# Service difficulty reports: N794AX, cancelled Apr 8, 2024

A list on [N794AX, cancelled Apr 8, 2024](https://openairdocs.org/deregistered/N794AX-2024-04-08.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 · 93 reports

- [SDR ABXA20171127141](https://openairdocs.org/sdr/ABXA20171127141.md): Sensor · malfunctioned · Nov 27, 2017 · N794AX · Boeing 767281 · Fuel Controlling System
  > PASSING THROUGH FLIGHT LEVEL 230, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. THE CREW COULD NOT RESTORE NORMAL ENGINE OPERATION VIA THE QUICK REFERENCE HANDBOOK PROCEDURES. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE RIGHT ENGINE'S MAIN ENGINE CONTROL
- [SDR ABXA20171124140](https://openairdocs.org/sdr/ABXA20171124140.md): Stator Vane · out of adjust · Nov 24, 2017 · N794AX · Boeing 767281 · Turbine Engine Air Inlet Section
  > DURING CLIMB THROUGH FLIGHT LEVEL 200, THREE LOUD BANGS OCCURRED THAT JOLTED THE AIRCRAFT. THE AIRPLANE SEEMED TO YAW EACH TIME. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE LEFT ENGINE'S VARIABLE STATOR VANE SYST
- [SDR ABXA20171122139](https://openairdocs.org/sdr/ABXA20171122139.md): Compressor · stalled · Nov 22, 2017 · N794AX · Boeing 767281 · Turbine Engine Compressor Section
  > RIGHT ENGINE HAD A COMPRESSOR STALL. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE FAULT ISOLATION MANUAL DIAGRAM 71-05, FAULT TREE 808 WAS ACCOMPLISHED. ALL FINDINGS WERE WITHIN LIMITS. THE CAUSE OF THE COMPRESSOR STALL IS UNKNOWN.
- [SDR ABXA20171121138](https://openairdocs.org/sdr/ABXA20171121138.md): Tee Fitting · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION ON THE ATTACH TEE AT THE REAR SPAR/UPPER RIB INTERSECTION OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121137](https://openairdocs.org/sdr/ABXA20171121137.md): Rib · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION ON UPPER RIB CHORD OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121135](https://openairdocs.org/sdr/ABXA20171121135.md): Floorbeam · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Fuselage Main, Floor Beam
  > CORROSION ON THE FORWARD SIDE OF THE FLOOR BEAM CHORD AT FUSELAGE STATION 1109, LBL 46, IN THE AFT LOWER CARGO COMPARTMENT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121134](https://openairdocs.org/sdr/ABXA20171121134.md): Tee Fitting · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, RBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121133](https://openairdocs.org/sdr/ABXA20171121133.md): Tee Fitting · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, LBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121132](https://openairdocs.org/sdr/ABXA20171121132.md): Stringer · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 32L AT FUSELAGE STATION 434. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121131](https://openairdocs.org/sdr/ABXA20171121131.md): Rib · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Wing, Rib/Bulkhead
  > CORROSION IN RIGHT LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121130](https://openairdocs.org/sdr/ABXA20171121130.md): Rib · cracked · Nov 21, 2017 · N794AX · Boeing 767281 · Wing, Rib/Bulkhead
  > CRACK IN RIGHT WING NOSE RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121129](https://openairdocs.org/sdr/ABXA20171121129.md): Rib · corroded · Nov 21, 2017 · N794AX · Boeing 767281 · Wing, Rib/Bulkhead
  > CORRODED NUT PLATES ON THE RIGHT WING LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121128](https://openairdocs.org/sdr/ABXA20171121128.md): Stringer · cracked · Nov 21, 2017 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > CRACK IN STRINGER 5L AT SPLICE. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121127](https://openairdocs.org/sdr/ABXA20171121127.md): Fitting · cracked · Nov 21, 2017 · N794AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CRACK IN FRAME TO STRINGER ATTACH CLIP AT STA 1702. THE ATTACH CLIP WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170830095](https://openairdocs.org/sdr/ABXA20170830095.md): Carabiner · missing · Aug 30, 2017 · N794AX · Boeing 767281 · Emergency Equipment
  > TWO EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), TWO NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS UNKNO
- [SDR ABXA20170513063](https://openairdocs.org/sdr/ABXA20170513063.md): Wire · shorted · May 13, 2017 · N794AX · Boeing 767281 · Engine Exhaust System Wiring
  > DURING TAXI, EICAS MESSAGE FOR THE LT REVERSER ISOLATION VALVE DISPLAYED AND THE THRUST REVERSER INDICATION CIRCUIT BREAKER TRIPPED OPEN. THE AIRPLANE WAS REMOVED FROM SERVICE. THE CAUSE OF THE EICAS MESSAGE AND TRIPPED CIRCUIT BREAKER WAS WIRE W756-503-24 WA
- [SDR ABXA20160506088](https://openairdocs.org/sdr/ABXA20160506088.md): Failsafe · cracked · May 6, 2016 · N794AX · Boeing 767281 · Fuselage Main, Frame
  > LOWER FASTENER HOLE IN RT FAILSAFE COMMON TO T FITTING IS CRACKED, VERIFIED BY HFEC HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUMENT 47008ORD04, THAT IS ATTACHED TO JC EA 53500014-003 FOR WORK STEPS TAKEN. CRACKED LENGTH.125",
- [SDR ABXA20160505089](https://openairdocs.org/sdr/ABXA20160505089.md): Failsafe · cracked · May 5, 2016 · N794AX · Boeing 767281 · Fuselage Main, Frame
  > LEFT FAILSAFE LOWER HOLE COMMON TO T FITTING HAS CRACK INDICATION, VERIFIED BY HFEC ROTARY HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUMENT 47008ORD03, THAT IS ATTACHED TO JC EA 53500013-003 FOR WORK STEPS TAKEN. CRACKED LENGTH
- [SDR ABXA20151209201](https://openairdocs.org/sdr/ABXA20151209201.md): Fitting · corroded · Dec 9, 2015 · N794AX · Boeing 767281 · Cargo/Baggage Doors
  > NUMBER 9, COUNTED FROM FRONT, MAIN DECK CARGO DOOR LATCH CAM PIN FITTING HAS CORROSION IN THE BORE. REMOVED, REPAIRED & RE-INSTALLED NR 9 LATCH PIN & LATCH PIN FITTING IAW REA B652-61882-MR & AMM SUPP 52-32-00. SDR INFO, CORRODED LEVEL 2, PN 368-53-00-95347-
- [SDR ABXA20151208199](https://openairdocs.org/sdr/ABXA20151208199.md): Skin · corroded · Dec 8, 2015 · N794AX · Boeing 767281 · Wing, Plate/Skin
  > SUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 912. REMOVED PANELS, REMOVED CORROSION & NDT INSPECTED. PERFORMED REPAIR ON REA B657-61824-MR. REINSTALLED PANELS IAW SRM 51-40-02 & REA B657-61824-MR. TOUCH UP PAINT TO BE DONE ON NR 1241. DANGER TAG REMOV
- [SDR ABXA20151208198](https://openairdocs.org/sdr/ABXA20151208198.md): Skin · corroded · Dec 8, 2015 · N794AX · Boeing 767281 · Wing, Plate/Skin
  > SUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 1025. REPAIRED CORRODED AREA ON RT WING AT REAR SPAR & WS 1030 IAW REA B657-61825-MR. REINSTALLED FIXED PANELS IAW SRM 51-40-02 & REA 657-61825. REPAIR AREA TO BE PAINTED ON NR 1241. FUEL PANEL 652BB TO BE L
- [SDR ABXA20151208196](https://openairdocs.org/sdr/ABXA20151208196.md): Skin · corroded · Dec 8, 2015 · N794AX · Boeing 767281 · Wing, Plate/Skin
  > LEFT WING SURFACE CORRODED AFT OF OVERWING EXIT AT WING TO BODY FAIRING AT APPROX STATION 938. REMOVED CORROSION & REPAIRED AREA IAW REA B657-61841-MR. SDR INFORMATION, CORRODED LEVEL 2, PN 112T3229-11, SN N/A, PART NAME RIB CHORD, EXACT FS & BS LOCATION ON
- [SDR ABXA20151205204](https://openairdocs.org/sdr/ABXA20151205204.md): Bulkhead · cracked · Dec 5, 2015 · N794AX · Boeing 767281 · Fuselage Main, Bulkhead
  > MID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER TS4 & TS5, RS23, INBD OF APU SHROUD. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH.100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS23. ACFT WAS GNDED.
- [SDR ABXA20151205203](https://openairdocs.org/sdr/ABXA20151205203.md): Bulkhead · cracked · Dec 5, 2015 · N794AX · Boeing 767281 · Fuselage Main, Bulkhead
  > MID FREQUENT EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH.100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.
- [SDR ABXA20151205202](https://openairdocs.org/sdr/ABXA20151205202.md): Bulkhead · cracked · Dec 5, 2015 · N794AX · Boeing 767281 · Fuselage Main, Bulkhead
  > MID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH.100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.
- [SDR ABXA20151203213](https://openairdocs.org/sdr/ABXA20151203213.md): Structure · cracked · Dec 3, 2015 · N794AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > LEFT 1809 FWD OUTER CHORD INBD FLANGE AT OTBD FASTENER BELOW SPLICE FITTING CRACKED APPROX 1.5". HFEC VERIFIED IAW NDTM PART 6 51-00-19. REMOVED & REINSTALLED ANGLES & ATTACH BRACKETS TO FACILITATE REPLACEMENT OF LT 1809 OUTER CHORD IAW SRM 51-40-02 PARA 7D
- [SDR ABXA20151203197](https://openairdocs.org/sdr/ABXA20151203197.md): Skin · corroded · Dec 3, 2015 · N794AX · Boeing 767281 · Wing, Plate/Skin
  > CORROSION SUSPECTED AT LT WING REAR SPAR WS 854. BLEND OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA 657-61837-MR, WS 810-815. BLEND OUT & TRIM OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA B657-61838-MR, WS 850 - 859. SDR INFORMATION CORRODED LEVEL
- [SDR ABXA20151202215](https://openairdocs.org/sdr/ABXA20151202215.md): Support Beam · corroded · Dec 2, 2015 · N794AX · Boeing 767281 · Wing Miscellaneous Structure
  > RIGHT WING TE UPPER PANEL SUPPORT AT WS 1052 IS CORRODED. REMOVED CORRODED PANEL SUPPORT BEAM & INSTALLED NEW FABRICATED BEAM REV NO 61536-0000-0005 & REA NO B657-61840 IAW SRM 51-40-02 GENERAL PG 7 PARA 70. CORRODED LEVEL 2, PN 113T1913024, PART NAME PANEL
- [SDR ABXA20151130214](https://openairdocs.org/sdr/ABXA20151130214.md): Skin Panel · corroded · Nov 30, 2015 · N794AX · Boeing 767281 · Wing, Plate/Skin
  > RIGHT WING SKIN UPPER TE IS CORRODED UNDER PANEL 113T1651 AT WS 512 - 521. CORROSION UNDER UPPER WING TRAILING EDGE PANEL WAS REPAIRED ON REA B657-61823-M. PANEL WAS REPAIRED ON NR-0468 & REINSTALLED ON NR-0682. CORRODED LEVEL 2, PN 112T3101-6, PART NAME SK
- [SDR ABXA20151127216](https://openairdocs.org/sdr/ABXA20151127216.md): Support · corroded · Nov 27, 2015 · N794AX · Boeing 767281 · Ailerons
  > RIGHT WING TE OTBD AILERON, HINGE SUPPORT RIB AT WS 1079.95 HAS CORROSION ON THE UPPER CHORD OF THE SUPPORT ASSEMBLY. REMOVED CORRODED CHORD & REPLACED WITH NEW FABRICATED UPPER CHORD REF REA B657-51827, IAW SRM 51-40-02 PG 2 PARA 4B & 51-40-02 PG 7 PARA 7D.
- [SDR ABXA20151125211](https://openairdocs.org/sdr/ABXA20151125211.md): Stringer · cracked · Nov 25, 2015 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > UPPER CARGO STRINGER 19L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 19L, STATION 698 - 720 IAW ENGINEERING SKETCH NO ESO2821 REV A & 767 - 200 SRM 53-00-03 REPAIR 1 DETAIL II. CRACKED 0.5", SN N/A, PART NAME STRINGER, EXACT FS & BS
- [SDR ABXA20151125194](https://openairdocs.org/sdr/ABXA20151125194.md): Bracket · cracked · Nov 25, 2015 · N794AX · Boeing 767281 · Leading Edge Devices
  > NUMBER 6 SLAT LOWER TE ATTACH ANGLE, OUTBOARD OF CTR AUX TRACK, IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION, CRACKED, LENGTH.250, PN 14T3166Y111, SN N/A, PART NAME BRACKET, EXACT FS & BS LOCATION A
- [SDR ABXA20151125193](https://openairdocs.org/sdr/ABXA20151125193.md): Attach Angle · cracked · Nov 25, 2015 · N794AX · Boeing 767281 · Leading Edge Devices
  > NUMBER 6 SLAT LOWER TE ATTACH ANGLE, LOCATED OUTBOARD OF OUTBOARD AUX TRACK IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION CRACKED LENGTH.250, PN 114T3166-71, SN N/A, PART NAME ANGLE, EXACT FS & BS LO
- [SDR ABXA20151118210](https://openairdocs.org/sdr/ABXA20151118210.md): Stringer · cracked · Nov 18, 2015 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > UPPER CARGO STRINGER 17L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. CONTACT ENGINEERING FOR REPAIR. REPAIRED CRACKED LONGERON STRINGER 17L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, SN
- [SDR ABXA20151118209](https://openairdocs.org/sdr/ABXA20151118209.md): Stringer · cracked · Nov 18, 2015 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > UPPER CARGO STRINGER 7L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED CRACKED LONGERON STRINGER 7L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES 02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, PART NAME STRINGER, SN N/A, EXACT FS
- [SDR ABXA20151117205](https://openairdocs.org/sdr/ABXA20151117205.md): Channel · corroded · Nov 17, 2015 · N794AX · Boeing 767281 · Wing Miscellaneous Structure
  > WING TE PANEL ATTACH LOWER CHANNEL SPLIT ON EDGE AT TE WS 936. REMOVED DAMAGED CHANNEL, NEW CHANNEL FABRICATED REA B657-61805 & INSTALLED NEW CHANNEL IAW SRM 51-40-02 & REA B657-61805. CORRODED LEVEL 2, PN 113T1912-3, PART NAME CHORD CHANNEL, SN NSN, FS & BS
- [SDR ABXA20151113212](https://openairdocs.org/sdr/ABXA20151113212.md): Stringer · cracked · Nov 13, 2015 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 21L AT FS. 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED 4.75", EXACT FS & BS LOC ON ACF
- [SDR ABXA20151111208](https://openairdocs.org/sdr/ABXA20151111208.md): Stringer · cracked · Nov 11, 2015 · N794AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE, CONTACT ENGINEERING FOR REPAIR. REPAIRED STRINGER 21L AT FS 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED
- [SDR ABXA20151111206](https://openairdocs.org/sdr/ABXA20151111206.md): Support · corroded · Nov 11, 2015 · N794AX · Boeing 767281 · Wing Miscellaneous Structure
  > AT OPENING ABOVE LT LG, AFT WING PANEL ATTACH BEAM CORRODED AROUND NUTPLATE. REMOVED CORRODED PANEL ATTACH BEAM, DRILLED FOR LOCATION & INSTALLED IAW SRM 51-40-05 TABLE 3 & 51-40-02-7. CORRODED LEVEL 2, PN 113T1632-197, SN N/A, PART NAME RIB TE PANEL SUPPORT
- [SDR ABXA20151111195](https://openairdocs.org/sdr/ABXA20151111195.md): Structure · corroded · Nov 11, 2015 · N794AX · Boeing 767281 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STABILIZER S10 UPPER AFT FLANGE AT RIB 2R OUTBOARD CORROSION. BLENDED AREA WITHIN LIMITS TO REMOVE CORROSION IAW SRM 51-10-02. SDR INFO, CORRODED LEVEL 2, STRINGER & WS LOCATION, FROM STRINGER 10 TO RIB 2R. ACFT WAS GNDED.
- [SDR ABXA20151110207](https://openairdocs.org/sdr/ABXA20151110207.md): Beam · cracked · Nov 10, 2015 · N794AX · Boeing 767281 · Nacelle/Pylon, Main Frame
  > NUMBER TWO STRUT INTERIOR STRUCTURE IS CRACKED WHERE PANEL 447ERX ATTACHES AT LOWER EDGE. R & R NR 2 PYLON HYD BAY OTBD BEAM WHERE PANEL 447ERX ATTACHES IAW SRM 51-40-02. CRACKED 1.0", PN 313T1380-242, PART NAME BEAM, AFT FAIRING OTBD, SN NSN, STRINGER & WS
- [SDR ABXA20151103200](https://openairdocs.org/sdr/ABXA20151103200.md): Keelbeam · corroded · Nov 3, 2015 · N794AX · Boeing 767281 · Fuselage Main, Keel
  > CORROSION FOUND ON LT LOWER KEEL CHORD STATION 952. CLEANED UP CORROSION ON LT LOWER KEEL CORD AT FS 952 IAW SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101. CORROSION IS WITHIN ALLOWABLE LIMITS. SDR INFO, CORRODED LEVEL 2, PN 145T8610-5005, PART NAME KEEL CORD, SN
- [SDR ABXA20150201002](https://openairdocs.org/sdr/ABXA20150201002.md): Switch · out of tolerance · Feb 1, 2015 · N794AX · Boeing 767281 · Door Warning System
  > MAIN CARGO DOOR LIGHT & SIREN ILLUMINATED DURING CLIMB OUT AT APPROXIMATELY 2.0 TO 2.1 PSID. INDICATION SWITCHES GAP ADJUSTED TO TOLERANCE & E1-1 BURNDY BLOCK CLEANED. WORN DOOR MECHANISM CAUSING SWITCH GAP TO FALL OUT OF TOLERANCE.
- [SDR ABXA2014021423](https://openairdocs.org/sdr/ABXA2014021423.md): Support · corroded · Feb 14, 2014 · N794AX · Boeing 767281 · Wing Miscellaneous Structure
  > HINGED PANEL 651TB OTBD LOWER PANEL ATTACH CHANNEL SPLIT ON EDGE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED BEAM, REPAIRED IAW REA B657-60865, PN 113T1623-40, SN N/A, PART NAME UPPER SUPPORT, LOCATION RTW WS 358 AFT OF REAR SPAR. ACFT WAS GROUNDED
- [SDR ABXA2014021422](https://openairdocs.org/sdr/ABXA2014021422.md): Structure · corroded · Feb 14, 2014 · N794AX · Boeing 767281 · Wing Miscellaneous Structure
  > TRAILING EDGE PANEL 652HB AFT ATTACH BEAM LOWER CHORD SPLIT ON EDGE. REPLACED LOWER CORD AT PANEL 652HB AFT ATTACH IAW SRM 51-40-02 PER 4 & 7. SDR INFO CORRODED, PN 113T1407-2, SN N/A, PART NAME CHORD LOWER, FUSELAGE & BODY STATION, LOCATION FROM WS 412 TO W
- [SDR ABXA2014021421](https://openairdocs.org/sdr/ABXA2014021421.md): Beam · corroded · Feb 14, 2014 · N794AX · Boeing 767281 · Wing Spar
  > REAR SPAR TO TE PANEL ATTACH BEAM SPLIT ON INBD SIDE LOWER CHORD AT STATION 257, 20 INCHES FROM REAR SPAR. REPLACED REAR SPAR TO TE PANEL ATTACH BEAM IAW SRM 51-40-02. SDR INFO CORRODED, PN 113T1622-9, SN N/A, PART NAME CHORD, BEAM LOWER, STRINGER & WING STA
- [SDR ABXA2014021324](https://openairdocs.org/sdr/ABXA2014021324.md): Skin · corroded · Feb 13, 2014 · N794AX · Boeing 767281 · Wing, Plate/Skin
  > RIGHT WING TRAILING UPPER WING SKIN IS CORRODED 40 INCHES OTBD OF FUSE AT FWD EDGE OF PANEL 651 FT. BLENDED CORROSION AS DESCRIBED IAW SRM 51-20-01, AREA BLENDED IS WITHIN LIMITS IAW ENGINEERING DISPOSITION ON ENTRY NR 8. UPSIZED TWO FASTENER HOLES COMMON TO
- [SDR ABXA2014021225](https://openairdocs.org/sdr/ABXA2014021225.md): Support Beam · corroded · Feb 12, 2014 · N794AX · Boeing 767281 · Spoilers
  > LEFT WING UPPER SURFACE, BULGE IN PANEL JUST FWD OF NR 5 SPOILER CTR OTBD FITTING. FOUND SPOILER SUPPORT BEAM TO BE CORRODED BEYOND LIMITS. FABRICATED NEW BEAN PN 654T0391-3 IAW REA B657-60857-MR & REPAIRED NEW BEAM IAW REA B657-60862-MR. INSTALLED BEAM IA
- [SDR ABXA2014021220](https://openairdocs.org/sdr/ABXA2014021220.md): Former · cracked · Feb 12, 2014 · N794AX · Boeing 767281 · Wing Spar
  > RIGHT WING LE NOSE BEAM FORMER IS CRACKED AT THE NR 8 SLAT INBD AUXILIARY TRACK INBD SIDE. REMOVED DAMAGED NOSE FORMER & INSTALLED NON-NOSE FORMER IAW SRM 51-40-02. SDR INFO CRACKED.750 INCHES, PN 114T2200-6, SN NSN, PART NAME FORMER, NOSE BEAM, LOCATION OS
- [SDR ABXA2014021216](https://openairdocs.org/sdr/ABXA2014021216.md): Angle · corroded · Feb 12, 2014 · N794AX · Boeing 767281 · Fuselage, Landing Gear Attach Fittings
  > CORROSION FOUND BETWEEN STATION 999 & STATION 1021 IN LT WW BEHIND MAIN GEAR DOOR ACTUATOR ON CTR BEAM. CLEANED LT WW BEHIND MLG DOOR ACTUATOR FS 999 - 1021, FOUND ANGLE PN 145T8601Y37 CORRODED. REPLACED IT WITH A NEW PART IAW SRM 51-40-02 PARA 7. SDR INFO

Next page: https://openairdocs.org/deregistered/N794AX-2024-04-08/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 = 'N794AX' AND deregistration_id = 'N794AX-2024-04-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N794AX-2024-04-08/reports

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