# Service difficulty reports: N1511A A list on [N1511A](https://openairdocs.org/aircraft/N1511A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 7 · 334 reports - [SDR UIEA2026102701000](https://openairdocs.org/sdr/UIEA2026102701000.md): Elt · unsecure · Oct 27, 2026 · N1511A · Boeing 767383 · Emergency Locator Beacon > PAPER STRAPS HOLDING THE ANTENNA OF THE PORTABLE ELT ON THE WALL NEXT TO THE DOOR IS BROKEN. REPLACED PORTABLE ELT IAW AMM 25-63-03 AND IPC 25-64-54. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2026061100458](https://openairdocs.org/sdr/UIEA2026061100458.md): Tamper Strip · torn · Jun 8, 2026 · N1511A · Boeing 767383 · Emergency Locator Beacon > ELT NEXT TO L1 DOOR HAS TAMPER TAPE TORN. R & R PORTABLE ELT BY L1 DOOR IAW AMM 25-63-03 & AIPC 25-64-54-01B. OPS CHKD OK. - [SDR UIEA2026042200238](https://openairdocs.org/sdr/UIEA2026042200238.md): Outflow Valve · faulted · Apr 22, 2026 · N1511A · Boeing 767383 · Pressure Regulator/Outflow Valve > CABIN ALTITUDE EICAS MSG WARNING. PERFORMED EMERGENCY DESCENT TO 10,000 FT @ FL330, DIFF PSI 60-7.0, CABIN ALT 10000-11000 FT. NOTED OUTFLOW VALVE WAS APPROX HALF OPEN, NO CHANGE W/ AUTO 2 OR AUTO 1, WAS A SLOW RATE DECOMPRESSION.(

PERFORMED BITE TEST OF CAB - [SDR UIEA2026032300105](https://openairdocs.org/sdr/UIEA2026032300105.md): Escape Reel · inoperative · Mar 23, 2026 · N1511A · Boeing 767383 · Emergency Equipment > 1 EACH ESCAPE HARNESS INOPERATIVE ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} ESCAPE HARNESSES) NR 2 ESCAPE HARNESS IS TRANSFER TO DMI 249625 PER MEL 25-61-01-02 CAT C DUE DATE 31MAR26. PLACARDS INSTALLED. MX ACTIONS C/W. INSTALLED - [SDR UIEA2025122701361](https://openairdocs.org/sdr/UIEA2025122701361.md): Not Reported · not reported · Dec 26, 2025 · N1511A · Boeing 767383 · Standard Practices/Structures > REJECTED TAKEOFF DUE TO NON-MECHANICAL CONDITION. SPEED WAS APPROXIMIATELY 30 KNOTS.AND BRAKE TEMPS NORMAL.. PERFORMED HIGH STOP INSPECTION IAW AMM 05-51-14, NO DISCREPANCIES NOTED AT THIS TIME. - [SDR UIEA2025121401344](https://openairdocs.org/sdr/UIEA2025121401344.md): Controller · faulted · Dec 14, 2025 · N1511A · Boeing 767383 · Cabin Pressure Controller > AT TOP OF DESCENT, CREW ALTITUDE EICAS MSG. CABIN ALT WENT TO 11,000 FT AFTER DESCENT TO 8000 FT, CABIN PRESS DIFF WAS 0.(

FOLLOWED FIM FOR CABIN ALTITUDE BITE CHECK PER FIM 21-31-00. FOUND CABIN ALT CONTROLLER 2 FAULT LOW FLOW. THEN FOLLOWED AMM 36-23-00 AI - [SDR UIEA2025102501279](https://openairdocs.org/sdr/UIEA2025102501279.md): Bottle · no test · Oct 25, 2025 · N1511A · Boeing 767383 · Fire Bottle, Fixed > #2 FIRE CARGO BOTTLE WON'T TEST(

PERFORMED ALL WIRING CHECKS FROM THE SQUIB TEST PANEL TO EACH SQUIB FOR BOTTLES 1, 2, & 2A PER WDM 26-23-12, FOUND PIN 14 ON D866 AND PIN 14 ON D864 HAD NO GROUND FOR TEST CIRCUIT. FOUND APU/CGO FIRE CONTROL PANEL REPLACED. L - [SDR UIEA2025093001247](https://openairdocs.org/sdr/UIEA2025093001247.md): Door Frame · cracked · Sep 30, 2025 · N1511A · Boeing 767383 · Fuselage Main, Structure > CRACK (1 EA) IS DETECTED AT L1 FWD ENTRY DOOR AFT LWR CORNER DURING OPEN HOLE HFEC INSPECTION IAW EO 6753A937(

REPAIRED WITH 2 EA OF FILLER AND 3 EA OF DOUBLER AS PER SRM 53-10-01-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025093001248](https://openairdocs.org/sdr/UIEA2025093001248.md): Fitting · cracked · Sep 30, 2025 · N1511A · Boeing 767383 · Fuselage Main, Structure > FUSELAGE SECTION 48 BODY STATION 1809.5 BULK HEAD LH TENSTION FITTING CRACK(

REAMED FASTENER HOLE TO A DIAMETER OF 0.3120" AS PER SRM 51-40-05 & SP1-TLS-25-0031-038. PERFORMED OPEN HOLE HFEC INSPECTION PER NDTM 51-00-16 PART 6, RESULT NORMAL. R/R FASTENER PE - [SDR UIEA2025093001249](https://openairdocs.org/sdr/UIEA2025093001249.md): Skin · damaged · Sep 30, 2025 · N1511A · Boeing 767383 · Leading Edge Devices > REQUIRED TO PERFORM SURFACE HFEC INSPECTION AT REPAIRED AREA (REF EO 6755A032)(

ACCOMPLISHED SURFACE HFEC INSPECTION AT RH HORIZONTAL STAB. REPAIRED AREA PER NDTM 51-00-19 PART 6, RESULT NORMAL. INSPECTED THE BLIND RIVETS LOCATED AT THE HORIZONTAL STAB RH UP - [SDR UIEA2025093001250](https://openairdocs.org/sdr/UIEA2025093001250.md): Door · cracked · Sep 30, 2025 · N1511A · Boeing 767383 · Service Doors > CRACKS (2 EA) ARE DETECTED AT R1 FWD ENTRY DOOR AFT LWR CORNER DURING OPEN HOLE HFEC INSPECTION IAW EO 6753A937(

REPAIRED WITH 2 EA OF REPAIR FILLER & 3 EA OF DOUBLER AS PER SRM 53-10-01-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025071600960](https://openairdocs.org/sdr/UIEA2025071600960.md): Oxygen Mask · no test · Jul 11, 2025 · N1511A · Boeing 767383 · Passenger Oxygen System > RH PAX OXYGEN MASK WILL NOT TEST. R/R RH PAX O2 MASK IAW AMM 35-11-51. OPS CHK GOOD AT THIS TIME. NO LEAKS NOTED AT THIS TIME. - [SDR UIEA2025071600961](https://openairdocs.org/sdr/UIEA2025071600961.md): Oxygen System · no discrepancy · Jul 11, 2025 · N1511A · Boeing 767383 · Passenger Oxygen System > PAX OXYGEN SYSTEM SUSPECT LEAK. SERVICED PAX O2 TO 1760 PSI PER AMM 12-15-08 & GMM 3.25.2 & 3.25.3. AFTER SITTING FOR 3 DAYS, NO LEAKS DETECTED. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025071600962](https://openairdocs.org/sdr/UIEA2025071600962.md): Seal · broken · Jul 11, 2025 · N1511A · Boeing 767383 · Emergency Locator Beacon > PORTABLE ELT SEAL BROKEN. INSPECTED TAMPER TAPE ON PORTABLE ELT IAW AMM 25-05-03. FOUND SMALL WEAR MARK BUT SEAL IS INTACT AND NOT BROKEN. NO FURTHER DEFECTS NOTED AT THIS TIME. - [SDR UIEA2025052800701](https://openairdocs.org/sdr/UIEA2025052800701.md): Seal · missing · May 27, 2025 · N1511A · Boeing 767383 · Emergency Equipment > F/O EVAS MISSING SEAL. R & R THE TAMPER SEAL IAW AMM 25-60-99. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025040900449](https://openairdocs.org/sdr/UIEA2025040900449.md): Bottle · low pressure · Apr 9, 2025 · N1511A · Boeing 767383 · Passenger Oxygen System > SUPERNUMERARY PAX O2 LOW.(

R/R PAX O2 CYLINDER IAW AMM 12-15-08. LEAK CHECK GOOD.

) - [SDR UIEA2024111501090](https://openairdocs.org/sdr/UIEA2024111501090.md): Pump · faulted · Nov 15, 2024 · N1511A · Boeing 767383 · Fuel Boost Pump > CTR L FUEL PUMP EICAS MSG IN CRUISE WITH 22000 LBS OF FUEL IN THE CTR TANK, FOUND C/B POPPED(

R/R LH FUEL CENTER OVERRIDE PUMP IAW AMM 28-22-05. OPS & LEAK CHK GOOD. DMI 220641 CLOSED

) - [SDR UIEA2024081900837](https://openairdocs.org/sdr/UIEA2024081900837.md): Escape Reel · unsecure · Aug 19, 2024 · N1511A · Boeing 767383 · Emergency Equipment > ESCAPE REELS ARE LOOSE(

RESECURED ESCAPE REELS IAW AMM 25-61-05/401. OPS CHECK GOOD

) - [SDR UIEA2024062000560](https://openairdocs.org/sdr/UIEA2024062000560.md): Elt · inoperative · Jun 19, 2024 · N1511A · Boeing 767383 · Emergency Locator Beacon > ENTRY WAY ELT AT L1 INOP ( EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS)(

TRANSFERRED TO DMI 211008 IAW MEL 25-63-10-01 CAT D DUE DATE 18OCT24. MCC NOTIFIED.REMOVED AND REPLACED PORTABLE ELT IAW AMM 25-63-03, THIS CLEARS DMI 211088, PLACARDS REMO - [SDR UIEA2024062000559](https://openairdocs.org/sdr/UIEA2024062000559.md): Elt · inoperative · Jun 18, 2024 · N1511A · Boeing 767383 · Emergency Locator Beacon > COCKPIT ELT INOP ( EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS)(

REMOVED AND REPLACED LAV PORTABLE ELT IAW AMM 25-63-03. OPS CHECKS GOOD. THIS CLEARS MDDR 211017. MCC NOTIFIED. PLACARDS REMOVED.

) - [SDR UIEA2024051800392](https://openairdocs.org/sdr/UIEA2024051800392.md): Hook And Loop · worn · May 17, 2024 · N1511A · Boeing 767383 · Fuselage Miscellaneous Structure > FO'S EVAS HOOK AND LOOP STRIP ON GLARESHIELD IS WORN OUT(

RE-SECURED FO'S EVAS GLARESHIELD VELCRO IAW B767 AMM 25-60-99. NO OTHER DEFECTS NOTED. - [SDR UIEA2024041900297](https://openairdocs.org/sdr/UIEA2024041900297.md): Doubler · damaged · Apr 27, 2024 · N1511A · Boeing 767383 · Fuselage Main, Structure > ONE CRACK INDICATION FOUND ON NOSE WHEEL WELL IN SRM 3 PLATE RADIUS ON RBL 25 VERTICAL CHORD AT WL 173 0.400 LONG(

DAMAGED DOUBLER WAS REPLACED PER EO6753A027. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400307](https://openairdocs.org/sdr/UIEA2024042400307.md): Skin · dented · Apr 27, 2024 · N1511A · Boeing 767383 · Trailing Edge Flaps > RH WING OUTBOARD FLAP INNER SURFACE FWD SECOND BAY STA 622 APPROX WITH TWO DENTS(

DENTS (2 EA) ON RH WING OUTBOARD FLAP INNER SKIN PANEL WERE REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400308](https://openairdocs.org/sdr/UIEA2024042400308.md): Skin · dented · Apr 27, 2024 · N1511A · Boeing 767383 · Trailing Edge Flaps > RH WING OUTBOARD FLAP INNER SURFACE FWD SECOND BAY STA 636 WITH DENT(

DENT ON RH WING OUTBOARD FLAP INNER SKIN LOWER PANEL AT OTEF 101.73 WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400309](https://openairdocs.org/sdr/UIEA2024042400309.md): Skin · debonded · Apr 27, 2024 · N1511A · Boeing 767383 · Horizontal Stabilizer, Plate/Skin > LH HORIZONTAL STAB FIXED LE, DISBONDED PREVIOUS REPAIR ON LOWER SKIN AT L.STA 366.377(

DISBOND ON LH HORIZONTAL STABILIZER LOWER SKIN WAS REPAIRED PER SRM 51-70-10-2R-0. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400310](https://openairdocs.org/sdr/UIEA2024042400310.md): Skin · delaminated · Apr 27, 2024 · N1511A · Boeing 767383 · Leading Edge Devices > LH WING, SLAT #4 SURFACE INNERSIDE AREA UPPER INSIDE CORNER WITH DELAMINATION.(

DELAMINATIONS (2 EA) ON LH WING SLAT #4 T/E WEDGE WERE REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400311](https://openairdocs.org/sdr/UIEA2024042400311.md): Skin · delaminated · Apr 27, 2024 · N1511A · Boeing 767383 · Leading Edge Devices > DELAMINATED UPPER CORNER OF SLAT 9 AT RH WING(

DELAMINATION ON RH WING SLAT# 9 T/E WEDGE UPPER SKIN INBD CORNER WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400312](https://openairdocs.org/sdr/UIEA2024042400312.md): Skin · delaminated · Apr 27, 2024 · N1511A · Boeing 767383 · Leading Edge Devices > DELAMINATED UPPER CORNER (UPPER SURFACE) OF SLAT 12 AT RH WING(

DELAMINATION ON RH WING SLAT #12 T/E WEDGE UPPER SURFACE WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042400315](https://openairdocs.org/sdr/UIEA2024042400315.md): Skin · delaminated · Apr 27, 2024 · N1511A · Boeing 767383 · Trailing Edge Flaps > LH WING, INBOARD FLAP SURFACE INNER SIDE AREA AFT FLAP OUTSIDE CORNER WITH DELAMINATION(

DELAMINATION ON LH WING INBOARD AFT FLAP LOWER SURFACE WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024042500316](https://openairdocs.org/sdr/UIEA2024042500316.md): Skin · corroded · Apr 27, 2024 · N1511A · Boeing 767383 · Wing, Plate/Skin > RH WING, TOP SURFACE,BTW WB 289.45 AND WBL 97.9566, DURING REMOVAL OF ACCESS SPOILER HINGE PANEL, CORROSION WAS FOUND ON THE SPOILER BEAM(

CORROSION RH WING TRAILING EDGE STRUCTURE INBOARD SPOILER SUPPORT BEAM UPPER CHORDS WERE REPAIRED PER SRM 57-51-02-2R-2 - [SDR UIEA2024042600317](https://openairdocs.org/sdr/UIEA2024042600317.md): Beam · corroded · Apr 27, 2024 · N1511A · Boeing 767383 · Wing Main, Frame Structure > CORROSION ON RH WING TRAILING EDGE STRUCTURE SPOILER BEAM UPPER CHORDS BETWEEN WBL 154.54 / 294.02(

CORROSION DAMAGES ON RH WING TRAILING EDGE STRUCTURE SPOILER BEAM UPPER CHORDS WERE BLEND OUT, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS PER SRM 57-51-02-1A - [SDR UIEA2023112080961](https://openairdocs.org/sdr/UIEA2023112080961.md): Blade · damaged · Nov 19, 2023 · N1511A · Boeing 767383 · Engine Air Intake System > BIRDSTRIKE ON RH ENG. FOUND FANBLADES #32 & 34 DAMAGED(

R/R FAN BLADES #32, 34, 13 AND 15 IAW AMM 72-31-02. C/W ENG TEST #8. ALL VIBE INDICATIONS WITHIN LIMITS.

) - [SDR UIEA2023091500834](https://openairdocs.org/sdr/UIEA2023091500834.md): Battery Pack · unknown · Sep 14, 2023 · N1511A · Boeing 767383 · Emergency Lighting > AISLE EMERGENCY LIGHING INOP. R/R EMERGENCY BATTERY PACK IAW AMM 33-51-07. OPS CHECKS GOOD. DMI 193326 CLOSED

) - [SDR UIEA2023060300555](https://openairdocs.org/sdr/UIEA2023060300555.md): Escape Reel · unknown · Jun 3, 2023 · N1511A · Boeing 767383 · Emergency Equipment > 1 EA INTERTIA REEL INOP. SUPPORT BRACKET BROKEN. INERTIAL REEL REMOVED FROM ACFT(

TRANSFERRED TO DMI 186721 IAW MEL 25-61-01-01 CAT C DUE DATE 13JUN23. MX ACTIONS C/W. INERTIAL REEL REMOVED FROM ACFT. 6 INERTIAL REELS REMAIN SERVICEABLE. INSTALLED DESCENT - [SDR UIEA2022122801220](https://openairdocs.org/sdr/UIEA2022122801220.md): Lamp · inoperative · Dec 26, 2022 · N1511A · Boeing 767383 · Emergency Lighting > EMERGENCY LIGHT ON RIGHT SIDE CEILING INOP. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00. - [SDR UIEA2022121101211](https://openairdocs.org/sdr/UIEA2022121101211.md): Skin · dented · Dec 12, 2022 · N1511A · Boeing 767383 · Leading Edge Devices > #10 SLAT HAS SEVERAL DEEP DENTS ON TOP OF THE SLAT.(

REPAIRED #10 SLAT IAW SRM 51-70-10-2R-2 REPAIR 2

) - [SDR UIEA2022090600939](https://openairdocs.org/sdr/UIEA2022090600939.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Tire Tube > LH WING, ON L9 AND RIB 1 WITH LEAK OF FUEL(

FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 136

) - [SDR UIEA2022090900943](https://openairdocs.org/sdr/UIEA2022090900943.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Engine Bleed Air System > ENGINE LH PERFORM TSM, PRV ( NOT CLOSED)(

ENGINE LH, TSM WAS PERFORMED. PRV, PRVC AND HPC WERE REPLACED AND TESTED OK IAW AMM 36-00-32-405-001 REV 136

) - [SDR UIEA2022090900944](https://openairdocs.org/sdr/UIEA2022090900944.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Hydraulic Power System > EVIDENCE OF HYDRAULIC LEAK, INBOARD PCA LEFT ELEVATOR(

ELEVATOR ACT ASSY POWER WAS REPLACED & OPS CHECK GOOD IAW AMM 27-31-05-424-027 REV 136

) - [SDR UIEA2022090900945](https://openairdocs.org/sdr/UIEA2022090900945.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Wing Structure > RH WING CENTER SECTION, LOWER SURFACE, SPLICE STRINGER L-6 AND BBL97.42 WITH LEAK FUEL(

FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013 PARAGRAPH 2

) - [SDR UIEA2022090900946](https://openairdocs.org/sdr/UIEA2022090900946.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Wing, Plate/Skin > RH WING LOWER SURFACE, AT L-10 BETWEEN WS 197 AND WS 228 WITH FUEL LEAK(

FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013 PARAGRAPH 2

) - [SDR UIEA2022090900947](https://openairdocs.org/sdr/UIEA2022090900947.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Wing Structure > RH WING LOWER SURFACE, AT L-10 BETWEEN WS 284 AND WS 344 WITH FUEL LEAK(

FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013 PARAGRAPH 2

) - [SDR UIEA2022090900948](https://openairdocs.org/sdr/UIEA2022090900948.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Wing Structure > RH WING LOWER SURFACE, AT L-10 AND WS 486 WITH FUEL LEAK(

FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013

) - [SDR UIEA2022090900949](https://openairdocs.org/sdr/UIEA2022090900949.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Long-Range Navigation (LORAN) System > LOG BOOK PAGE 1524770: ATC FAULT WITH LH XPONDER SELECTED(

FIM TASK 34-53 FAULT TREE 805 WAS PERFORMED. TEST WAS SATISFACTORY

) - [SDR UIEA2022090900950](https://openairdocs.org/sdr/UIEA2022090900950.md): Rod End Bearing · none · Sep 9, 2022 · N1511A · Boeing 767383 · Flight Control System > LH ELEVATOR, INBOARD POWER CONTROL ACTUATOR, INPUT ROD END BEARING DAMAGED(

INBOARD POWER CONTROL ACTUATOR INPUT ROD END BEARING WAS REPLACED AMM 27-31-07-424-016 REV 136

) - [SDR UIEA2022090900951](https://openairdocs.org/sdr/UIEA2022090900951.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Elevator Tab Control System > RIGHT ELEVATOR ACTUATOR INPUT ROD, RIGHT CENTER OUT OF LIMITS (COLLAPSING DIRECTIONS 65.5LBS/0.845")(

RIGHT ELEVATOR ACTUATOR INPUT ROD WAS REPLACED 27-31-07-424-016 REV136. OPS CHECK GOOD

) - [SDR UIEA2022090900952](https://openairdocs.org/sdr/UIEA2022090900952.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Aircraft Fuel System > RH FUEL LEAK BETWEEN WSTA 197.4/226.3 AT STGR L-15(

FUEL LEAK WAS REPAIRED AMM 28-11-00-308-013 REV 136.

) - [SDR UIEA2022090900953](https://openairdocs.org/sdr/UIEA2022090900953.md): None · none · Sep 9, 2022 · N1511A · Boeing 767383 · Aircraft Fuel System > RH FUEL LEAK BETWEEN WSTA 375.8/404.4 AT STGR L-6(

FUEL LEAK WAS REPAIRED AMM 28-11-00-308-013 REV 136

) - [SDR UIEA2022062800674](https://openairdocs.org/sdr/UIEA2022062800674.md): Truck · smoke · Jun 24, 2022 · N1511A · Boeing 767383 · Brake > AFTER 400 YARDS OF TAXI ANOTHER AIRCRAFT REPORTED SMOKE COMING FROM BOTH LANDING GEAR TRUCKS. ARFF REPORTED NO HEAT READING. RTB(

PERFORMED GVI OF LT/RT MAIN LANDING GEAR ALONG WITH WHEELS AND BRAKES NO DEFECTS FOUND. PERFORMED ANTI SKID BITE TEST IAW B767 A - [SDR UIEA2022012700078](https://openairdocs.org/sdr/UIEA2022012700078.md): None · none · Jan 27, 2022 · N1511A · Boeing 767383 · Oxygen System > CAPTS O2 MASK NOT WORKING PROPERLY.(

SWAPPED CAPTAINS O2 MASK WITH # 1 SUPERNUMARY O2 MASK IAW AMM 35-11-51. CAPT MASK OPS GOOD. # 1 SUPERNUMARY O2 MASK TRANSFERRED TO MDDR 160411 IAW MEL 36-11-03-02A, CAT C, DUE DATE 06FEB22.

/

CVG MX- 29JAN. LP 15 Next page: https://openairdocs.org/aircraft/N1511A/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 n_number = 'N1511A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N1511A/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.