA H-5750-T0371632 P1SDR FDEA202211092764Skin · damagedRH OUTBOARD ELEVATOR - UPPER SKIN SURFACE HAS IMPACT DAMAGE AT LOCATION OF INBOARD FWD CORNER,MWT. REPAIRED RH OB ELEVATOR TOP SURFACE (6"X6") REF. 767 SRM 55-20-01-2R REPAIR 1 & 767 SRM 51-70-04-0G PAR 4E. PERFORMED BALANCE CALCULATION PER 767 SRM 51-60-0SDR FDEA202211092739Seal Depressor · crackedFORWARD CARGO DOOR AFT SEAL DEPRESSOR DAMAGED APPROXIMATELY 14" ABOVE BOTTOM SEAL. INSTALLED NEW SEAL DEPRESSOR PNR:143T8542Y4 IAW SRM-51-40-02-0G.SDR FDEA202211052733Former · crackedFORMER CRACKED AT R/W FLE OSS 441, (PN INSTALLED 114T2170-6, WITH 114T2171-3) REPLACED PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441; WANT ALSO TO ATTACH FORMERS THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S.SDR FDEA202210292695Skin · chafedL/H WING NO. 5 LEADING EDGE SLAT LOWER TRAILING EDGE CHAFFED AT APROX OSS 441 M.W.T. REPAIRED #5 SLAT PER EA H-5750-T0371376SDR FDEA202210292694Idg · faultedBEGINNING T/O ROLL ON RWY 18L AT MEM, RECEIVED R GEN DRIVE EICAS T/O REJECTED AT 7 KTS GROUND SPEED. EXITED RUNWAY. RAN QRH, DIRECTED RIGHT GEN DRIVE DISCONNECT, APU STARTED, REJECTED LANDING CHECKLIST ACCOMPLISHED AND AFTER LANDING CHECKLIST. RETURNED TSDR FDEA202210262674Skin · damagedLEFT WING SLAT NO. 5 TRAILING EDGE WITH MISSING MATERIAL. LEFT WING SLAT NO 5 TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG. 201 SHEET 1-2, PAGE 1-2 AND SRM 51-70-10-2R REP. 4, FIG. 202 SHEET 8, PAGE 149, 162, 163 REV. 82 12-15-21SDR FDEA202210222644Former · crackedL/WING FLE OSS 499 HAS A CRACKED FORMER REPLACED FORMER B67-57-002-03 AT L/WING FLE OSS 499 USING EA H-5720-T0371261 AS REFERENCE.SDR FDEA202210192611Apu · inoperativeAPU SHUTDOWN- FAULT LIGHT AFTER T.O. APPROXIMATELY 2000 FEET. APU IS REQUIRED PER MEL 24-00-01-01-B. ATTEMPT RESTART AS PER QRH. RESTART SUCCESSFUL. ON ARRIVAL APU SHUTDOWN AND FAULT INDICATED AGAIN. PERFORMED APU BITE PROCEDURE IAW FIM 49-11 FAULT TREESDR FDEA202210172589Former · crackedL/H FIXED LEADING EDGE FORMER CRACKED AT OSS 441 0000280794 : SHAEFFER, DAVID C - 18-OCT-2022 04:30 REPLACED CRACKED FORMER REF EA TH-5720-T0371169 P1SDR FDEA202210082517Skin · dentedLEFT WING OUT BOARD TRAILING EDGE FLAP WITH DENT (LOWER SURFACE) LEFT WING OUTBOARD FLAP T/E, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-7 AND B767 SRM 51-70-03-0G PARAG. 5.A.(1) FIG. 5 PAG. 19, 36 REV. 82 DEC 15/2021SDR FDEA202210072515Wedge · gougedRS WING #8 SLAT AT FLE OSS 499 ON TRAILING EDGE UNDERNEATH AT GOUGED (1" FWD OF TRAILING EDGGE) #8 SLAT GOUGED AREA ON LWR TRAILING EDGE WEDGE, REPAIR DONE AT RS SLAT LOCATION OSS 499 (SIZE 2.4Ï¿½ X .3Ï¿½) USING EA H-5750-T0371016P1 (REPAIR & RSC EA) & 767SDR FDEA202210072513Former · crackedR/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-14) REPLACED PARTS WITH NEW FORMER B67-57-002-04 ALONG WITH ANGLE B67-57-003-04 ON RS FOR FLE OSS 499, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND NSDR FDEA202210072512Former · crackedR/H WING AT STATION OSS.441 L/E FORMER IS CRACKED (P/N: 114T2170-6) REPLACED PARTS WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FOR FLE OSS 441, ATTACHED FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND SDR FDEA202210072511Former · crackedL/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-13) REPLACED PARTS WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON LS FOR FLE OSS 499, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND NSDR FDEA202210072510Former · crackedL/H WING AT STATION OSS.441 L/E FORMER IS CRACKED (P/N: 114T2170-5) REPLACED PARTS WITH NEW FORMER B67-57-002-01 ALONG WITH ANGLE B67-57-003-01 ON LS FOR FLE OSS 441, ATTACHED FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS AND SDR FDEA202210062501Former · crackedLH WING HAS A CRACKED LEADING EDGE FORMER AT SLAT #5 INBOARD TRACK AREA REPLACED PARTS WITH NEW FORMER B67-57-002-01 ALONG WITH ANGLE B67-57-003-02 ON LS FOR FLE OSS 441, ATTACH FORMER THROUGH SKIN AND REPLACE ALL LOOSE FASTENERS ON FLEÏ¿½S. WITH SCREWS ANSDR FDEA202210052475Former · crackedRH WING - FIXED LEADING EDGE STRUCTURE AT WING STA 499 HAS A CRACKED FORMER BRACKET,MWT. 0000392280 : BILLMAN, CRAIG B - 05-OCT-2022 23:14 REPLACED LEADING EDGE FORMER AS REQUIRED PER EA-H-5720-T0370963 PT1.SDR FDEA202210052474Former · crackedRH WING - FIXED LEADING EDGE STRUCTURE AT WING STA 441 HAS A CRACKED FORMER BRACKET,MWT. REPAIRED PER E.A. H-5720-T0370963 P1. REPLACED CRACKED FORMERSDR FDEA202210052473Former · crackedL/H WING LEADING EDGE FORMER CRACKED WITH ONE EACH SHEARED CHERRY MAX RIVET AT LS FLE OSS 499.60. REPLACED L/W L/E FORMER STA OSS 499.6 REF E.A. H-5720-TO370966 P1.SDR FDEA202210052472Former · crackedL/H WING LEADING EDGE FORMER CRACKED WITH ONE EACH SHEARED CHERRY MAX RIVET AT LS FLE OSS 441.60. M.W.T. 0000301922 : VERNON, JAMES L - 05-OCT-2022 22:55 REPLACED L/W L/W FORMER STA. OSS 441.6 REF E.A. H-5720-T0370966 P1SDR FDEA202210052471Wedge · dentedLEFT WING SLAT NO. 6 TRAILING EDGE WEDGE WITH DENT. RH WING SLAT #6 TRAILING EDGE WEDGE UPPER SURFACE AT POSITION ISS 231-236 SKIN WAS REPAIRED IAW SRM 51-70-10-2R REP. 4 PAG. 143-154 FIG. 201, SRM 57-43-02-2R FIG. 201 PAG. 1-2 REV. 82 DEC15/2021SDR FDEA202210012442Case · damaged#1 ENGINE FWD FAN CASE, FWD OUTER LINER AT 1-2 O'CLOCK POSITION IS DAMAGED AROUND INBD INLET TEMP SENSOR. REF CF6-80C2 BOEING MM 72-22-02. IPC REF 72-33-01-05 ITEM 95, ORDERED LINER SEGMENT CPN 7214605 AOG ON MSN 2121530. MARKED WITH TAPE. C/W E.A. H-7233SDR FDEA202210012441Former · crackedRIGHT WING LEADING EDGE FORMER AT #5 SLAT WING STATION OSS 441 HAS EVIDENCE OF DAMAGE. REPLACE PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441, ON LS FLE OSS 441, ATTACHED THE FORMER THROUGH THE SKIN AND REPLACE ALL LOSDR FDEA202210012440Former · crackedRIGHT WING LEADING EDGE FORMER AT #5 SLAT WING STATION OSS 441 HAS EVIDENCE OF DAMAGE. MWT REPLACE PART WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441, ON LS FLE OSS 441, ATTACHED THE FORMER THROUGH THE SKIN AND REPLACE ALSDR FDEA202209302421Former · crackedR/H WING LEADING EDGE FORMER AT OSS 441 BROKEN. MWT REPLACED FORMER 114T2170-6 & ANGLE 114T2171-4 WITH NEW FORMER B67-57-002-02 ALONG WITH ANGLE B67-57-003-02 ON RS FLE OSS 441 USING EA (WRI 57-20/2556) H-5720- T0370878 P1 AS REFERENCE.SDR FDEA202209292397Former · crackedL/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-13) REPLACED FORMER (B67-57-002-3) AT LS FLE OSS 499 USING EA H-5720-T0370864P1 AS REFERENCE.SDR FDEA2022093092397Former · crackedL/H WING AT STATION OSS.499 L/E FORMER IS CRACKED (P/N: 114T2511-13) REPLACED FORMER (B67-57-002-3) AT LS FLE OSS 499 USING EA H-5720-T0370864P1 AS REFERENCE.SDR FDEA202209252369Former · crackedCRACK ON NOSE FORMER OSS 441.596 L/H SIDE. REPLACED L/H LEADING EDGE FORMER AT STA OSS441 IAW E.A. H-5720-T0370796 PART1SDR FDEA202209252368Former · crackedR/H LEADING EDGE FORMER CRACKED AT OSS 441 REPLACED R/H LEADING EDGE FORMER AT STA OSS-441 IAW E.A. H-5720-T0370795 PART1
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