Boeing 767-31B
Service difficulty reports · 616
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 = '76731B' 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 = '76731B' 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 UIEA2022061300581Fuel Filter · installedLEFT & RIGHT ENGINE FUEL FILTERS REQUIRES REPLACEMENT AT APPROX. 150 FLT HOURS DUE TO FUEL TANK ENTRY TO BE REPLACE PRIOR TO 108387 FLT HOURS . REMOVED AND REPLACED #1 ENGINE FUEL FILTER PER 767 M/M 73-11-03-404-009-1100, REQUIRES LEAK CHECK. REMOVED &SDR UIEA2022061300582Surge Valve · faultyAPU BLEED VALVE INOP REMOVED AND REPLACED APU AIR SHUTOFF VALVE IAW B767 AMM 36-11-10. NO LEAKS FOUND PENDING OPS CHECK, OPS CHECK GOOD, BUT BLEED PRESSURE LOW. T/S PER FIM 49-11 FAULT TREE 979. FOUND SURGE CONTROL VALVE FAULTY. REMOVED & REPLACED APU SURGE SDR UIEA2022061300583Door · openOVER WING EMERGENCY EXIT DOOR'S LH & RH DEACTIVATE AND OPEN DOORS FOR INSPECTION REQUIREMENTS .DISARMED THE L/H & R/H OFF WING ESCAPE SYSTEM, REF 767 M/M 25-65-00-042-001. REMOVED L/H & R/H OVERWING ESCAPE HATCHES (4EA) REF 767 M/M 52-21-01-002-201. REF NRSDR UIEA2022061300584Fastener · missingENGINE # 1 EXHAUST NOZZLE WEAR PAD AT THE 7 O' CLOCK POSITION MISSING FASTENER (1) .INSTALLED MISSING FASTENER AT ENGINE # 1 EXHAUST NOZZLE WEAR PAD AT THE 7 O' CLOCK POS AS PER B767-300 SRM 51-40-02-0G-0.)SDR UIEA2022061300585Door · faultyOVER WING EMERGENCY EXIT DOORS CLOSE AND REACTIVATE LH & RH. AFTER INSPECTION COMPLETED. REINSTALLED BOTH LEFT & RIGHT OVER WING EXIT DOORS PER B767-300 AMM 52-21-01. PERFORMED OFF WING ESCAPE SYSTEM ON BOTH SIDES IAW B767-300 AMM 25-65-00. SQUIB TESDR UIEA2022061300586Safety Clip · damagedLOWER FUSELAGE, BOTH SAFETY PINS TO DEACTIVATE CYLINDER OF OVER WING SLIDES WITH FLAGS MISSING / DAMAGE. REMOVED & REPLACED LWR& FUSELAGE INFLATION CYLINDER DEACTIVATION PINS PER B767-300 AMM& 25-65-02.SDR UIEA2022061300587Seat Belt · damagedCOCKPIT 2ND OBS SEAT BELTS LH & RH TSO TADS ILLEGIBLE & DAMAGE.REMOVED AND REPLACED OBS SEAT BELT PER B767-300 AMM 25-11-00. OPS CHECK; GOODSDR UIEA2022061300588Clamp · damagedFWD, MID & AFT MEGAPHONE CLAMPS DAMAGE.(REMOVED AND REPLACED DAMAGED MEGAPHONE CLAMPS AT FWD, MID AND AFT MEGAPHONE AS PER 767-300 SRM 51-40-02-0G-0.</P>)SDR UIEA2022061300589Rod · unserviceableENG # 2 O/B FAN COWL, AFT HOLD OPEN ROD DON'T RETRACT . REMOVED AND REPLACED # 2 ENG O/B CORE COWL HOLD OPEN ROD. OPS CHECK NORMAL IAW B767-300 AMM 71-11-11.SDR UIEA2022061300590O-Ring · leakingFOUND PNEUMATIC LEAK AT PRVC SENSE LINE LOCATION "E" AS PER EO #1936A088. REMOVED AND REPLACED O' RING AT LOCATION "E". RECHECKED PER EO# 1936A088. NO LEAKS NOTED.SDR UIEA2022061300591O-Ring · leakingFOUND PNEUMATIC LEAK AT PRVC AT PRVC ACTUATOR PRESSURE TUBE LOCATION "K" AS PER EO# 1936A088. REMOVED & REPLACED O' RING AT LOCATION "K". RECHECKED PER EO #1936A088. NO LEAK NOTED.SDR UIEA2022061300592Cover · brokenLEFT AFT OVER WING EMERGENCY EXIT DOOR COVER ASSEMBLY IS BROKEN. REMOVED AND REPLACED LH AFT EMERGENCY HATCH COVER PER 767 MM 52-21-02-402-001. OPS CHECK GOOD</P>)SDR UIEA2022061300593Seal · missingBOTH RIGHT & FWD LEF OVER WING EMERGENCY EXIT DOOR CUT OUT SILLS MISSING CORNER SEALS . (INSTALLED CORNER SEALS IN BOTH LEFT & RIGHT OVERWING EMERGENCY EXIT DOORS PER B767-300 AMM 20-30-01SDR UIEA2022061300594Sealant · deterioratedALL FOUR ( 4 ) OVER WING EMERGENCY EXIT DOOR CUTOUT SEAL DEPRESSOR SURFACES HAVE CRACK .(<P>NO SEAL DEPRESSOR DAMAGED. FOUND SEALANT DETERIORATED. CLEANED AREA AND RESEALED ALL 4 OVER WING EMERGENCY EXIT DOOR CUTOUTS PER B767-300 AMM 20-30-01-992-001.<SDR UIEA2022061300595Connector · leakingENG # 2 EVIDENCE OF HYD LEAK IN PYLON CONNECTION. CLEANED AREA AS REQUIRED IAW B767-300 AMM 12-25-01. TIGHTENED #2 ENGINE PRESS LINE HYDRAULIC DRIVEN PUMP IAW B767-300 29-11-05. PENDING LEAK CHECK. PERFORMED LEAK CHECK PER B767-300 AMM 71-00-00 & 29-11-00. SDR UIEA2022061300596Hydraulic Line · contaminatedENG # 1 EVIDENCE OF HYDRAULIC LEAK O/B SIDE OF ENGINE CONTAMINATED WITH DRIED UP HYDRAULIC FLUID. CLEANED #1 ENG HYDRAULIC LEAK PER B767-300 AMM 12-25-01. PENDING LEAK CHECK. PERFORMED LEAK CHECK PER B767-300 AMM 71-00-00 FOR ENG #1 HYD SYSTEM AND AMM 24-SDR UIEA2022061300597Inertia Reel · unserviceableCOCKPIT F/O LH SEAT BELT TSO TAG ILLEGIBLE . REMOVED & REPLACED FO INERTIA REEL PER B767-300 AMM 25-11-04. OPS CHECK GOOD.SDR UIEA2022061300598Slide Raft · out of positionRH O/WING OVHD BIN RAFT NOT SECURED WITH STRAPS RW 23. RESECURED RH OVERHEAD RAFT PER B767-300 AMM 25-62-00SDR UIEA2022061300599Pressure Sensor · inoperativeCENTER HYDRAULIC PRESSURE INDICATOR INOP. REMOVED AND REPLACED CENTER HYDRAULIC PRESSURE TRANSMITTER IAW AMM 29-31-01. OPS CHECK PASSED, SYSTEM OK AT THIS TIME.SDR UIEA2022051500480Switch · failedBARBER POLE WOULD NOT ADVANCE AFTER PASSING 10,000FT. INVESTIGATED AND FOUND VMO SWITCH TO BE IN THE ALT POSITION. SWITCHED VMO LIMITING SWITCH TO NORM POSITION IAW AMM 22-00-02</P>)SDR UIEA2022022600170Failsafe · crackedFUSELAGE SECTION 45 STA 955 REAR SPAR BULKHEAD SIDE FITTINGS FAIL SAFE STRAP RH SIDE WITH CRACK INDICATION.(<P>FAIL SAFE STRAP WAS REPAIRED</P>)SDR UIEA2022022600171Bracket · brokenENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 9 HOURS(<P>THE CLAMP SUPPORT ROOD OF THE ACCESS 447BR PANEL WAS REPLACED</P>)SDR UIEA2022022600172Bracket · brokenENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 2 HOURS(<P>MANIFOLD REPLACED</P>)SDR UIEA2022022600173Clamp · brokenRH. HYDRAULIC BAY, CLAMP TO STORE SUPPORT ROD OF THE ACCESS PANEL447BR IS BROKE.(<P>THE CLAMP OF THE SUPPORT OF ACCESS PANEL 447BR WAS REPLACED</P>)SDR UIEA2022022600174Control Manifold · looseENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH WEAR AND LOOSE BETWEEN 11 HOURS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)SDR UIEA2022022600175Angle · crackedCABIN FLOOR STRUCTURE SEC 46 BETWEEN STA 1562 / 1582 - TWO LOCATIONS (LBL 88.5 AND RBL 88.5) UNION ANGLES WITH CRACK(<P>CABIN FLOOR STRUCTURE WAS REPLACED</P>)SDR UIEA2022022600176Bracket · brokenENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 3 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)SDR UIEA2022022600177Bracket · brokenENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 11 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)SDR UIEA2022022600178Bracket · brokenENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 7.30 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)SDR UIEA2022022600179Bracket · brokenENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 11 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)SDR UIEA2022022600180Fuel Tank · leakingCENTER WING, AUXILIARY FUEL TANK RBBL 97.95 AND STGR L-6 WITH FUEL LEAK(<P>FUEL LEAKS WERE REPAIRED</P>)SDR UIEA2022022600181Fuel Tank · leakingCENTER WING, AUXILIARY FUEL TANK, RBBL 97.95 AND STGR L-10 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED </P>)SDR UIEA2022021400106None · nonePASSENGER MASKS OBSERVED DEPLOYED ROW 8 SEATS H K(<P>INSPECTED AND CHECKED AND STOWED PASSENGER OXYGEN MASKS AT SEATS 8 H K AS PER AMM 35-21-05 AND OK FOR SERVICE.</P>)SDR UIEA2022020400093Oven · fireSMOKE AND SMALL FIRE IN OVEN #7 TRAYS APPEAR TO BE THE WRONG SIZE(<P><SPAN>FOUND OBSTRUCTION BEHIND #7 OVEN TRAYS. CLEANED OBSTRUCTION AND PERFORMED OPS CK PER CMM 25-36-34. OPS CK GOOD. C/W SMOKE IN CABIN INSPECTION REF AMM 05-51-56. NO DEFECTS NOTED.</SPAN><SDR UIEA2022011900065Unknown · odorSTRONG "DIRTY SOCK" ODOR COMING FROM PACKS ON DESCENT BELOW 10,000 FT.(<P>UPON ARRIVAL AND DURING OPS OF PAX ON GROUND, DETECTED NO SMELL OR ODOR. GVI OF PAX PER AMM 21-23-00. FOUND NO DEFECTS AT THIS TIME. OK TO CONTINUE.</P>)SDR UIEA2022011200012Elt · noneFIXED ELT INOP(<P>TRANSFERRED TO MDDR 159654 UNDER MEL 25-63-10-02A CAT2 EXP 10 APR 22.</P> / <P>LOG PAGE 1377618: R/R FIXED ELT IAW AMM SUPPLEMENT DC 356-0220-00. OPS CHECK GOOD. NO DEFECTS NOTED. DMI NO. 159654 CLEARED.</P> / <P> </P> / <P> </P>)SDR UIEA2022011300014Bulb · noneCEILING EMERGENCY LIGHT AT SEAT 40H INOP.(<P><SPAN>RELAMPED IAW AMM 33-51-04 OPS CHECK GOOD.</SPAN></P>)SDR UIEA2021112302433Shear Tie · noneSHEAR TIE COMMON TO FRAME WEB AT BS 1329 STR 38L, INBD AND OTBD SHEAR TIES HAVE CORROSION.(<P>REMOVED AND REPLACED 2EA SHEAR TIES AT AFT CARGO PIT BS 1329, INBD AND OTBD OF STR 38L PER SRM 51-40-02-0G-0 PGS 2-3</P>)SDR UIEA2021111002391None · noneDENT ON EXTERNAL UPPER SURFACE OF HORIZONTAL STAB CENTER SECTION BETWEEN RIB 1R AND 2R AT STA 1767(<P>REMOVED DAMAGE, INSTALLED REPAIR DOUBLER AND TRIPLER IAW BOEING MSG# EAC-TLS-21-0003, REFERENCE FAA FORM 8100-9, DATED OCT. 10, 2021.</P>)SDR UIEA2021112902436None · noneSTRINGER 38L CORRODED IN MULTIPLE SPOTS FROM BS 1219 TO 1351 AFT CARGO COMPARTMENT.(<P>REMOVED CORROSION FROM S38L, BS 1219 TO 1307 WITHIN LIMITS, BS 1329 TO 1351 OUT OF LIMITS PER B767-300 SRM 53-00-03-1A-1, FIG. 101. FABRICATED AND REPLACED STRINGER SECTION SDR UIEA2021112902437None · noneBS 1329 FRAME AND WEB CUT BETWEEN S37L TO S39L FOR ACCESS TO S38L REPAIR ON PWO# HM499-20446.(<P>REPAIRED FRAME WEB AND FAIL-SAFE CHORD BS 1329 BETWEEN S37L TO S39L PER BOEING REPAIR SKETCH EAC-TLS-21-0002 AND FAA FORM 8100-9 DATED 18 NOV 2021. </P>)SDR UIEA2021112902438None · noneS38L AND REPAIR SPLICES REQUIRED FOR REPAIR BETWEEN BS 1307 AND 1340 DUE TO CORROSION. REFERENCE ALSO PWO# HM499-20243, RAM N664GT-21-(<P>FABRICATED AND INSTALLED STRINGER SECTION AND REPAIR SPLICES AT S38L, BS 1307 TO 1340 PER B767-300 SRM 53-00-03-2R-2.</P>)SDR UIEA2021112902439None · noneLH WING RIB 32 (WS 1018.2) DISCREPANT HOLES COMMON TO S10L, S9L AND S7L.(<P>REAMED DAMAGED FASTENER HOLES COMMON TO S10L, S9L AND S7L AND INSTALLED FREEZE PLUGS AND FASTENERS MESSAGE EAC-TLS-21-0005 AND FAA FORM 8100-9 DATED 21 NOV 2021.</P>)SDR UIEA2021112902440None · noneLH WING #5 INBD. SLAT CRACKED AT THE INBD. EDGE DUE TO CONTACT WITH #1 ENG. OBTD. THRUST REVERSER(<P>REPAIRED LH WING #5 INBD. SLAT INBD. EDGE PER BOEING MSG# EAC-TLS-21-0004 APPROVAL SOURCE FAA FORM 8100-9 DATED 20 OCT 2021 AND DWG 114T4105</P>)SDR UIEA2021111002387None · noneDURING CLIMB WXR FAIL ON EHSI. WEATHER RADAR INOP(<P><SPAN>PERFORMED FIM TASK 34-43 FAULT TREE 805. NO FAULTS FOUND.</SPAN></P>)SDR UIEA2021110202326None · noneAPU GENERATOR INOP ( APU GENERATOR, EXCEPT ER OPERATIONS (NOTIFY DISPATCH) )(<P>TRANFER TO MDDR 156038 DDG 24-00-02A CAT C DUE DATE 11NOV21.DISP EH@1236.</P> / <P>03NOV21 - 1238759 - ITEM# 12 - CVG - REMOVED AND REPLACE BPCU IAW AMM 21-41-03 AND RELAY K103 (SSDR UIEA2021102702291Unknown · odorSTRONG ODOR FROM BOTH PACKS, SIMILAR TO WET PAINT OR WET SOCKS. MOST NOTICEABLE WITH THRUST SETTING CHANGES.(<P>PERFORMED DVI OF PACKS FOR CONTAMINATION, NO CONTAMINANTS FOUND AT THIS TIME. PERFORMED OPERATIONAL CHECK OF PACK, COULD NOT DUPLICATE SMELL. REF AMSDR UIEA2021102502281None · noneAPU INOP ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60 )(<P>TRANSFERRED TO MDDR 155562 IAW MEL 49-11-01A, CAT C.</P> / <P>LP <SPAN>1429464 - </SPAN><SPAN>PERFORMED MCD TEST IAW 52-32-00 STEP 3H3, PERFORMED TEST ON APU AND GROUNDSDR UIEA2021101202218Valve · noneRT PACK TEMP EICAS(<P>PLACED ON MEL 21-51-03 MDDR 155001 CAT - C DUE DATE 22 OCT 21 MCC DW 0849Z.</P> / <P>12OCT-CVG MX: LP 1407496, ITEM M3: REMOVED AND REPLACED RH PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CK GOOD, MDDR 155001 CLEARED. MCC NOTIFIEDSDR UIEA2021092702134Switch · inoperativeCAPT WX SELECT LIGHT INOP(<P>DEFERRED TO DMI # 154044, MEL 34-43-01-05, DUE 22 JAN 22, "CAT D" NO MX ACTION.</P> / <P>07OCT21 - 1361984 - ITEM# 4 - ONT - VERIFIED WXR PUSH BUTTON FUNCTIONS AS REQUIRED PER B767 AMM 34-43-00. LIGHTED "ON" PUSHBUTTON PN # 433-673
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