# Service difficulty reports: N788AX, cancelled Nov 15, 2018 A list on [N788AX, cancelled Nov 15, 2018](https://openairdocs.org/deregistered/N788AX-2018-11-15.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 · 76 reports - [SDR ABXA201811263126](https://openairdocs.org/sdr/ABXA201811263126.md): Skin · dented · Oct 23, 2018 · N788AX · Boeing 767281 · Leading Edge Devices > DENT ON #12 SLAT (RIGHT WING) UPPER SKIN AT OUTBOARD SLAT STATION 992. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA2018112623123](https://openairdocs.org/sdr/ABXA2018112623123.md): Failsafe · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Fuselage Main, Structure > CORROSION ON FORWARD LOWER CARGO DOOR INNER SILL FAIL SAFE STRAP. REPLACED FAIL SAFE STRAP. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811263122](https://openairdocs.org/sdr/ABXA201811263122.md): Door Frame · cracked · Oct 23, 2018 · N788AX · Boeing 767281 · Fuselage Main, Structure > CRACK IN THE FRAME OF THE LOWER AFT CORNER OF THE L1 DOOR. THE FRAME WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811263121](https://openairdocs.org/sdr/ABXA201811263121.md): Beam · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Horizontal Stabilizer Structure > CORROSION ON THE RIGHT HORIZONTAL STABILIZER FIXED TRAILING EDGE BEAM UPPER CHORD BETWEEN ELEVATOR STATIONS 237 AND 261. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811263120](https://openairdocs.org/sdr/ABXA201811263120.md): Spar · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > CORROSION ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD BETWEEN REAR SPAR STATIONS 200 AND 226.6. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213119](https://openairdocs.org/sdr/ABXA201811213119.md): Fitting · chafed · Oct 23, 2018 · N788AX · Boeing 767281 · Nacelle/Pylon, Attach Fittings > CHAFE ON #1 PYLON INBOARD SIDE LOAD FITTING AT NACELLE STATION 302. THE WEAR AREA MEASURED 3.60” LONG X 0.150” WIDE X 0.043” DEEP (ENTIRE LENGTH). THE FITTING WAS REPAIRED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213118](https://openairdocs.org/sdr/ABXA201811213118.md): Angle · cracked · Oct 23, 2018 · N788AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure > CHAFE AND CRACK ON #1 PYLON INBOARD HYDRAULIC BAY LOWER BEAM ZEE ANGLE. THE ZEE ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA2018112103117](https://openairdocs.org/sdr/ABXA2018112103117.md): Skin · dented · Oct 23, 2018 · N788AX · Boeing 767281 · Leading Edge Devices > DENT ON #12 SLAT ON TOP SKIN. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213116](https://openairdocs.org/sdr/ABXA201811213116.md): Attach Fitting · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing, Attach Fittings > CORROSION ON LEFT WING TRAILING EDGE LOWER PANEL ATTACH CHORD. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213115](https://openairdocs.org/sdr/ABXA201811213115.md): Attach Fitting · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing, Attach Fittings > CORROSION ON RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH CHORD AT WING STATION 433. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213114](https://openairdocs.org/sdr/ABXA201811213114.md): Attach Fitting · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing, Attach Fittings > CORROSION ON LEFT WING LEADING EDGE LOWER PANEL ATTACH STRUCTURE. REPLACED WEB. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213113](https://openairdocs.org/sdr/ABXA201811213113.md): Rib · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing, Rib/Bulkhead > CORROSION ON THE #4 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. THE AIRLOAD RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213112](https://openairdocs.org/sdr/ABXA201811213112.md): Spar · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing Spar > CORROSION ON THE LEFT WING LEADING EDGE FRONT SPAR AT LEADING EDGE STATION 867. THE FRONT SPAR'S WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213111](https://openairdocs.org/sdr/ABXA201811213111.md): Rib · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing, Rib/Bulkhead > CORROSION ON #2 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213110](https://openairdocs.org/sdr/ABXA201811213110.md): Rib · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing, Rib/Bulkhead > CORROSION ON #1 SLAT INBOARD AUX TRACK INBOARD LOWER STRUT. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213108](https://openairdocs.org/sdr/ABXA201811213108.md): Circuit Breaker · failed · Oct 23, 2018 · N788AX · Boeing 767281 · AC Power Distribution System > EXCESSIVE HEAT AT C10 CIRCUIT BREAKER "C BUS PWR" INSIDE P6-2 PANEL. REPLACED CIRCUIT BREAKER C884 AND WIRE W1032-004-6. THE AIRPLANE WAS GROUNDED. THE CAUSE OF THE EXCESSIVE HEAT IS UNKNOWN. - [SDR ABXA201811213107](https://openairdocs.org/sdr/ABXA201811213107.md): Structure · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Horizontal Stabilizer Structure > CORROSION ON LOWER FLANGE ON RIGHT HORIZONTAL STABILIZER CHORD 17. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213106](https://openairdocs.org/sdr/ABXA201811213106.md): Strut · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Wing Main, Frame Structure > CORROSION ON LOWER STRUT ON AIRLOAD RIB ON RIGHT WING. THE STRUT WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213104](https://openairdocs.org/sdr/ABXA201811213104.md): Doubler · corroded · Oct 23, 2018 · N788AX · Boeing 767281 · Ailerons > CORROSION ON DOUBLER FORWARD OF THE OUTBOARD AILERON ON THE LEFT WING. THE DOUBLER WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA201811213105](https://openairdocs.org/sdr/ABXA201811213105.md): Stiffener · cracked · Oct 23, 2018 · N788AX · Boeing 767281 · Fuselage Miscellaneous Structure > CRACK IN THE MAIN DECK CARGO FLOOR BEAM VERTICAL STIFFENER AT FUSELAGE STATION 266.5. THE STIFFENER WAS REPLACED. THE AIRPLANE WAS GROUNDED. - [SDR ABXA2018072713078](https://openairdocs.org/sdr/ABXA2018072713078.md): Skin Panel · chafed · Jul 13, 2018 · N788AX · Boeing 767281 · Wing, Plate/Skin > CHAFE DAMAGE TO THE LOWER WING SKIN PANEL # 1 (P/N: 111T4015-4) AND LOWER CENTER WING BEAM (LBL 62.05) WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWER CHORD (P/N: 111T5012-17). THE CHAFE AREA COMMON TO THE LOWER CENTER WING SKIN PANEL # 1 MEASURED W - [SDR ABXA201807132076](https://openairdocs.org/sdr/ABXA201807132076.md): Beam · chafed · Jul 12, 2018 · N788AX · Boeing 767281 · Wing Main, Frame Structure > CHAFING AT BODY STATION 900, LBL 57 ON THE LOWER WING SKIN PANEL (P/N: 111T4015-4) AND LOWER CENTER WING BEAM WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWER CHORD (P/N: 111T5012-17). THE SKIN PANEL, WEB, DOUBLER, AND CHORD WERE REPAIRED. THE AIRPLA - [SDR ABXA20171205145](https://openairdocs.org/sdr/ABXA20171205145.md): Escape Reel · missing · Dec 5, 2017 · N788AX · Boeing 767281 · Emergency Equipment > ONE EMERGENCY DESCENT SAFETY HARNESS WAS MISSING FROM ITS STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), A NEW SAFETY HARNESS WAS INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING HARNESS IS UNKNOWN. - [SDR ABXA20170624071](https://openairdocs.org/sdr/ABXA20170624071.md): Unknown · odor · Jun 24, 2017 · N788AX · Boeing 767281 · Air Distribution System > WHILE THE LEFT ENGINE WAS IN OPERATION, THE LEFT PRESSURE REGULATING SHUTOFF VALVE WAS CLOSED. A STRONG ODOR WAS ASSOCIATED WITH IT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT ENGINE WAS OPERATED WITH NO DEFECT FOUND. THE CAUSE OF THE ODOR W - [SDR ABXA2016216004](https://openairdocs.org/sdr/ABXA2016216004.md): Coupling · failed · Feb 16, 2016 · N788AX · Boeing 767281 · Air Distribution System > WITH THE EQUIPMENT COOLING SWITCH IN OVRD POSITION & BOTH PACKS OPERATING AT 39,000 FEET, THE CABIN ALTITUDE CLIMBED TO 11,000 FEET. THE FLIGHT CREW DESCENDED TO 10,000 FEET TO REGAIN PRESSURIZATION. REPLACED THE COUPLING & SEAL THAT JOINS THE CONDITIONED AI - [SDR ABXA20150502068](https://openairdocs.org/sdr/ABXA20150502068.md): Mec · faulty · May 1, 2015 · N788AX · Boeing 767281 · Fuel Control/Turbine Engines > ADVANCED THRUST LEVER APPROX HALF WAY FOR TAKEOFF ON LT ENG & ENG WOULD NOT ACCELERATE. REPLACED LT ENG MAIN ENG CONTROL. - [SDR ABXA20150227017](https://openairdocs.org/sdr/ABXA20150227017.md): Smoke Detector · false activation · Feb 27, 2015 · N788AX · Boeing 767281 · Smoke Detection > LAVATORY SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. REPLACED LAVATORY SMOKE DETECTOR. - [SDR ABXA20150224031](https://openairdocs.org/sdr/ABXA20150224031.md): Beam · corroded · Feb 24, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous Structure > DURING OK TO CLOSE OF LE PANELS FOUND CORROSION ON NUT STRIP ON FIXED LE AT APPROX LES 590. FOUND CORROSION TO BE ON NOSE BEAM WEB COMMON TO NUTPLATES. REMOVED WEB & FABRICATED NEW ONE FROM 7075-76-050 PO 0056503. INSTALLED NEW WEB & REMOVED ASSEMBLY IAW SR - [SDR ABXA20150224029](https://openairdocs.org/sdr/ABXA20150224029.md): Beam · corroded · Feb 24, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer Miscellaneous Structure > LEFT HORIZONTAL STABILIZER UPPER REAR BEAM HAS AREAS OF CORROSION FROM ELEVATOR STATION 49 - 302. OUT OF LIMITS AREA ELEVATOR STATION 146 - 150.5. REPAIRED IAW REA B655-61427. THREE BLEND LOCATIONS FOUND TO BE WITHIN ACCEPTABLE LIMITS WHEN COMBINING SRM 55- - [SDR ABXA20150224020](https://openairdocs.org/sdr/ABXA20150224020.md): Angle · cracked · Feb 24, 2015 · N788AX · Boeing 767281 · Vertical Stabilizer, Attach Fittings > VERTICAL STABILIZER TO SKIN ANGLE LT OTBD END CRACKED, ACCESS THROUGH PANEL 324AL. REMOVED ANGLE, FABRICATED NEW ANGLE IAW DWG 173T1302 FROM 2024-T3.040. PERFORMED HFEC INSPECTION. INSTALLED NEW ANGLE IAW SRM 5140-02. SDR INFO, CRACKED 1.900", PN 173T1302 - [SDR ABXA20150222028](https://openairdocs.org/sdr/ABXA20150222028.md): Rib · corroded · Feb 22, 2015 · N788AX · Boeing 767281 · Wing, Rib/Bulkhead > RIGHT WING TE LOWER CHORD OF SUPPORT RIB AT WS 1080 IS CORRODED & SPLIT. R & R RT WING TE LOWER CHORD OF SUPPORT RIB WS 1080 IAW SRM 51-40-02 & DOC 113T1521 REV 6. FABRICATED ON REA B657-61431. SDR INFO, PN 113T1521-16, PART NAME CHORD, SN NSN, CORRODED LEV - [SDR ABXA20150221026](https://openairdocs.org/sdr/ABXA20150221026.md): Spar · corroded · Feb 21, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > LEFT HORIZONTAL STABILIZER REAR SPAR & TE BEAM ARE CORRODED AT ELEVATOR STATION 325. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD ELEVATOR STATION 321.5 - 337.5 IAW REA B655-61425-MR. TE BEAM AT ELEVATOR STATION 325 FOUND TO - [SDR ABXA20150221025](https://openairdocs.org/sdr/ABXA20150221025.md): Spar · corroded · Feb 21, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > LEFT HORIZONTAL STABILIZER REAR SPAR IS CORRODED AT ELEVATOR STATION 139 - 143. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR UPPER CHORD ELEVATOR STATION 139 - 143 IAW REA B655-61435-MR. SDR INFO, PN 182T1100-1, PART NAME REAR SPAR UPPER CHOR - [SDR ABXA20150221022](https://openairdocs.org/sdr/ABXA20150221022.md): Rib · corroded · Feb 21, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 91 UPPER CHORD OF THE TE RIB IS CORRODED. R & R CHORD PN 183T1400-5 IAW SRM 51-40-02. SDR INFO, PN 183T1400-5, PART NAME UPPER CHORD, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT ELEVATOR STATION 91. - [SDR ABXA20150220027](https://openairdocs.org/sdr/ABXA20150220027.md): Structure · cracked · Feb 20, 2015 · N788AX · Boeing 767281 · Fuselage Miscellaneous Structure > EA 53500009-001 NEEDS ACCOMPLISHED. REPAIRED DAMAGED CHORD RT STATION 883.5 STRINGER 18R IAW SRM 53-50-07 REPAIR 1. SDR INFO CRACKED 0.250", PN 145T8000-1, SN N/A, PART NAME CHORD, FS LOCATION ON ACFT, FS 883.5, STRINGER LOCATION ON ACFT, STRINGER 18R. ACFT - [SDR ABXA20150220023](https://openairdocs.org/sdr/ABXA20150220023.md): Rib · corroded · Feb 20, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IS CORRODED. INSTALLED NEW LT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IAW REA B657-61411-MR & SRM 51-40-02. SDR INFO, CORRODED LEVEL 2, PN 183T1340-29, P - [SDR ABXA20150220021](https://openairdocs.org/sdr/ABXA20150220021.md): Keelbeam · corroded · Feb 20, 2015 · N788AX · Boeing 767281 · Fuselage Main, Keel > RIGHT KEEL BEAM LOWER INBD FLANGE LOWER SURFACE CORROSION FS 998 - 1007. REPAIRED RT KEEL BEAM IAW REA B653-61424-MR. SDR INFO, CRACKED, CORRODED L2, PN 145T8611, SN NSN, PART NAME KEEL BEAM, FS & BS LOCATION ON ACFT RT 998 TO 1007. ACFT WAS GNDED. - [SDR ABXA20150219030](https://openairdocs.org/sdr/ABXA20150219030.md): Beam · corroded · Feb 19, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous Structure > CORROSION FOUND ON FIXED LE STRUCTURE AT APPROX LE STATION 894 AT SCREW HOLE. REMOVED NOSE BEAM WEB ASSEMBLY, FABRICATED NEW WEB & REINSTALLED ASSEMBLY WITH NEW WEB IAW SRM 51-40-02 & DWG 114T2300. SDR INFO, CORRODED L2, PN 114T2300-39, SN NSN, PART NAME NOS - [SDR ABXA20150219024](https://openairdocs.org/sdr/ABXA20150219024.md): Rib · corroded · Feb 19, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 325 UPPER CHORD OF THE TE RIB IS CORRODED. REPLACED UPPER T CHORD FITTING ON LT HORIZONTAL STATION 325. PN 183T1530-5AX IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 183T1530-5AX, SN NSN, PART NAME UPPER CHORD, FS - [SDR ABXA20150217019](https://openairdocs.org/sdr/ABXA20150217019.md): Beam · corroded · Feb 17, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous Structure > HYDRAULIC LINE SUPPORT CLIP OTBD & AFT OF TOP OF LG CORRODED ON TE SUPPORT. REMOVED CLIP, FOUND BEAM TO BE CORRODED. REPLACED BEAM, REINSTALLED CLIP IAW SRM 51-40-02 & DWG 113T1633. SDR INFO, CORRODED LEVEL 2, PN 113T1633-217, PART NAME BEAM, SN NSN, STRING - [SDR ABXA20150217018](https://openairdocs.org/sdr/ABXA20150217018.md): Angle · corroded · Feb 17, 2015 · N788AX · Boeing 767281 · Fuselage Main, Keel > LEFT FWD KEEL BEAM FWD STATION 977, LBL 2 CORROSION FOUND, MARKED WITH NR. FOUND ANGLE AT STATION 977, LBL 2 TO BE CORRODED BEYOND LIMITS IAW SRM 53-50-12 FIG 101. R & R ANGLE IAW SRM 51-40-02. SDR INFO, CORRODED LEVEL 2, PN 145T8604-2, PART NAME ANGLE, SN - [SDR ABXA20150209005](https://openairdocs.org/sdr/ABXA20150209005.md): Beam · corroded · Feb 9, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous Structure > CORROSION AROUND NUTPLATE AT APPROX LES 620. R & R WEB IAW SRM 51-40-02. SDR INFO, CORRODED, PN 114T2300-225, SN N/A, PART NAME NOSE BEAM. ACFT WAS GNDED. - [SDR ABXA20150206006](https://openairdocs.org/sdr/ABXA20150206006.md): Spar · corroded · Feb 6, 2015 · N788AX · Boeing 767281 · Wing Spar > CORROSION AROUND NUTPLATES ON REAR SPAR TO TE BEAM UPPER CHORD AT WS 433 NEAR TE. R & R UPPER CHORD WS 433 REAR SPAR TO TE IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 113T1510-33, SN NSN, PART NAME CHORD, AILERON SUPP STRINGER & WS LOCATION ON ACFT WS 433. - [SDR ABXA2014041046](https://openairdocs.org/sdr/ABXA2014041046.md): Unknown · fumes · Apr 8, 2014 · N788AX · Boeing 767200 · Air Distribution System > ON TOP OF DESCENT, THE FLIGHT CREW COULD SMELL ELEC FUMES. COMPLIED WITH SMOKE, FIRE, & FUMES CHECKLIST & FUMES CEASED. INSPECTED THE MAIN EQUIPMENT CTR, FWD EQUIPMENT COMPARTMENT, GALLEY AREA, HOT CUP, LAVATORY & RT AIR PACK, NO DEFECTS WERE FOUND. OPERATE - [SDR ABXA20130516434](https://openairdocs.org/sdr/ABXA20130516434.md): Angle · damaged · May 16, 2013 · N788AX · Boeing 767281 · Fuselage Miscellaneous Structure > FUSELAGE SKIN AT LT HORIZONTAL ANGLE, BS 1809, S12L HAS DEFECT INDICATION IN LOWER FWD FASTENER OF INSPECTED AREA 1 IAW NDTM PART 6, FIG 1. FASTENER OBLONG, REAMED TO.341" ON EXTERIOR RUB STRIP CUT OUT LOCATION. FASTENER DOUBLER REPAIRED IAW ENGINEERING REA - [SDR ABXA20130514436](https://openairdocs.org/sdr/ABXA20130514436.md): Skin · corroded · May 14, 2013 · N788AX · Boeing 767281 · Fuselage Main, Plate/Skin > RIGHT SIDE EMERGENCY EXIT DOOR CUTOUT FOUND WITH CORROSION IN THE FORWARD LOWER CORNER AREA APPROX. 2" LONG. REMOVED CORROSION IN RT SIDE EMERENCY EXIT CUTOUT FORWARD LOWER CORNER AREA. IAW REAB653-60542, ACFT WAS GROUNDED. - [SDR ABXA20130506432](https://openairdocs.org/sdr/ABXA20130506432.md): Mount · corroded · May 6, 2013 · N788AX · Boeing 767281 · Engine Mount Section > NR 2 ENGINE AFT MOUNT HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED ENGINE MOUNT IAW B767 MM CH 71-21-02-4, ACFT WAS GROUNDED. - [SDR ABXA20130503435](https://openairdocs.org/sdr/ABXA20130503435.md): Stiffener · corroded · May 3, 2013 · N788AX · Boeing 767281 · Fuselage Miscellaneous Structure > STIFFENER BETWEEN KEELBEAM PANELS CORRODED ON BOTH ENDS, STIFFENER CORRODED BEYOND LIMITS, R & R IAW SRM 51-40-02, PARA 4B AND 51-40-0, ACFT WAS GROUNDED. - [SDR ABXA20130501433](https://openairdocs.org/sdr/ABXA20130501433.md): Mount · corroded · May 1, 2013 · N788AX · Boeing 767281 · Engine Mount Section > NR 1 ENGINE AFT ENGINE MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED AFT ENGINE MOUNT IAW B767 AMM 71-21-02-4, ACFT WAS GROUNDED. - [SDR ABXA20121129311](https://openairdocs.org/sdr/ABXA20121129311.md): Inertia Reel · unsecure · Nov 29, 2012 · N788AX · Boeing 767281 · Emergency Equipment > EMERGENCY ESCAPE DEVICE (INTERTIAL REEL) FELL OUT OF HOLDER DURING FLIGHT. REPLACED DESCENT DEVICES IN SUPERNUMERARY COMPARTMENT CONTAINER AT POS 7 IAW AMM 25-61-03-04, ACFT WAS GROUNDED. Next page: https://openairdocs.org/deregistered/N788AX-2018-11-15/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 = 'N788AX' AND deregistration_id = 'N788AX-2018-11-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N788AX-2018-11-15/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.