Boeing 767-306
Service difficulty reports · 2,510
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 = '767306' 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 = '767306' 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 P5CA2016062800152Light · inoperativeRT GENERATOR DRIVE DISC, DRIVE LIGHT NOT ON WITH ENGINE SHUTDOWN. LIGHT TEST OK. RELAMPED RT GEN DRIVE DISC, SWITCH IAW AMM 33-13-00. PERFORMED OPS CHECK TEST OK, RT IDG IAW AMM 24-11-01. OPS CHECK GOOD.SDR P5CA2016061900144Acm · malfunctionedLEFT PACK TEMP EICAS MSG ON TAXI PLACED LT PACK ON MDDR 67656 IAW MEL 21-51-01-01. MAINTENANCE PROCEDURES C/W PLACARD INSTALLED. LT PACK WILL NOT RESET IN AUTO OR STANDBY. REMOVED AND REPLACED LT ACM MM 21-51-07. REMOVED AND REPLACED HOT AIR SUPPLY TUBE IASDR P5CA2016061900145Unknown · odorVERY STRONG SMOKE ODOR ON TAXI. INSPECTED UPPER CARGO COMPARTMENT, LWR FWD AND AFT CARGO COMPARTMENT. INSPECTED LT AND RT PACK COMPARTMENT. NO EVIDENCE OF SMOKE FOUND IAW AMM 05-51-56.SDR P5CA2016061900143Relay · failedLEFT FWD FUEL BOOTS PUMP AUTOMATIC FUNCTION INOPERATIVE. TRANSFER TO MEL 28-22-01-01. T/S SYSTEM USING WIRING DIAGRAM 28-25-11, 28-22-11, AND FIM TASK 28-25, FAULT TREE 808. REPLACED LT FWD PUMP PWR SENSE RELAY K513 IAW SWPM CH 20-81-19, SYSTEM CK'S GOOD IASDR P5CA2016061200134Controller · malfunctionedRIGHT ENGINE PRV STATUS MSG. R & R RT ENGINE PRV AND PRV CONTROLLER IAW AMM LEAKS AND OPS CHECK GOOD, AMM 36-11-18 AND AMM 36-11-19.SDR P5CA2016060300123Warning Light · false activationAUTOMATIC FUNCTION OF LT FWD PUMP WHEN APU RUNNING LOW PRESSURE LIGHT REMAINS ILLUMINATED. ACCOMPLISHED SUCESSFUL OPS CHECK OF FWD LT BOOST PUMP REF AMM 49-11-00. OPS GOOD ON SEVERAL CYCLES. NO PREVIOUS HISTORY. OK FOR SERVICE.SDR P5CA2016053100121Escape Rope · unwanted deployNR 2 & NR 4 DESCEND DEVICES FOUND DEPLOYED UPON ARRIVAL. R & R DESCENT DEVICES IAW SMM 25-61-63.SDR P5CA2016042000082Warning Message · false activationDURING CLIMBOUT, LEFT DUCT PRESSURE NOTED AT 55 PSI. RIGHT INDICATED NORMAL PRESSURE AT 35. NO EICAS MESSAGE WAS DISPLAYED. PRESSURE NORMALIZED DURING CRUISE FLIGHT. AIR SUPPLY BITE PROCEDURE C/O IAW FIM 36-20 WITH NO FAULT NOTED, AS WELL AS ENGINE GROUND RSDR P5CA2016041900080Plug · looseDURING WALK AROUND, FOUND OIL LEAK NR 1 ENGINE FOUND PLUG ON NR 1 ENGINE FUEL/OIL COOLER LOOSE, TIGHTENED PLUG TO 45 FT/LB AND SAFE TIED. REF 79-21-01. LEAK CHECKED OK AT THIS TIME.SDR P5CA2016021400033Switch · malfunctionedEMERGENCY LIGHTS COME ON WHEN A/C POWER IS SHUTOFF. EMERGENCY LIGHTS SWITCH WAS IN OFF. REPLACED EMERGENCY LIGHT SWITCH IAW WDM 33-51-11. SYSTEM OPS CHECKED GOOD IAW AMM 33-51-00.SDR P5CA2016020400018Exciter · faultedPERFORMED APU COLD SOAK START, DID NOT START. APU FAULT EICAS APPEARED. LP 696503, ITEM 1: ITEM TRANSFERRED DO DMI MDDR 64015, PLACARD INSTALLED. APU INOPERATIVE ER OPERATIONS NOT ALLOWED. T/S ECU- IGN UNIT FAULTY. ITEM M3: R & R EXCITER BOX IAW 49-41-03. OSDR P5CA2016012500014Proximity Switch · malfunctionedPROBE HEAT EICAS WOULD NOT CLEAR AFTER ENGINE START. REPLACED RT MLG PROXIMITY SWITCH IAW AMM 32-09-07-002. OPS CHECK GOOD.SDR P5CA2015123100225Terminal · looseEICAS MESSAGE LT FWD WINDOW. FOUND WINDOW POWER INPUT TERMINAL LUG BOLT, ONE SIZE TOO BIG, CONNECTOR FOUND LOOSE AND ARCING. REPLACED BOLT, OPS CHECK GOOD REF AMM 56-11-01 FOR TERMINAL INSTALLATION.SDR P5CA2015123000220Anti-Ice Valve · malfunctionedSTATUS MSG, "RT ENGINE TAI VALVE. R & R RT ENGINE TAI VALVE IAW AMM 30-21-03. ACCOMPLISHED GROUND OPS CHECK, SYSTEM OPS CHECK NORMAL.SDR P5CA2015123000221Controller · malfunctionedLEFT FWD WINDOW HEAT INOPERATIVE. TS LT FWD WINDOW HEAT INOPERATIVE, FOUND POPPED CIRCUIT BREAKER ON P36. RESET CB IAW MCC, REPLACED WHCU FOR LT FWD WINDOW. OPS CHECKS GOOD IAW AMM 30-41-01.SDR P5CA2015122800218Bleed Valve · malfunctionedAPU AUTOSHUTDOWN, FAULT LIGHT ILLUMINATED. ECU BITE SHOWED REVERSE FLOW MSG. APU BLEED SURGE VALVE REPLACED IAW AMM 49-53-01 OPS CHECK OK NEW ECU BITE NO FAULTS.SDR P5CA2015122600216Window · failedLT FWD WINDOW HEAT INOPERATIVE. INTERMITTENT FAILURE. REMOVED L1 WINDOW AND TEMP INSTALLED NEW WINDOW IAW MM 56-11-01-004-039. COMPLETED INSTALL OF L1 WINDOW IAW AMM 56-11-01, OPS CHECK GOOD AT THIS TIME. COMPLETED STEP 17 AT 1401.SDR P5CA2015122400215Controller · inoperativeLEFT FWD WINDOW INOPERATIVE. R & R CONTROL UNIT IAW MM 30-41-00, OPS CHECK GOOD AT THIS TIME.SDR P5CA2015122000212Shutoff Valve · warning messageRIGHT ENGINE HPSOV, RT ENGINE TAI VALVE STATUS MESSAGE. R & R RT ENGINE HPSOV IAW AMM 36-11-07. OPS AND LEAK CK GOOD THIS CLEARS MDDR 62780 PLACARDS. REMOVED MCC NOTIFIED.SDR P5CA2015121700209Control Unit · malfunctionedAPU AUTO SHUTDOWN, MINI FLAG 17. T/S TO FAULT ECU, R & R APU ECU IAW AMM 49-61-05, OPS CHECK OK. R & R APU OIL SCAVENGE FILTER, LEAK CHECK OK. R & R APU GENERATOR OIL FILTER DIFFERENTIAL PRESSURE SWITCH, PN: 3876048-3, SN: 99071691539D, OPS CHECK OK.SDR P5CA2015121700210Idg · failedLOSS OF LT GENERATOR AT 1500 FT. ALL SHORT FINAL. ATTEMPTED ONE RESET. WOULD NOT RECONNECT. R & R LT IDG IAW AMM 24-11-01, OPS CHECKS GOOD, NO OTHER DEFECT NOTED AT THIS TIME.SDR P5CA2015121400207Receptacle · looseFWD L1 WINDOW INOP, HEAT, PERFORMED FIM TEST 30-41, FTR 803, AMBER CONTROL LIGHT CAME ON. IAW TABLE 102, MEASURED RESIST FROM J4 & J5-10.2 OHM. REMOVED CONTROLLER. NOTED REAR RECEPTACLE LOOSE. SECURED; REINSTALLED IAW AMM 30-41-01, TESTED.SDR P5CA2015121400205Skin · damagedPERFORMED REPAIR OF MULTIPLE EXTERNAL SKIN DAMAGES ON FUSELAGE SECTION 43 AND 46, BS 434 TO 654+44 B/T S-39L AND S-39R, BS 1197+110 TO 1480 B/T S-26R AND S-36R AND AT S-31L, REF NRC M0023-M0026, M0033, M0035 AND M0036. REPAIR PERFORMED IAW REA MF01084R0094, RSDR P5CA2015121400206Battery Pack · inoperativeFWD BATTERY PACK EMERGENCY LIGHT INOPERATIVE, REF IAI NRC M0568. REINSTALL BATTERY PACK EMERGENCY LIGHT IN FWD POS IAW J/C 371-25-C5066-001-AV, CHECK OK, AFTER CAPACITY TESTED AND INSPECTED IN SHOP.SDR P5CA2015121400204Strut · crackedCRACK REPAIR ON STRUT NR 2 INBD SIDE SKIN PANEL, NAC BS 221.25 TO 237.5, REF NRC M0538, REPAIR PERFORMED IAW REA MF01084R0148, REV NEW, DATED 29 OCT 15, REA MF0108R0148, REV A, DATED 15 NOV 15 AND AS INSTRUCTED BY SR 4-3029397194, MESSAGE.SDR P5CA2015121100187Floorbeam · corrodedCORROSION DAMAGE AT FUSELAGE BS 246 MAIN DECK FLOORBEAM - MID CHORD, PN 141T5814-158, WL200, BETWEEN RBL 55 AND RBL 73, REF IAI NRC M0066. REPAIR PERFORMED IAW SRM 53-10-51, FIGURE 201, REPAIR 2, AS CATEGORY A, PERMANENT REPAIR. THIS REPAIR CLASSIFIED AS MAJSDR P5CA2015121100188Stringer · crackedCRACK ON STRINGER 1L LOCATED AT FUSELAGE BS-368, REF IAI NRC C0028. REPAIRED SRM 53-00-03, FIG 201, REPAIR 1 AS CATEGORY A, PERMANENT REPAIR. THIS REPAIR CLASSIFIED AS MAJOR BY EO 6753A258, REV 0.SDR P5CA2015121100189Skin · damagedSCRATCHES ON FUSELAGE SKIN, BUTT JOINT AND LAP JOINT, AT BS 196.5, STR 21R, REF IAI NRC M0315. REPAIR PERFORMED IAW IAI REA MF01084R0113, REV, NEW, AND AS INSTRUCTED BY SR 4-2989086791. THIS REPAIR, RELATED TO AD 2010-06-16, SB 767 53A193, R2 AND SRM 53-00-0SDR P5CA2015121100191Skin · damagedDEEP ABRASION DAMAGE REPAIR AT FUSELAGE SKIN BS 390-412, STR 22L-23L, REF IAI NRC M0022, REPAIR PERFORMED IAW SRM 53-00-01, FIG 201, REPAIR 29 IAW REF SRM THIS REPAIR IS A CATEGORY B: REPAIR. INITIAL INSPECTION THRESHOLD IS AT 37500 FC, TOTAL.SDR P5CA2015121100193Hinge Fitting · damagedHINGE FITTING ASSY, WEAR DAMAGE REPAIR ON ENGINE'S NR1 FAN COWL BS 188.2, REPAIR PERFORMED IAW REA MF01084R0071, REV A DATED 13OCT15.SDR NOCA04311Support Channel · corrodedFOUND CORROSION ON 3 LAV THRESHOLD SUPPORT CHANNELS. REMOVED CORROSION OUT OF LIMITS. REMOVED AND REPLACED SUPPORT CHANNELS AS PER MM 51-21-03.SDR NOCA20110112001Angle · crackedSUPPORT CAP CRACKED LEFT WING L/E CAVITY LES 550.10. REMOVED LOWER CHORD P/N 114T2207-5 AND LOWER NUT PLATE ANGLE DRILLED UP NEW ANGLE AND PRIMED. INSTALLED NEW ANGLE AS DRAWING 114T2207 AND PER SRM 57-41-04.SDR NOCA03511Angle · crackedANGLE CRACKED NR 2 ENGINE SAILBOAT FAIRING A-FRAME. REPLACED CRACKED ANGLES AS PER SRM 51-10-02.SDR NOCA03411Angle · crackedLEFT WING STA 550 NR 4 SLAT INBD OF INBD TRACK ANGLE CRACKED. REMOVED OLD ANGLE PER SRM 51-10-02. DRILLED UP NEW ANGLE AND INSTALLED AS PER SRM 51-20-05.SDR NOCA03211Angle · crackedLT WING STA 500 UNDER SLAT NR 5 OUTBOARD SIDE OF OUTBOARDD TRACK ANGLE CRACKED. REMOVED AND DRILLED REPLACMENT ANGLE AS PER SRM 51-10-22.SDR NOCA03111Rib · crackedAFT END OF L/E RIB CRACKED LES 662 AFT OF NR 9 SLAT. REMOVED ANGLE DRILLED AND INSTALLED RIB ANGLE AS PER SRM 51-10-02.SDR NOCA03011Crossmember · corrodedCORROSION AT KEEL BEAM CROSS MEMBER. REMOVED CORROSION AT KEEL BEAM CROSS MEMBER 2 TEES OUT OF LIMITS. REMOVED AND REPLACED KEEL BEAM CROSS MEMBERS AS PER SRM 53-50-12.SDR NOCA02611Slide · low pressureR4 DOOR SLIDE PRESSURE AT EXTREME LOW END OF NORMAL OPERATIONAL RANGE. REMOVED AND REPLACED R4 DOOR SLIDE AS PER NAA JOB CARD 767-25-029-01.SDR NOCA01311Door Frame · damagedFUSELAGE DAMAGED BY GROUND EQUIPMENT APPROXIMANT 3FT AFT OF L4 DOOR FRAME OUT OF SRM LIMITS. REMOVED DAMAGE AREA AS PER SRM 53-00-01. ACCOMPLISHED HFEC TO ENSURE ALL DAMAGED REMOVED, ACCOMPLISHED REPAIR AS PER SRM 53-00-01, EO 767-53-036, MAJOR REPAIR FORM 3SDR NOCA06410Light · inoperativeEMERGENCY LIGHTS INOP AT ROW 14B. REPLACED EMERGENCY LIGHT STRIPS AT 14B, OPS CHECK GOOD.SDR NOCA06310Connector · dirtyRIGHT ENG FIRE LP 1 STATUS MSG. CLEANED WAFER CONNECTORS AT M683 RIGHT ENGINE FIRE DETECTION CARD, T/S PER FIM 26-11-00 FIG 104 ALL LOOPS RESISTANCE & INSULATION CHECKS WITH IN LIMITS SYSTEM, OK FOR SERVICE.SDR NOCA05610Light · inoperativeL-3 DOOR EMERGENCY LIGHT INOP. RELAMPED AND TESTED L-3 DOOR EXTERIOR EMERGENCY LIGHT PER MM 33-51-00.SDR NOCA05510O-Ring · leakingACFT DIVERTED, DUE TO NR 1 ENGINE IDG ON MEL INOP AND APU AUTO SHUTDOWN IN FLIGHT DUE TO LOW OIL. APU OIL LEAK FOUND ON ITEM1, LOGPAGE 86747, DUE TO FAULTY O-RING AT OIL FILL CAP, FOUND APU OIL CAP DOWN AND LATCHED. SERVICED APU WITH 4 QTS OF OIL AND REPLACESDR NOCA05410Seal · leakingA/C 765 FLT 404 EN ROUTE TO FRU OUT OF LEJ, FLT CREW ADVISED THE APU OIL QUANTITY IS DECREASING AND EXPECT THE APU TO SHUT DOWN SHORTLY. WITH THE LEFT GENERATOR DEFERRED INOP AND THE LOOSE OF THE APU GENERATOR THE A/C WILL ONLY ONE ELEC SOURCE, AS SUCH THE A/SDR NOCA05310Generator · malfunctionedA/C N765 EN ROUTE RMS TO FRU ADVISED MCC THE LEFT GENERATOR DRIVE LIGHT CAME ON. FLT CREW PERFORMED QRH PROCEDURES GENERATOR DRIVE LIGHT STAYED ON. NOTE: THE APU WAS INOP. THE A/C DIVERTED TO LEJ. A SOFT OVERWEIGHT LANDING WAS ACCOMPLISHED OVERWEIGHT LANDISDR NOCA03810Fire Loop · inoperativeLEFT ENG / FIRE LOOP 2 STATUS MSG SEVERAL TIMES DURING FLT. PLACARD PER MEL 26-11-1 CAT C
NOTE. A/C DOWNGRADED TO 120 ETOPS DUE TO LEFT ENG FIRE LOOP 2 INOP CI 26-06.SDR NOCA02310Computer · malfunctionedAILERON LOCKOUT EICAS MSG. ACCOMPLISHED FIM TASK 27-11-00 FIG 104. ACCOMPLISHED BITE CHECKS, ALL CHECKS OK. REF AMM 22-00-02, MCDP TST 07 ACCOMPLISHED, NO FAULTS NOTED. RUDDER RATIO EICAS MSG. ACCOMPLISHED FIM TASK 27-21-00 FIG 104. ACCOMPLISHED BITE CHESDR NOCA04009Lamp · burned outTHE AIRCRAFT HAS A MISSED APPROACH / GO-AROUND ON APPROACH INTO BGR MX REP WAS CALLED TO THE FLIGHT DECK PER CAPTAINS REQUEST. MX REP RE-LAMPED THE INOP LIGHT, OPS CHECK OK.SDR NOCA02909Light · inoperativeEMERGENCY FLOOR LIGHT STRIP (RT SIDE FWD) NEEDS TO BE RELAMPED. RELAMPED EMERGENCY FLOOR PATH STRIP IAW MM 33-51-10-402-113. OPS CHECK OK.SDR NOCA02709Pca · failedRUDDERS LOCKED ON LANDING. TILLER NOSE WHEEL STEERING OK. ACCOMPLISHED ON PL 765-0905-03, PERFORMED FIM TASK 27-21-00 FIG 107. REMOVED ACCESS PANEL 324BL, 324EL, 324GL, 324JL, 324LL, PERFORMED VISUAL INSPECTION OF FEEL CENTERING AND TRIM MECHANISM, ALSO ALL
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