# Service difficulty reports: N797AX

A list on [N797AX](https://openairdocs.org/aircraft/N797AX.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 4 · 155 reports

- [SDR ABXA2024012300014](https://openairdocs.org/sdr/ABXA2024012300014.md): Fuel Sys · warning light · Jan 20, 2024 · N797AX · Boeing 767281 · Aircraft Fuel System
  > FUEL CONFIGURATION LIGHT ON. TRIED TRANSFERING FROM LEFT TO RIGHT, UNABLE TO EXTINGUISH FUEL CONFIGURATION LIGHT AC RETURNED TO BLOCKS AND MAINTENANCE TRANSFERRED FUEL FROM LEFT TO RIGHT.NO DEFECTS NOTED IAW AMM 28-00-00 RETURNED AC TO SERVICE.
- [SDR ABXA2024010805](https://openairdocs.org/sdr/ABXA2024010805.md): Unknown · unknown · Jan 8, 2024 · N797AX · Boeing 767281 · AC Generator-Alternator
  > AFTER ENGINE START RT GEN DRIVE LIGHT DID NOT EXTINGUISH. AC RETURNED TO GATE AND GROUNDED BY MAINTENANCE, MAINTENANCE RESET INPUT DRIVE RING.IAW AMM 24-11-00 OPS CHECK GOOD.AND RETURNED AC TO SERVICE.
- [SDR ABXA2024010502](https://openairdocs.org/sdr/ABXA2024010502.md): Unknown · unknown · Jan 5, 2024 · N797AX · Boeing 767281 · Electrical Power System
  > ON ENG START L GEN DRIVE & L GEN OFF EICAS ILLUMINATED-CREW DISCONNECTED L GEN IDG AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC. MAINTENANCE RESET LH ENG GEN FIELD AND RECONNECTED IDG. OPS CHECK GOOD IAW AMM 24-11-00. AC RETURNED TO SERVICE.
- [SDR ABXA20230518109](https://openairdocs.org/sdr/ABXA20230518109.md): Smoke Detector · defective · May 16, 2023 · N797AX · Boeing 767281 · Fire Detection
  > DURING DESCENT THE FWD EQPT SMOKE EICAS MESSAGE AND EQUIPMENT COOLING SMOKE ANNUNCIATOR LIGHT ILLUMINATED. FOLLOWED QRH BOTH LIGHTS STAYED ILLUMINATED. CONTACTED ATC AND DECLARED AN EMERGENCY AND REQUESTED CLEARANCE DIRECT TO KCVG. WE WERE CLEARED DIRECT TO TH
- [SDR ABXA20221118128](https://openairdocs.org/sdr/ABXA20221118128.md): Overheat · false indication · Nov 17, 2022 · N797AX · Boeing 767281 · Cabin Cooling System
  > AFTER BOTH ENGINE STARTS RECEIVED A FWD EQUIP OVERHEAT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS TEST. EQ. COOLING MANUAL TEST PER AMM 21-58-00 NO EICAS MSG NOTED RAN THE SYSTEM FOR 15 MINUTES. OPS CHECKED GOOD. AIRCRAFT RE
- [SDR ABXA202209302187](https://openairdocs.org/sdr/ABXA202209302187.md): Control Panel · faulted · Aug 31, 2022 · N797AX · Boeing 767281 · Autopilot System
  > LEFT AND RIGHT AUTOPILOTS BECAME INOPERATIVE.CREW ELECTED TO TURN BACK TO CVG. AIRCRAFT LANDED WITHOUT FURTHER INCIDENCE. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED MCP IAW AMM 22-41-01, OPS GOOD, A/C RETURNED TO SERVICE.
- [SDR ABXA2022071177](https://openairdocs.org/sdr/ABXA2022071177.md): None · none · Jul 11, 2022 · N797AX · Boeing 767 · Air Conditioning System
  > AFTER FLAP RETRACTION ON TAKEOFF FLIGHT DECK TEMP BEGIN TO RISE UP TO 47'C WE TRIED TO GAIN CONTROL OF TEMP BY GOING TO STANDBY N, DID NOT WORK. ALSO TRIED OPERATING TRIM AIR VALVE IN MANUAL DID NOT WORK. ALSO TRIED TURNING THE TRIM AIR SWITCH OFF, DID NOT WOR
- [SDR ABXA2023050474](https://openairdocs.org/sdr/ABXA2023050474.md): Splice Plate · corroded · Apr 18, 2022 · N797AX · Boeing 767281 · Wing Structure
  > DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE LEFT WING FIXED LEADING EDGE UPPER SPLICE PLATE(114T0223-19) FWD OF THE FRONT SPAR. CORROSION IS LOCATED AT APPROXIMATELY WS 450. CORROSION WAS REMOVED BY BLENDING AND MIN
- [SDR ABXA2022031647](https://openairdocs.org/sdr/ABXA2022031647.md): Skin · corroded · Mar 16, 2022 · N797AX · Boeing 767281 · Wing Miscellaneous Structure
  > DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE LH WING SKIN PANEL NO. 1(112T4102-1) AT THE REAR SPAR AND WS 440-450. THE CORROSION IS LOCATED ON THE UPPER SURFACE OF THE BOTTOM SKIN AND TRAVELS BETWEEN THE SKIN AND REAR SPAR, AND
- [SDR ABXA2022030146](https://openairdocs.org/sdr/ABXA2022030146.md): None · corroded · Mar 1, 2022 · N797AX · Boeing 767281 · Fuselage Structure (General)
  > DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL OUTER CHORD(143T8004-1). THE NOMINAL THICKNESS OF THE CHORD IN THE SUBJECT AREA IS 0.300 INCH. THE MINIMUM REMAINING THICKNESS IN THE AREA IS 0.226 INCH
- [SDR ABXA20211023107](https://openairdocs.org/sdr/ABXA20211023107.md): Valve · intermittent · Oct 23, 2021 · N797AX · Boeing 767281 · Tire
  > ANTISKID OFF EICAS MSG. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REPLACED PARKING BRAKE VALVE IAW AMM 32-44-04. PERFORMED OPS CHECK OF PARKING BRAKE SYSTEM IAW B767 AMM 32-44-00-730-801. ALL TEST PASS. NO LEAKS NOTED. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021107097](https://openairdocs.org/sdr/ABXA2021107097.md): Mechanism · damaged · Oct 7, 2021 · N797AX · Boeing 767281 · Aileron Control System
  > AILERON CONTROL CHECK AND CONTROL YOKE WILL NOT SPRING RETURN TO CENTER, AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LEFT LATERAL CONTROL FEEL, CENTERING AND TRIM MECHANISM DAMAGED.REMOVED AND REPLACED IAW AMM 27-22-08. RII-27-03 COMPL
- [SDR ABXA20200803216](https://openairdocs.org/sdr/ABXA20200803216.md): Shutoff Valve · intermittent · Nov 13, 2020 · N797AX · Boeing 767281 · Cabin Cooling System
  > HOLDING NR 1, SUDDENLY GOT WARM IN COCKPIT. WINDOWS FOGGED, THEN EICAS COMPACTED. BOTH PILOT EADI/EHSI WENT FULL BRIGHT. THEN F/O'S EADI BLANKED. AIRCRAFT BACK TO BLOCK AND GROUNDED. CONDUCTED EQUIPMENT COOLING SYSTEM BIT, IAW B767 FIM 21-58 FT 873, NO FAU
- [SDR ABXA20200803154](https://openairdocs.org/sdr/ABXA20200803154.md): Pump · failed · Jul 31, 2020 · N797AX · Boeing 767281 · Engine Fuel Pump
  > LEFT ENGINE HAD NO FUEL FLOW ON START. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020030520042](https://openairdocs.org/sdr/ABXA2020030520042.md): Panel · corroded · Feb 20, 2020 · N797AX · Boeing 767281 · Wing, Plate/Skin
  > LH WING FUEKL TANK PANEL 533AB CORRODED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020030514044](https://openairdocs.org/sdr/ABXA2020030514044.md): Angle · corroded · Feb 14, 2020 · N797AX · Boeing 767200 · Fuselage Miscellaneous Structure
  > LH MLG WW HAS LIGHT CORROSION AT STA 1021 JUST AFT OF CENTER SYSTEM HYD RETURN CONNECTION. AIRCRAFT WA GROUNDED.
- [SDR ABXA2020030514043](https://openairdocs.org/sdr/ABXA2020030514043.md): Attach Angle · corroded · Feb 14, 2020 · N797AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > LH WW AR STA 1021 ATTACH ANGLE CORRODED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020030513041](https://openairdocs.org/sdr/ABXA2020030513041.md): Stringer Splice · corroded · Feb 13, 2020 · N797AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > BOTH HOLES ON AFT STRINGER SPLICES AT STA 676 S25L ARE CRACKED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020030512040](https://openairdocs.org/sdr/ABXA2020030512040.md): Keelbeam · corroded · Feb 12, 2020 · N797AX · Boeing 767281 · Fuselage Main, Keel
  > LH WW KEEL BEAM WEB AREA AT APPROX. STA 1049 HAS CORROSION. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020030511039](https://openairdocs.org/sdr/ABXA2020030511039.md): Attach Angle · corroded · Feb 11, 2020 · N797AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > LH WW ATTACH ANGLE IB OF DOOR ACTUATOR HAS AREA OF CORROSION. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2020030511038](https://openairdocs.org/sdr/ABXA2020030511038.md): Attach Angle · corroded · Feb 11, 2020 · N797AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > LH WW ATTACH ANGLE IB OF DOOR ACTUATOR HAS AREA OF CORROSION. AIRCRAFT WAS GROUNDED.
- [SDR ABXA2019120218176](https://openairdocs.org/sdr/ABXA2019120218176.md): Light · unknown · Nov 18, 2019 · N797AX · Boeing 767200 · Emergency Lighting
  > THE RIGHT FORWARD DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE EMERGENCY LIGHTS WERE TROUBLESHOT IN ACCORDANCE WITH THE 767 FIM 33-51, FAULT TREE 803. THE M735 EMERGENCY LIGHTS POWER SUPPLY AND THE M736 E
- [SDR ABXA201812030136](https://openairdocs.org/sdr/ABXA201812030136.md): Ring · corroded · Nov 20, 2018 · N797AX · Boeing 767281 · Fuselage Main, Structure
  > CORROSION IN THE SECTION 48 PRESSURE RING (BODY STATION 1582) AT THREE BOLT LOCATIONS: S27R (UPPER/OUTBOARD), S33R (UPPER/OUTBOARD), AND S36L (LOWER/INBOARD). THE PRESSURE RING WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201812030135](https://openairdocs.org/sdr/ABXA201812030135.md): Splice · corroded · Nov 20, 2018 · N797AX · Boeing 767281 · Fuselage Main, Structure
  > CORROSION IN THE TENSION BOLT HOLE OF SPLICE FITTING AT BODY STATION 1809.5, WATER LINE 214.76. THE SPLICE FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201812030134](https://openairdocs.org/sdr/ABXA201812030134.md): Skin · corroded · Nov 20, 2018 · N797AX · Boeing 767281 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON THE UPPER RIGHT HORIZONTAL STABILIZER SKIN PANEL AT RIB STATION 12 AND STRINGER 3. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2018072709077](https://openairdocs.org/sdr/ABXA2018072709077.md): Skin · dented · Jul 9, 2018 · N797AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > TWO DENTS ON THE FUSELAGE SKIN AT STATION 632. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201806215069](https://openairdocs.org/sdr/ABXA201806215069.md): Skin · dented · Jun 15, 2018 · N797AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN ADJACENT TO BS 632 FRAME, BETWEEN STRINGERS 24L AND 25L WAS DENTED. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20180318030](https://openairdocs.org/sdr/ABXA20180318030.md): Support · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON THE SUPPORT AT BS 1417. THE SUPPORT WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20180318029](https://openairdocs.org/sdr/ABXA20180318029.md): Tee Fitting · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON THE RIGHT WING TEE FITTING AT WS 255. THE TEE FITTING WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20180318028](https://openairdocs.org/sdr/ABXA20180318028.md): Splice Plate · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON THE RIGHT WING INBOARD RIGHT MAIN LANDING GEAR SPLICE PLATE AT WS 255. THE SPLICE PLATE WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20180318027](https://openairdocs.org/sdr/ABXA20180318027.md): Support Beam · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Fuselage Main, Structure
  > CORROSION ON THE BULK CARGO BAY LOWER NET SUPPORT BEAM AT BS 1413. THE SUPPORT BEAM WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20180318026](https://openairdocs.org/sdr/ABXA20180318026.md): Skin · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > CORROSION ON THE FUSELAGE SKIN AT BS 756 BETWEEN STRINGERS 34R AND 35R. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20180318025](https://openairdocs.org/sdr/ABXA20180318025.md): Stringer · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 34L AT BS 748. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20180318024](https://openairdocs.org/sdr/ABXA20180318024.md): Panel · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing, Plate/Skin
  > CORROSION ON THE LEFT WING LOWER TRAILING EDGE PANEL LOWER SURFACE BETWEEN WING STATIONS 903 AND 909. THE PANEL WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20180318023](https://openairdocs.org/sdr/ABXA20180318023.md): Beam · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON THE LEFT WING NOSE BEAM BETWEEN OUTBOARD SPAR OSS 783 AND 791 AND BETWEEN OUTBOARD SPAR OSS 884 AND 909. THE NOSE BEAM SECTIONS WERE REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20180318022](https://openairdocs.org/sdr/ABXA20180318022.md): Splice Plate · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON THE RIGHT WING OUTBOARD FRONT SPAR LOWER PANEL ATTACH STRUCTURE (SPLICE PLATE) AT OUTBOARD FRONT SPAR STATION 925. THE SPLICE PLATE WAS REPAIRED. ACFT WAS GROUNDED.
- [SDR ABXA20180318021](https://openairdocs.org/sdr/ABXA20180318021.md): Beam · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing Main, Frame Structure
  > CORROSION ON THE RIGHT WING INBOARD SPOILER BEAM UPPER CHORD BETWEEN WS 282 AND 432. THE CHORD WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20180318020](https://openairdocs.org/sdr/ABXA20180318020.md): Spar · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing Spar
  > CORROSION ON THE RIGHT WING AFT SPAR UPPER ANGLE AT WS 470. THE ANGLE WAS REPAIRED. THE ACFT WAS GROUNDED.
- [SDR ABXA201803280019](https://openairdocs.org/sdr/ABXA201803280019.md): Skin · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Wing, Plate/Skin
  > CORROSION ON THE RIGHT WING UPPER SKIN LOWER SURFACE AT WING STATION 470. THE SKIN WAS REPAIRED. THE ACFT WAS GROUNDED.
- [SDR ABXA20180318018](https://openairdocs.org/sdr/ABXA20180318018.md): Bulkhead Web · corroded · Mar 18, 2018 · N797AX · Boeing 767281 · Fuselage Main, Bulkhead
  > CORROSION ON THE MAIN LANDING GEAR WHEEL WELL PRESSURE BULKHEAD WEB AT BS 955. THE BULHEAD WEB WAS REPAIRED. ACFT WAS GROUNDED.
- [SDR ABXA20170830099](https://openairdocs.org/sdr/ABXA20170830099.md): Carabiner · missing · Aug 30, 2017 · N797AX · Boeing 767281 · Emergency Equipment
  > ONE EMERGENCY DESCENT SAFETY HARNESS CARABINER WAS MISSING FROM ITS STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), A NEW SAFETY HARNESS CARABINER WAS INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINER IS UNKNOWN.
- [SDR ABXA20160718117](https://openairdocs.org/sdr/ABXA20160718117.md): Skin · corroded · Jul 18, 2016 · N797AX · Boeing 767200 · Fuselage Main, Plate/Skin
  > REMOVED CORROSION IAW SRM 57-51-02, FIG 101. INITIAL THICKNESS.094, REMAINING THICKNESS.061. BLENDED AREAS REQUIRED REPAIR AND WERE REPAIRED ON REA B657-62130. CORRODED LEVEL 2, PN 113T1621-58, SKIN, FS/BS LOCATION: FROM R/W T/E TO UPPER STR, WS LOCATION:
- [SDR ABXA20160718116](https://openairdocs.org/sdr/ABXA20160718116.md): Skin · corroded · Jul 18, 2016 · N797AX · Boeing 767200 · Fuselage Main, Plate/Skin
  > FOUND SKIN CORROSION COMMON TO THE TRIMMED OUT SECTION OF THE FAIL SAFE. CORROSION IS ISOLATED TO THE LOWER HOLE. COMPLIED WITH TASK CARD EA 53500014-004 AND DOCUMENT 470080RD10 CORROSION WAS REMOVED, WITHIN THE ALLOWABLE LIMITS. CORRODED, LEVEL 2, PN 145T34
- [SDR ABXA20160718115](https://openairdocs.org/sdr/ABXA20160718115.md): Failsafe · cracked · Jul 18, 2016 · N797AX · Boeing 767200 · Fuselage Main, Frame
  > COMPLIED WITH TC S53-050·04-2. RT WHEEL WELL STA 955, RT FAIL-SAFE HAS HFEC DEFECT INDICATION AT LOWER HOLE COMMON TO FAIL-SAFE AND TEE FITTING. REF: SB 767-53A0100, FIG 2, SH 1. COMPLIED WITH FAIL SAFE TRIM OUT AT TC EA 53500014-003 AND DOCUMENT 47008 AND 04
- [SDR ABXA20160628106](https://openairdocs.org/sdr/ABXA20160628106.md): Unknown · odor · Jun 28, 2016 · N797AX · Boeing 767281 · Air Distribution System
  > BOTH CREW MEMBERS SMELLED A STRONG ELECTRICAL ODOR. THE MAIN EQUIPMENT CENTER WAS INSPECTED. THERE WAS NO EVIDENCE OF BURNED WIRES OR EQUIPMENT. THE CAUSE OF THE ODOR WAS NOT FOUND.
- [SDR ABXA20160212031](https://openairdocs.org/sdr/ABXA20160212031.md): Beam · corroded · Feb 12, 2016 · N797AX · Boeing 767200 · Wing Miscellaneous Structure
  > WING TE UPPER PANEL ATTACH BEAM RUNNING LENGTH WAYS, CORRODED ON FWD SIDE AT WS.273, INBD OF NR 6 SPOILER, AS SEEN THRU PANEL 551VB OPENING. REMOVED ATTACH BEAMS & INSTALLED SERVICEABLE ATTACH BEAMS, PN 113T1633-157 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 11
- [SDR ABXA20160211028](https://openairdocs.org/sdr/ABXA20160211028.md): Structure · corroded · Feb 11, 2016 · N797AX · Boeing 767200 · Fuselage Main, Attach Fittings
  > UPPER WING TE PANEL, ATTACH CHORD AT WING TO FUSELAGE JUNCTION, ABOVE UPLOCK CYLINDER, CORRODED AROUND NUTPLATES. REMOVED ATTACH CHORD & INSTALLED SERVICEABLE ATTACH CHORD, PN 113T1621-55 IAW SRM 51-40-2. CORRODED LEVEL 2, PN 113T1621-55, PART NAME ATTACH CO
- [SDR ABXA20160210030](https://openairdocs.org/sdr/ABXA20160210030.md): Structure · corroded · Feb 10, 2016 · N797AX · Boeing 767200 · Wing Miscellaneous Structure
  > UPPER CHORD CORRODED ON REAR SPAR TO WING TE BEAM, AT STATION 285, AT AFT END AS SEEN UNDER INBD END OF NR 6 SPOILER. REMOVED TE BEAM ASSEMBLY, R & R UPPER CHORD, PN 113T1623-141, WITH SERVICEABLE CHORD, INSTALLED TE BEAM ASSEMBLY IAW SRM 51-40-2. CORRODED L
- [SDR ABXA20160210027](https://openairdocs.org/sdr/ABXA20160210027.md): Structure · corroded · Feb 10, 2016 · N797AX · Boeing 767200 · Fuselage Miscellaneous Structure
  > STATION 859.5, RBL 89 INNER CHORD CRACKED.450" APPROX AT TRANSITION RADIUS, IAW ES02568 FIG 1 SH 2 ATTACHED TO NEA 53000045-001 FOR CRACK LOCATION. REPAIRED INNER CHAP AT STRINGER 859.5, RBL 89. IAW EA 53000048-101 & REA B653-61905-513. CORROSION LEVEL 2, P
- [SDR ABXA20160208029](https://openairdocs.org/sdr/ABXA20160208029.md): Beam · corroded · Feb 8, 2016 · N797AX · Boeing 767200 · Spoilers
  > WING TE AFT LOWER CHORD FOR PANEL 552HB AT TE WS 418 SPLIT ON EDGE. R & R CHORD AT STATION 418 IAW SRM 51-40-02. FABRICATED CHORD, PN 133T1407-1, IAW REA B657-61929MR. CORRODED LEVEL 2, PN 113T1407-1, SN NSN, PART NAME, SPOILER BEAM CHORD LOWER, EXACT FS &

Next page: https://openairdocs.org/aircraft/N797AX/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 = 'N797AX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N797AX/reports

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