# Service difficulty reports: N768AX

A list on [N768AX](https://openairdocs.org/aircraft/N768AX.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 2 · 89 reports

- [SDR ABXA20231126216](https://openairdocs.org/sdr/ABXA20231126216.md): Unknown · unknown · Nov 26, 2023 · N768AX · Boeing 767281 · Leading Edge Slat Control System
  > WHILE CONFIGURING FOR LANDING. WE GOT A L/E SLAT ASMY & DISCRETE LIGHT OCCURRED DURING APPROACH FLAPS @ 25 DEGS. MISSED APPROACH WAS ACCOMPLISHED & EMERGENCY WAS DECLARED. AFTER LANDING A/C GROUNDED BY MAINTENANCE. T/S PER FIM 27-58 FT 803. NO FAULTS NO
- [SDR ABXA20231013198](https://openairdocs.org/sdr/ABXA20231013198.md): Fuse · unserviceable · Oct 13, 2023 · N768AX · Boeing 767281 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, UPON RETRACTING THE LANDING GEAR A GEAR DISAGREE FLT ABX3102.DIVERTED BACK TO PHX. AC GROUNDED DEFERRED THE LANDING GEAR ACTUATING SYSTEM IAW MEL 32-30-1. MAINTENANCE PROCEDURES C/W. PLACARDS INSTALLED. MBCB 10/23/2023.A/C REPO.FLIGHT TO ILN,
- [SDR ABXA20230711144](https://openairdocs.org/sdr/ABXA20230711144.md): Selector Valve · faulted · Jul 9, 2023 · N768AX · Boeing 767281 · Hydraulic System, Main
  > RESERVE BRK VALVE EICAS DURING TAXI OUT, VALVE LT ON SWITCH ON AND ISO VLV LT ON ACC PANEL ON, SW OFF. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED TEST TO ISOLATE C1 ACMPCENTER SYSTEM PER AMM 29-11-00, ISOLATED ACMP SUPPLY SHUTOFF
- [SDR ABXA20230703141](https://openairdocs.org/sdr/ABXA20230703141.md): Unknown · unknown · Jul 2, 2023 · N768AX · Boeing 767281 · Flight Control System
  > AILERON LOCKOUT EICAS/DISCRETE LIGHT ILLUMINATED DURING PUSHBACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RERACKED / RH STAB TRIM AILERON LOCKOUT MODULE. PREFORMED AILERON LOCKOUT TEST IAW B767 AMM 27-11-00. TEST GOOD.OPS CK GOOD AC
- [SDR ABXA20230522111](https://openairdocs.org/sdr/ABXA20230522111.md): Unknown · unknown · May 19, 2023 · N768AX · Boeing 767281 · Stabilizer Control System
  > STAB TRIM EICAS MESSAGE ON CLIMBOUT AT 7000 MSL STAB TRIM EICAS MESSAGE REMAINED ILLUMINATED WITH BOTH AUTOPILOT ENGAGED AND DISENGAGED AFTER LANDING WHEN RESET TO 2. STAB EICAS MESSAGE EXTINGUISHED. STAB TRIMMING WAS AT 1/2 RATE. CREW ELECTED TO RETURN TO DEP
- [SDR ABXA2023050473](https://openairdocs.org/sdr/ABXA2023050473.md): Unknown · unknown · Apr 28, 2023 · N768AX · Boeing 767281 · Trailing Flap Position Indicating System
  > TRAILING EDGE FLAP DISAGREEMENT EICAS MESSAGE DISPLAYED DURING FINAL SEGMENT OF THE APPROACH AND A MISS APPROACH WAS ACCOMPLISHED TO COMPLETE THE REQUIRED NON NORMAL CHECKLIST AND AN EMERGENCY WAS DECLARED DUE TO HIGHER THAN NORMAL LANDING SPEED AND STRONG GUS
- [SDR ABXA2023041859](https://openairdocs.org/sdr/ABXA2023041859.md): Unknown · unknown · Apr 17, 2023 · N768AX · Boeing 767281 · Doors
  > E/E ACCESS DOOR ON EICAS AND ACCESS DOOR LIGHT OVERHEAD. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE OPENED AND CLOSED E+E ACCESS DOOR FROM INSIDE AND OUTSIDE THE A/C IAW B767 AMM 52-71-00 AND VERIFIED EICAS MESSAGE AND OVERHEAD WARNING DIS
- [SDR ABXA2023041858](https://openairdocs.org/sdr/ABXA2023041858.md): Unknown · unknown · Apr 17, 2023 · N768AX · Boeing 767281 · Engine Starter
  > R ENG STARTER EICAS MSG ON GROUND DURING START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED RT. ENG. START VALVE IAW MEL 80-00-2-1. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA2023011207](https://openairdocs.org/sdr/ABXA2023011207.md): Cabin Air Sys · fault message · Jan 11, 2023 · N768AX · Boeing 767281 · Cabin Temperature Controller
  > FWD CABIN TEMP EICAS ADVISORY MSG. FWD CABIN TEMP INOP DISCRETE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT AND THEN DEFERRED PER MEL 21-61-1-2. MAINTENANCE PROCEDURES COMPLIED WITH. AIRCRAFT RETURNED TO SERVI
- [SDR ABXA2023011106](https://openairdocs.org/sdr/ABXA2023011106.md): Throttle · failed · Jan 6, 2023 · N768AX · Boeing 767281 · Auto Throttle System
  > THRUST MANAGEMENT FAILED, RESET AND FAILED ON THE PUSH. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED TMC IAW MEL 22-30-1A. PLACARD INSTALLED; MX PROCEDURES C/W. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA2022072286](https://openairdocs.org/sdr/ABXA2022072286.md): None · faulty · Jul 22, 2022 · N768AX · Boeing 767 · Pneumatic System
  > RH ENG BLEED VALVE ON TAKE OFF PWR. CREW ABORTED TAKE OFF AT 70 KTS AND RETURNED TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RH HIGH PRESSURE VALVE CONTROLLER IAW AMM 36-11-08. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA2023050475](https://openairdocs.org/sdr/ABXA2023050475.md): Frame · cracked · Jun 30, 2022 · N768AX · Boeing 767281 · Aerodynamic Fairings
  > DURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE WAS REQUIRED TO INSPECT THE RIGHT INNER FRAME CHORD, LOCATED AT BS 883.5, LBL 89 PER ABX JOB CARD ABX-NEA-5350-0015-001 (AD 2012-22-17, SB 767- 53A0209 AND AD 2018-11-08, SB 767-53A0278). DURING INSPECTI
- [SDR ABXA2023050476](https://openairdocs.org/sdr/ABXA2023050476.md): Keelbeam · cracked · Jun 22, 2022 · N768AX · Boeing 767281 · Aerodynamic Fairings
  > DURING AN AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED CORROSION AND A CRACK ON THE R/H SIDE KEEL BEAM CHORD, UPPER FLANGE AT STA 792. AFTER LOCAL FASTENERS IN THE CHORD UPPER FLANGE HAD BEEN REMOVED, A 4.75” CRACK WAS DISCOVERED. A SURFA
- [SDR ABXA2022032848](https://openairdocs.org/sdr/ABXA2022032848.md): None · none · Apr 28, 2022 · N768AX · Boeing 767281 · APU Cowling/Containment
  > APU PNEUMATICS INOP, AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENACE DEFERRED APU IAW MEL 49-11-1-1. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA2022041142](https://openairdocs.org/sdr/ABXA2022041142.md): None · none · Apr 11, 2022 · N768AX · Boeing 767 · Airborne Auxiliary Power Unit (APU) System
  > A/C BLOCKED OUT MX WAS TOLD CREW COULD NOT START LH ENGINE AC WAS RETURNING TO GATE MX ON BOARD TALKED TO CREW SAID NO APU PRESSURE. AIRCRAFT BLOCKED AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED APU AIR IAW MEL 49-11-1-1 MBCB 05/21/22, MX PROCEDURES C/W
- [SDR ABXA2022030130](https://openairdocs.org/sdr/ABXA2022030130.md): Actuator · failed · Mar 1, 2022 · N768AX · Boeing 767281 · Engine Fuel and Control
  > ON LEFT ENGINE START, ENGINE VALVE DID NOT EXTINGUISH, ABORTED START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE CONDITION MOTOR. IAW 76-11-01 OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA202201503](https://openairdocs.org/sdr/ABXA202201503.md): None · none · Jan 4, 2022 · N768AX · Boeing 767281 · Navigation System
  > DURING TAXI OUT SHORT OF MIKE TAXIWAY ON SIERRA. MANUALLY TUNED FLM VOR MANUALLY IN BOTH VOR'S. CONFIRMED WITH ATC THAT THE FLM VOR IS OPERATIONAL! OFF FLAGS REMAINED IN VIEW. RETURNED TO GATE. AND GROUNDED BY MAINTENANCE. CONDUCTED TEST OF L/H AND R/H VOR, N
- [SDR ABXA20211211129](https://openairdocs.org/sdr/ABXA20211211129.md): None · none · Dec 11, 2021 · N768AX · Boeing 767281 · Engine Controls
  > DURING RIGHT ENG START WHEN ADVANCING RT FUEL CONTROL, EICAS MESSAGE R ENG FUEL VALVE APPEARED AND DISAGREE ENGINE VALVE LIGHT ILLUMINATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND DAMAGED WIRING IN FORWARD CARGO COMPARTMENT. WIRI
- [SDR ABXA202109139090](https://openairdocs.org/sdr/ABXA202109139090.md): Cable · binding · Sep 9, 2021 · N768AX · Boeing 767281 · Engine Fuel Indicating System
  > ON TAXI OUT, R ENG STARTED SURGE +/- 2% N2, +/- 100 FF, +/- 40 EGT, +/- 1% N1. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND R/H ENG VSV FEEDBACK CABLE TO HAVE HIGH PULL FORCE.R&R RH ENG VSV FEEDBACK CABLE IAW AMM 75-31-03. AIRCRAFT RET
- [SDR ABXA2021830083](https://openairdocs.org/sdr/ABXA2021830083.md): Start Valve · binding · Aug 30, 2021 · N768AX · Boeing 767281 · Engine Start Valves/Controls
  > LH ENGINE START VALVE FAILED TO OPEN. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND L/H ENGINE START VALVE BINDING DURING MANUAL OPERATION. REMOVED OLD, THEN INSTALLED NEW L/H START CONTROL VALVE PER AMM 80-11-02. AICRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021829080](https://openairdocs.org/sdr/ABXA2021829080.md): Starter · faulted · Aug 29, 2021 · N768AX · Boeing 767281 · Engine Starter
  > LEFT ENGINE FAILED TO START, N2 NEVER GOT ABOVE 8.7 DUCT PRESSURE WAS NORMAL. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE #1 ENGINE STARTER IAW B767 AMM 80-11-0. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA20210715066](https://openairdocs.org/sdr/ABXA20210715066.md): Pneumatic System · faulted · Jul 15, 2021 · N768AX · Boeing 767281 · APU Bleed Air System
  > APU PNEUMATIC PRESSURE WENT TO ZERO AFTER PUSHBACK AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE, CYCLED APU. REGAINED DUCT PRESSURE AFTER RESTART. OPERATED BOTH PACKS. W/ PRESSURE BUILDING. IAW AMM 49-52-00. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA202143023](https://openairdocs.org/sdr/ABXA202143023.md): Shutoff Valve · stuck · Apr 3, 2021 · N768AX · Boeing 767281 · Engine Bleed Air System
  > RT ENG BLEED OFF LIGHT ON WITH ALSO THE RT PACK OFF LIGHT ON DURING TAXI. AIRCRAFT LINED UP FOR TAKE OFF AND RT ENG. BLEED LIGHT DID NOT EXTINGUISH DURING ENGINE ACCELERATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. REMOVE
- [SDR ABXA202112621](https://openairdocs.org/sdr/ABXA202112621.md): Control Panel · defective · Jan 26, 2021 · N768AX · Boeing 767281 · Pneumatic Distribution System
  > AFTER PUSH BACK, LEFT ENGINE WOULD NOT START DUE TO NO PNEUMATIC AIR. AIRCRAFT BTB AND GROUNDED. REMOVED AND REPLACED BLEED AIR SUPPLY CONTROL PANEL, IAW B767 AMM 36-11-26. OPERATIONS CHECK NORMAL, AIRCRAFT RELEASED.
- [SDR ABXA20200803228](https://openairdocs.org/sdr/ABXA20200803228.md): Apu · unknown · Dec 20, 2020 · N768AX · Boeing 767281 · APU Core Engine
  > APU AUTO SHUTDOWN AFTER PUSH BACK, BTB AIRCRAFT GROUNDED BY MAINTENANCE. CHECKED APU ECU, IAW B767 FIM 49-11 FAULT TREE 958, AND FOUND NO MESSAGES. STARTED APU AND RAN FOR.75 HOURS, RAN BOTH PACKS, DRY MOTORED NR 1 ENGINE AND NO DISCREPANCIES NOTED, IAW B76
- [SDR ABXA20200803207](https://openairdocs.org/sdr/ABXA20200803207.md): Valve · binding · Nov 4, 2020 · N768AX · Boeing 767281 · Heating System
  > AFT CARGO OVERHEAT LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE INSPECTED AND DEFERRED SYTEM AIRCRAFT WAS RELEASED FOR FLIGHT.
- [SDR ABXA20200710123](https://openairdocs.org/sdr/ABXA20200710123.md): Duct · ruptured · Jul 8, 2020 · N768AX · Boeing 767281 · Air Distribution System
  > AFTER ENGINE START, OVERHEAT (OVERHEAD LIGHT) ILLUMINATED ON EQUIPMENT COOLING PANEL WITH ASSOCIATED EICAS MESSAGE FORWARD EQUIPMENT COOLING OVERHEAT. VERY LOW AIRFLOW THROUGH AC GASPERS. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020061105066](https://openairdocs.org/sdr/ABXA2020061105066.md): Warning Light · illuminated · Jun 5, 2020 · N768AX · Boeing 767281 · Pitot/Static System
  > AFTER ENG. START THE F/O PITOT DISCREET LIGHT REMAINED ILLUMINATED WITH F/O PITOT EICAS MESSAGE DISPLAYED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020062955104](https://openairdocs.org/sdr/ABXA2020062955104.md): Stringer · corroded · May 15, 2020 · N768AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > STR 38R CORRODED JUST FWD OF STA 434 FACTORY SPLICE. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2020062914102](https://openairdocs.org/sdr/ABXA2020062914102.md): Door Sill · cracked · May 14, 2020 · N768AX · Boeing 767200 · Fuselage Miscellaneous Structure
  > LEFT EMER. EXIT HATCH LOWER SILL FRAME IS CRACKED AT STA.889. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2020062955105](https://openairdocs.org/sdr/ABXA2020062955105.md): Stringer Splice · corroded · May 5, 2020 · N768AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > FLC STRINGER 39R APPROX. STA.752 CORROSION ON SPLICE PLATE. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2020062951103](https://openairdocs.org/sdr/ABXA2020062951103.md): Shear Tie · cracked · May 1, 2020 · N768AX · Boeing 767281 · Fuselage Internal Mounting Structure
  > FORWARD LOWER CARGO STA 368 BETWEEN S38L-S37L SHEAR TIE CRACKED FROM RIVET HOLE. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2020062940101](https://openairdocs.org/sdr/ABXA2020062940101.md): Longeron Splice · corroded · Apr 30, 2020 · N768AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > LONGERON EXTENSION FITTING AT KEEL AT STA.785 S38L CORRODED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2019080624130](https://openairdocs.org/sdr/ABXA2019080624130.md): Controller · malfunctioned · Jul 24, 2019 · N768AX · Boeing 767281 · Pneumatic Distribution System
  > ON TAKEOFF/POWER UP, THE RIGHT ENGINE BLEED DISCRETE LIGHT ILLUMINATED. THE LEFT & RIGHT ENGINE BLEED EICAS & MASTER CAUTION LIGHTS ILLUMINATED AND THERE WAS A SMELL OF SOMETHING BURNING. THE TAKEOFF WAS ABORTED AT A SPEED OF LESS THAN 60 KNOTS. THE AIRPLANE W
- [SDR ABXA20180831100](https://openairdocs.org/sdr/ABXA20180831100.md): Support Beam · gouged · Aug 31, 2018 · N768AX · Boeing 767281 · Trailing Edge Flaps
  > GOUGE IN THE NR 7 FLAP SUPPORT BEAM NR 1 HOLE AT THE 12:00 POSITION. THE GOUGE DAMAGE WAS REMOVED BY REAMING THE HOLE BEYOND THE MAXIMUM PRODUCTION SIZE. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20180831099](https://openairdocs.org/sdr/ABXA20180831099.md): Support Beam · corroded · Aug 31, 2018 · N768AX · Boeing 767281 · Wing, Landing Gear Attach Fittings
  > CORROSION ON THE CHORD AFT OF THE MAIN LANDING GEAR SUPPORT BEAM AT RIGHT WING STATION 336. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20180831098](https://openairdocs.org/sdr/ABXA20180831098.md): Web · corroded · Aug 31, 2018 · N768AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT RIGHT FORWARD WING TO BODY AREA AT FUSELAGE STATION 720. THE WEB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20180831097](https://openairdocs.org/sdr/ABXA20180831097.md): Support · corroded · Aug 31, 2018 · N768AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON THE TRAILING EDGE PANEL SUPPORT UPPER CHORD AT RIGHT WING STATION 300. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20170130005](https://openairdocs.org/sdr/ABXA20170130005.md): Failsafe · cracked · Jan 30, 2017 · N768AX · Boeing 767281 · Fuselage Main, Structure
  > RIGHT FAILSAFE STRAP BS 955 CRACKED AT LOWER ATTACH HOLE COMMON TO TEE FITTING. CRACKED AREA TRIMED OUT AND REPAIRED IAW SDR. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20170130004](https://openairdocs.org/sdr/ABXA20170130004.md): Failsafe · cracked · Jan 30, 2017 · N768AX · Boeing 767281 · Fuselage Main, Structure
  > LEFT FAILSAFE STRAP BS 955, CRACKED AT LOWER ATTACH HOLE COMMON TO TEE FITTING. REMOVED AND REPLACED THE FAILSAFE STRAP IAW JOB CARD EA 53500013-007 AND INSTALLED A NEW FAILSAFE AIRCRAFT WAS GROUNDED.
- [SDR ABXA20170127010](https://openairdocs.org/sdr/ABXA20170127010.md): Frame · corroded · Jan 27, 2017 · N768AX · Boeing 767281 · Fuselage Main, Frame
  > TWO HOLES IN LEFT HAND SIDE FRAME FITTING (PICKLE FORK) COMMON TO FUSELAGE SKIN SIZE.309" HAVE DEFECT INDICATION FROM HFEC HOLE SCAN. REAMED HOLES UP UNTIL NO FURTHER DEFECTS WERE NOTED REA WAS GIVEN TO REPAIR THE HOLES. HOLES REPAIRED IN ACCORDANCE WITH REA
- [SDR ABXA20170127009](https://openairdocs.org/sdr/ABXA20170127009.md): Frame · corroded · Jan 27, 2017 · N768AX · Boeing 767281 · Fuselage Main, Frame
  > CORROSION FOUND ON FORWARD LOWER FACE OF LEFT HAND SIDE FRAME FITTING (PICKLE FORK) AROUND SEVEN FASTENER HOLES COMMON TO MATING SURFACE OF REAR SPAR WEB PAD UP AREAS. REMOVED CORROSION SPOT FACED COMMOMON TO BOLT HOLES. NDT CHECKED NO DEFECTS REMAINING ROTO P
- [SDR ABXA20170127008](https://openairdocs.org/sdr/ABXA20170127008.md): Structure · corroded · Jan 27, 2017 · N768AX · Boeing 767281 · Fuselage Main, Structure
  > AFT SPAR WEB HAS CORROSION ON THE PAD UP AREA COMMON TO MULTIPLE HOLES. REMOVED CORROSION, SPOT FACED CORROSION NEAR HOLES NDT CHECKED NO FURTHER DEFECTS NOTED ROTO PEENED BLENDED AND SPOT FACED AREAS REPAIRED BLENDED AND SPOT FACED AREAS IN ACCORDANCE WITH RE
- [SDR ABXA20170119007](https://openairdocs.org/sdr/ABXA20170119007.md): Failsafe · cracked · Jan 19, 2017 · N768AX · Boeing 767281 · Fuselage Main, Structure
  > LEFT FAILSAFE STRAP AT BS 955 IS CORRODED AND CRACKED PAST TRIM OUT LIMITS. REPLACED THE FAILSAFE.
- [SDR ABXA20160730126](https://openairdocs.org/sdr/ABXA20160730126.md): Bulkhead · corroded · Jul 30, 2016 · N768AX · Boeing 767281 · Fuselage Main, Bulkhead
  > FOUND UNACCOUNTED OIL CAN REPAIR NEAR THE OUTER EDGE STIFFENER. REMOVED UNACCOUNTED REPAIR STIFFENER IAW SRM 51-40-02, FABRICATED NEW STIFFENER IAW SRM 53-80-08, REPAIR 8, STEP 3, LOCATED IAW SRM 53-80-08. TREATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40
- [SDR ABXA20160730125](https://openairdocs.org/sdr/ABXA20160730125.md): Channel · cracked · Jul 30, 2016 · N768AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE COMPARTMENT. REMOVED REPAIR CHANNEL IAW SRM 51-40-02. FABRICATED NEW REPAIR CHANNEL IAW SRM 53-80-08, REPAIR 3, PG 203, LOCATED CHANNEL IAW SRM 53-80-08. TREATED CHANNEL IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02 AND 53-80-08. REF REO G20
- [SDR ABXA20160728119](https://openairdocs.org/sdr/ABXA20160728119.md): Keelbeam · corroded · Jul 28, 2016 · N768AX · Boeing 767281 · Fuselage Main, Keel
  > CORROSION AT BS 990 - 1010 LEFT SIDE OF KEEL BEAM ALONG THE UPPER SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 53-50-12. REPAIRED IAW SRM 53-50-12 REPAIR 1, REO-G20121 REV. A, AND REA B653-62037MR.
- [SDR ABXA20160727123](https://openairdocs.org/sdr/ABXA20160727123.md): Bracket · cracked · Jul 27, 2016 · N768AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > AFT CARGO STA 1087 UNDER STR 38L JUST AFT OF FORWARD BULKHEAD HAS EVALUATED BLEND ON STR 38L IN AFT CARGO STA 1087 AFT OF FORWARD BULKHEAD, ORIGINAL MATERIAL THICKNESS.125", REMOVED.048", REMAINING THICKNESS.077". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15
- [SDR ABXA20160720124](https://openairdocs.org/sdr/ABXA20160720124.md): Beam · corroded · Jul 20, 2016 · N768AX · Boeing 767281 · Fuselage Main, Structure
  > FORWARD CARGO DOOR LOWER SILL BEAM UPPER SURFACE CORRODED AT AFT REPAIRED FORWARD CARGO DOOR LOWER SILL BEAM UPPER SURFACE, HIGH FREQUENCY, NO CRACKS NOTED. INSTALLED NEW FASTENERS IAW SRM 51-40-02. INNER CHORD, PART LOCATION: FLC STA 624-628 AT RBL44, PN: 1
- [SDR ABXA20170720121](https://openairdocs.org/sdr/ABXA20170720121.md): Skin · cracked · Jul 20, 2016 · N768AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > CRACK INDICATION FOUND L-1 DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED FUSELAGE SKIN STA 287 TO STA 347, S18L TO S24L BELOW L-1 DOOR IAW REO-G20052, REV B AND NR-B653-62038MR. SDR INFO: PART NAME: FUSELAGE SKIN, PN: 141T3331-5, SN: NSN, STA 287-347, LT BELOW

Next page: https://openairdocs.org/aircraft/N768AX/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 = 'N768AX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N768AX/reports

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