Boeing 767-338
Service difficulty reports · 1,328
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 = '767338' 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 = '767338' 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 ABXA20150527074Support Rib · corrodedNUMBER 2 FLAP OTBD SUPPORT HAS 1 ROTARY ACTUATOR HOLE WITH A DEFECT INDICATION ON HFEC ROTARY SCAN, HOLE IS LOCATED AT 2:00 LOOKING OTBD. REA B657-61551 ISSUED, REMOVED DISCREPANT HOLE, RE-SCANNED, NO DEFECTS NOTED. INSTALLED FREEZE PLUG & REAMED TO 1.380" ISDR ABXA20150527073Support Rib · corrodedNUMBER 1 FLAP SUPPORT INBD FLANGE HAS 2 ROTARY ACTUATOR HOLES WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN, HOLES ARE AT 10:00 AND 10:30 LOCATIONS LOOKING OTBD. AFTER CLEANING & RE-CANNING DISCREPANT HOLE AT 10:00 POSITION, NO FURTHER DEFECTS NOTED. REA B 657SDR ABXA20150524071Skin · crackedELT ANTENNA LOCATION, SKIN HAS HFEC CRACK INDICATION AT MID OTBD ANTENNA MOUNT HOLE. REPAIRED ELT ANTENNA SKIN AT MID OTBD ANTENNA MOUNT HOLE IAW EWO NR 57133-0000-0005 & SRM 53-00-01 REPAIR 14. SDR INFO, PN 146T1331-1, PART NAME SKIN, SN NSN, CRACKED .200, SDR ABXA20150521069Skin · chafedVERTICAL STABILIZER ACCESS 324AL FUSELAGE MOUNTED FWD & AFT FLANGE COMMON TO PANEL MATING SURFACE CHAFED. R & R SKIN FAIRING IAW SRM 51-40-05 & 51-40-02. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. APPLIED TOP COAT IAW AMM 51-21-10. SDR INFO, CORRODED PNSDR ABXA20150507070Skin · crackedRIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND TWO FASTENERS IN SECTION 48B, STATION 654.5 BETWEEN STRINGER 3R & 4R. REPAIRED CRACKED SKIN ON EXTERNAL FUSELAGE AT STATION 1654 IAW SRM 53-00-01. SDR INFO, PN 148T3121, PART NAME FUSELAGE SKIN, SN NSN, CRACKED LENSDR IXXA20150506076Light · intermittentEMERGENCY DOORS DISCREET LIGHT ON OVERHEAD PANEL ILLUMINATES INTERMITTENTLY, NO ACCOMPANYING EICAS MSG. R & R EMER DOORS DISCRETE LIGHT ASSEMBLY ON OVERHEAD PANEL IAW WPSM 20-84-18. OPERATIONAL CHECKED SATISFACTORY.SDR ABXA20150106001Manifold · crackedLEFT ENG LOW PRESS TURBINE VIBRATION LEVEL AT 4.8 - 5.0 DURING FLIGHT. CRACKS FOUND ON THE ENGINE’S TURBINE CASE COOLING MANIFOLD. REPLACED LT ENG. CAUSE UNKNOWN AT THIS TIME. PENDING ENG SHOP FINDINGS.SDR IXXA20140910030Beam · corrodedTRAILING EDGE LOWER PANEL ATTACH CHORD SPOILER SPLIT ON EDGE. OTBD LOWER SPOILER BEAM CHORD R & R IAW REA 47112REA05.SDR IXXA20140910028Door Sill · corrodedCORROSION OUT OF LIMITS ON MAIN DECK CARGO DOOR CUT OUT LOWER SILL LOWER SEAL DEPRESSOR. REPAIRED AREA IAW ENGINEERING ASSISTANCE DOCUMENT 47112REA06.SDR IXXA20140910029Support · crackedLEFT WING ROTARY ACTUATOR SUPPORT NR 1 THREE CRACKED HOLES AT 11 O'CLOCK, 12 O'CLOCK & 5 O'CLOCK POSITION. THREE CRACKED HOLES OF THE LT WING ROTARY ACTUATOR SUPPORT REPAIRED IAW REA 47112REA04.SDR ABXA20140812259Intercostal · corrodedCORROSION BETWEEN STATION 544 - 566 LBL45 AT BALL MAT NUTPLATE ATTACH POINT. REMOVED CORROSION IAW SRM 51-10-00, REPAIRED AREA AT LBL 45 BETWEEN 544 - 566 IAW SRM 51-70-11. CORRODED LEVEL 2, PN 143T5021, PART NAME INTERCOSTAL, SN NSN, FS & BS LOC FROM 544 TOSDR ABXA20140812257Frame · crackedFUSELAGE FRAME FAIL SAFE AT BS 904 LT IS CRACKED AT THE LOWEST FASTENER BELOW FLOOR. REPAIRED FUSELAGE FRAME CHORD AT BS 904 LT IAW JC EA 53000051-101. PN 691T0003T51, PART NAME INNER CHORD, SN NSN, CRACKED LENGTH 1.1, EXACT FS & BS LOC ON ACFT 904. ACFT WASDR ABXA20140810258Skin · crackedFUSELAGE SKIN CRACKED IN TWO PLACES AT FS 1658, STRINGER 12A LT. CUT OUT DAMAGED SKIN, FABRICATED DOUBLER & FILLER FROM 7075T6 .071 & .063 PO 0050971 & 0053815 & INSTALLED IAW SRM 53-00-01, REPAIR 1. TREATED, PRIMED & TOPCOAT IAW SRM 51-20-01. PN 148T3131-5SDR IXXA20140910027SStiffener · crackedNUMBER 2 PYLON AFT SIDE OF STRUT, LT & RT STIFFENERS CRACKED. OLD STIFFENERS REMOVED. NEW STIFFENERS FABRICATED IAW DWG 313T3380 & INSTALLED IAW SRM 51-40-02. PROTECTIVE COATING APPLIED IAW SRM 51-20-01.SDR IXXA20140910026SStructure · corrodedCORROSION NOTED NR 1 PYLON LBL 4 TO LBL 5, WL 123 TO WL 125. R & R CHORD IAW SRM 51-40-02.SDR IXXA20140910031Angle · crackedCRACKED ANGLE AT NR 1 LOWER STRUT FAIRING OTBD AFT UPPER CORNER. R & R CRACKED ANGLE IAW SRM 51-40-02.SDR IXXA20140910024SRib · crackedLEFT WING INTERNAL LE, AIR LOAD CRACKED AT THE UPPER ATTACHMENT NEAR ILES 685.0 HFEC VERIFIED. R & R LT WING LE AIR LOAD RIB & WEB AT LWS 685 IAW SRM 51-40-02.SDR IXXA20140910022SRib · crackedLEFT WING INTERNAL LE, AIR LOAD RIB CRACKED AT THE UPPER ATTACHMENT NEAR ILES 651.1 HFEC VERIFIED. R & R AIR LOAD AT UPPER ATTACHMENT IAW 57-41-09 & 51-40-02 & SRM 51-40-03. PAINTED & C1C PROTECTED IAW SRM 51-20-01 & SRM 53-50-01.SDR IXXA20140910021Rib · crackedLEFT WING INTERNAL LE AIR LOAD RIB IS CRACKED AT THE UPPER ATTACHMENT AT ILES 500.0 VERIFIED WITH HFEC. REPLACED LOWER CHORD FOR UPPER ATTACH POINT IAW SRM 57-41-09 & SRM 51-40-02. TREATED & PAINTED WITH CIC PROTECTION IAW SRM 51-20-01 & SRM 53-50-01.SDR ABXR201400006Support · corrodedRIGHT OTBD FLAP NR 7 SUPPORT OTBD FLANGE HOLE HAS DEFECT INDICATION WITH EDY CURRENT. REPAIRED IAW REA.SDR ABXR2014070400005Support · corrodedLEFT OTBD FLAP NR 1 SUPPORT OTBD FLANGE HOLE HAS DEFECT INDICATION WITH EDDY CURRENT. REPAIRED IAW REA.SDR ABXR2014070400004Stringer · crackedBS 654+22, STR 17L CRACKED. REPAIRED STRINGER IAW SRM.SDR ABXR070400003Stringer · crackedBS 654+22, STR 11L CRACKED. R & R STRINGER SECTION IAW SRM.SDR ABXR070400002Support Beam · corrodedLEFT WING T/E UPPER PANEL SUPPORT BEAM CORRODED WS 235. REPAIRED IAW SRM.SDR IXXA20140609006Support · damagedRIGHT OTBD FLAP NR 7 SUPPORT OUTBOUND FLANGE HOLD AT 2 O'CLOCK HAS DEFECT INDICATION WITH ROTARY SCAN. POSSIBLE CORROSION OR PITTING. REPAIRED FLANGE AT 2 O'CLOCK POSITION TO .480. FREEZE PLUG INSTALLED & DRILLED TO NOMINAL LIMITS IAW REA 47100REA01.SDR IXXA20140609005Support · damagedLEFT OTBD FLAP NR 1 SUPPORT OTBD FLANGE HOLE AT 12 O'CLOCK HAS DEFECT INDICATION WITH ROTARY SCAN. POSSIBLE CORROSION OR PITTING. REPAIRED FLANGE AT 12'O CLOCK POSITION TO FINAL OF .480. FREEZE PLUG INSTALLED & DRILLED TO NOMINAL LIMITS IAW REA 47100REA01.SDR IXXA20140605004Stringer · crackedSTATION 654+22 STRINGER 17L CRACKED 5 INCHES. REPAIRED STRINGER 17L AT STATION 654+22 IAW SRM 53-00-03.SDR IXXA20140603003Support Beam · corrodedLEFT WING TE UPPER PANEL SUPPORT BEAM CORRODED ON UPPER FLANGE ALONG ENTIRE LENGTH AT WS 285. R & R LT WING TE SUPPORT BEAM IAW SRM 51-40-02.SDR ABXA2014051394Skin · puncturedTHREE INCH SQUARE PUNCTURE THROUGH FUSELAGE SKIN BETWEEN FUSELAGE STATIONS 1373 & 1395 BETWEEN STRINGERS 26R & 27R. REPAIRED IAW SRM 53-00-01, REPAIR 12 WITH SLIGHT DEVIATIONS DUE TO DAMAGE BEING NEAR AN EXTERNAL LIGHT & A BUTT JOINT. .
SDR ABXA2014031738Engine · bird ingestionON TAKEOFF, BIRD STRIKE TO THE RT ENG. HIGH EGT, 1025 DEGREES FOR 2 SECONDS. RT ENG SHUT DOWN, AIR TURN BACK.SDR ABXA2014010804Strut · crackedNUMBER 2 SLAT OTBD AUXILIARY TRACK ATTACH FITTING OTBD LOWER STRUT SPLIT ON EDGE. INSTALLED NEW LOWER STRUT IAW SRM 51-40-02 & REA NR B657-60825-MR. SDR INFO 1/2 INCH CRACK, PN 114T2224-15, PART NAME STRUT, SN NSN, LOC AT 0SS 937.929. ACFT WAS GROUNDED.SDR ABXA2014010803Slat · corrodedNUMBER 4 SLAT UPPER LE SKIN SURFACE CORRODED & BUBBLED. NR 4 SLAT CORRODED OUT OF LIMITS. R & R SLAT IAW AMM 27- 581-02, OPERATIONS CHECKED GOOD. SDR INFO LEVEL 2 CORROSION, PN 114T4104-53, PART NAME SLAT, SN 000742, LOC FROM LES 500 TO LES 690. ACFT WAS SDR ABXA2014010706Retainer · crackedNUMBER 1 INBD NACELLE AT HYD BAY HAS A CRACKED SEAL RETAINER IN THE MIDDLE AREA. R & R SEAL RETAINER IN THE MIDDLE SECTION OF NR 1 NACELLE HYD BAY DOOR IAW SRM 51-40-02, PAR 7, PG 4. SDR INFO CRACKED LENGTH 1, 1.5 INCHES PN 313J2380-269, SN NA, PART NAME SEASDR ABXA2014010705Bracket · crackedTHREE ANGLE BRACKETS ON THE LOWER INTERIOR EDGE OF THE NR 6 SLAT ARE TWO EACH CRACKED & ONE EACH HAS LOOSE HARDWARE, APPROXIMATE STATION 281. R & R TWO EACH CRACKED BRACKETS & RE TORQUED LOOSE HARDWARE ON ONE EACH BRACKET ON NR 6 SLAT APPROXIMATE STATION OSS SDR IXXA20131223044Bracket · crackedLEFT MLG DOOR LOOSE. FWD BRACKET ON MLG DOOR BROKEN. REPLACED FWD TRUNNION DOOR HINGE FITTING & INSTALLED LT TRUNNION DOOR IAW B767 AMM 32-12-11.SDR ABXA20131009578Computer · failedENROUTE, LEVEL AT FL350 CENTER AUTOPILOT SHORTLY THERE AFTER NOTED BRIEF ODOR OF SMOKE. DEFERRED, CLEARED 10/08/2013-PERFORMED OHM CHECK OF WIRING FROM FCC COMPUTER TO AILERON, DIRECTIONAL AND ELEVATOR SERVO'S NO DEFECTS NOTED. R & R CENTER FCC IAW AMM 22-11SDR IXXA20131002037Angle · crackedNR 1 ENGINE PYLON INSPECTION, FOUND A CRACK AT ANGLE AT INTERCOSTAL TO FORWARD MIDSPAR FITTING. R & R ANGLE IAW SRM 51-40-2. ACFT GROUNDED.SDR ABXA20130929575Skin · corrodedLEFT HORIZONTAL STABILIZER HAS A SPOT OF CORRORSION ON UPPER SURFACE AT HSBL 264. BLENDED AREA OF CORROSION ON UPPER SURFACE AT HSBL 24 IAW SRM 51-10- 00. REPAIRED SKIN BLENDOUT IAW REA B655-60721-MR. CLOSED ACCESS PANELS IAW SRM 51-40-02, PAR 7. LEVEL 2 CORSDR ABXA20130924573Skin · corrodedLEFT HORIZONTAL STAB HAS A SPOT OF CORROSION ON UPPER SURFACE AT HSBL 336. REPAIRED DAMAGE CAUSE BY CORROSION IAW REA B655-60720-MR. LEVEL 2 CORROSION, PN: 182T3200, SKIN PANEL, HSRL 334 TO HSBL 336, REAR SPAR TO REAR SPAR. ACFT WAS GROUNDED.SDR ABXA20130917574Access Panel · corrodedFOUND CORRORSION ON AFT FLANGE FOR REFUELING PANEL 521QB. REMOVED CORROSION IAW SRM 51-10-02 COMPLIED WITH REA 657-60710. ACFT WAS GROUNDED.SDR ABXA20130924546Warning Message · false activationAFTER BLOCKOUT, EICAS MESSAGE RT ENGINE FIRE LP1. PERFORMED RT ENGINE FIRE LP1 OPS CHECKED IAW AMM 23-11-00. EICAS ERASE PROCEDURE IAW AMM 31-41-00-2. NO FURTHER FAULTS NOTED. OPS CHECKED NORMAL.SDR QLMF2013F00150Wire Harness · damagedDURING VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING 767-28A0053, REV 03. MINOR DAMAGE WAS FOUND TO OUTER SLEEVING AT A CREASE MARK. FURTHER INSPECTION TO WIRING CARRIED OUT IAW SB 767-28A0053 WITH NO SIGNS OF DAMAGE.SDR QLMF2013F00146Sleeve · shortHEAVY MX HAS BEEN CARRIED OUT, VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING ON ACFT IAW MFG SB 767-28A0053, REV 03. LT AFT BOOST PUMP M333 D01542: SMALL HOLE 2 FT 9 INCHES UP FROM THE CONNECTOR, OUTER SLEEVE TOO SHORT. SOME WEAR ALONG THE OUTER SLESDR ABXA20130629476Skin · crackedDENT BS 500 S17-18L. SKIN DETERMINED CRACKED. REPAIRED SKIN IAW SRM 53-00-01. REMOVED AND REINSTALLED SIDEWALL PANELS AND KICK PANEL IAW AMM 75-27-09-4 AND REA B653-60595-MR, ACFT WAS GROUNDED.SDR QMLF201306270137Sleeve · shortDURING INSP OF THE LT WING FUEL PUMP WIRE HARNESS CONDUITS, FOUND THE SPAR TO M636 (LT AUX FUEL PUMP) HAD A HOLE IN THE TEFLON SLEEVING AND THE CONDUITS FOR M1730 (LT FUEL JETTISON PUMP) DID NOT EXTEND FULLY TO THE FIRST P-CLAMP ON BACK OF SPAR. BOTH ELECTRISDR ABXA20130625474Beam · chafedTHREE CHAFED AREAS ON LOWER BEAM AFT OF SECOND PANEL LATCH FOR 437BR. R & R HYD BAY ACCESS DOOR LOWER BEAM IAW SRM 51-40-02. PYLON BEAM INBD.SDR ABXA20130620475Attach Fitting · crackedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT STRUCTURE BETWEEN STAB REAR SPAR AND T/E IS CRACKED ON FWD RT FLANGE ACCESS THROUGH PANEL 324CLX FS 1746. R & R ATTACHED STRUCTURE ANGLE IAW SRM-300 51-40-02. ACFT WAS GROUNDED.SDR 2013F00130Wire Harness · damagedVISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING IAW SB 767-28A0053, REV 03. OUTER SLEEVING ON RT FWD AND RT AFT FUEL BOOST PUMP LOOMS BOTH HAVE MULTIPLE SPLITS AND WORN AREAS ALONG THEIR LENGTH. NO DEFECTS FOUND WITH INNER SLEEVES OR ELECTRICAL CABLES.SDR 2013F00128Sleeve · damagedHEAVY MX HAS BEEN CARRIED OUT. VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING IAW SB 767-28A0053, REV 03. THIS INSPECTION IS MANDATED BY AD/B767/123 (FAA AD 2000-11-06 AMDT 39-11754 REFERS) ISSUED BY (CASA). DURING RT AUX TANK OVERRIDE, JETTISON WIRESDR 2013FA0000287Sleeve · splitDURING RT MAIN TANK BOOST PUMPS WIRE BUNDLES INSPECTION FOUND SLEEVES SPLIT AND NOT IN ONE CONTINUOUS PIECE THROUGH THE CONDUIT, FUEL PUMPS WIRE BUNDLES INSPECTED SERVICEABLE. RT MAIN TANK BOOST PUMPS WIRE BUNDLES SLEEVES REPLACED IAW SB 767-28A0053, REV 3.
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