# Service difficulty reports: N795AX, cancelled Apr 9, 2024

A list on [N795AX, cancelled Apr 9, 2024](https://openairdocs.org/deregistered/N795AX-2024-04-09.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 3 · 120 reports

- [SDR ABXA202210132110](https://openairdocs.org/sdr/ABXA202210132110.md): Fmc · malfunctioned · Oct 12, 2022 · N795AX · Boeing 767281 · Flight Management Computing Hardware System
  > AFTER LEFT ENG START, LEFT FMC WENT FULL BRIGHT WHICH CAUSED AND OVERLAY OF LINES. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE LEFT CDU IAW MEL 34-61-1-1A. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED. AIRCRAFT RETU
- [SDR ABXA2022082283](https://openairdocs.org/sdr/ABXA2022082283.md): Outflow Valve · faulted · Aug 22, 2022 · N795AX · Boeing 767281 · Pressure Regulator/Outflow Valve
  > LOSS OF ALL CABIN PRESSURIZATION CONTROL @ FL 360 MX PAGE SHOWED AUTO 1/AUTO2 INOP. HI FLOW /EICAS SHOWED CABIN ALT MASTER WARNING CABIN AUTO INOP MASTER CAUTION. CREW ELECTED TO AIR TURNBACK TO DEN, MAINTENANCE GROUNDED AIRCRAFT. MAINYENANCE T/S PER 767FIM 21
- [SDR ABXA2022080591](https://openairdocs.org/sdr/ABXA2022080591.md): Warning Message · false activation · Aug 5, 2022 · N795AX · Boeing 767281 · Hydraulic Pump (Electric/Engine), Main
  > AFTER START R HD DEMAND PUMP EICAS MSG. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CK OF RH ACMP & RH ENG DRIVEN HYD PUMPS WITH & WITH-OUT ENG RUNNING IAW B767 AMM 29-11-00. ALL OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR 2022FA0000302](https://openairdocs.org/sdr/2022FA0000302.md): None · none · Jun 19, 2022 · N795AX · Boeing 767281 · AC Generation System
  > L GEN DRIVE, L GEN "OFF" EICAS MESSAGE. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. PERFORMED BPCU BITE IAW B767 FIM 24-20 FAULT TREE 01 AND TASK 24-20 804. RECONNECTED IDG AND RAN ENG. COULD NOT DUPLICATE NO FAULTS FOUND. PLACARD REMOVED. MX PROC C/W. AIRCRAFT
- [SDR ABXA2022022528](https://openairdocs.org/sdr/ABXA2022022528.md): Duct · cracked · Feb 25, 2022 · N795AX · Boeing 767281 · Cabin Pressure Control System
  > LEFT PACK WILL NOT HOLD CABIN ALTITUDE BELOW 10000'. AT FL 340, CABIN ALTITUDE ALARM SOUNDED. CABIN RETURNED TO AN ALTITUDE BELOW 10000' AT FLT 280. CREW ELECTED TO DO AN AIR TURNBACK. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENA
- [SDR ABXA2022012818](https://openairdocs.org/sdr/ABXA2022012818.md): Not Reported · not reported · Jan 28, 2022 · N795AX · Boeing 767281 · Cabin Cooling System
  > R PACK TEMP" ICAS MESSAGE AFTER BLOCK OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. BITE R PACK CONTROL PANEL CONTROL PANEL, NO FAULT SHOW ON CURRENT OR PREVIOUS FAULTS, RUN R PACK ONE HOUR ALL TEMP ARE NORMAL. OPS CHECKED GOOD IAW B767 MM 21-51-00.
- [SDR ABXA2022012700615](https://openairdocs.org/sdr/ABXA2022012700615.md): Pump · intermittent · Jan 26, 2022 · N795AX · Boeing 767281 · Hydraulic Pump (Electric/Engine), Main
  > L HYD PRIM PUMP EICAS MSG" EICAS MESSAGE AND LEFT ENGINE DRIVEN PRIMARY PUMP "PRESS LIGHT ILLUMINATED. AICRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE.REMOVED AND REPLACED #1 ENGINE EDP IAW AMM CHP 29 -11-05. LEAK CHECK GOOD. PERF - PWR CHK AT L ENG HYD
- [SDR ABXA2022010602](https://openairdocs.org/sdr/ABXA2022010602.md): Relay · sticking · Jan 6, 2022 · N795AX · Boeing 767281 · Ice/Rain Protection System
  > L AOA PROB EICAS MESSAGE ON ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R/R RELAYS AT POS. K400 AND K644 I/A/W B767 WDM, CH.30-32-11. PERFORMED TEST OF AOA PROBE HEAT I/A/W B767 AMM, CH. 30-32-00. OPS CHECK GOOD.AIRCRAFT RETURN
- [SDR ABXA20211119121](https://openairdocs.org/sdr/ABXA20211119121.md): Cable · binding · Nov 19, 2021 · N795AX · Boeing 767281 · Compressor Bleed Control
  > LT ENG COMPRESSOR STALL (MODERATE) ALL ENG INDICATIONS NORMAL IN CLIMB THROUGH 35000'. FLIGHT CREW ELECTED TO DIVERT TO CVG. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND VSV CABLE BINDING.REMOVED OLD, THEN INSTALLED NEW L/H ENGINE VSV CABLE PER AMM
- [SDR ABXA20211011099](https://openairdocs.org/sdr/ABXA20211011099.md): Transmitter · faulty · Oct 12, 2021 · N795AX · Boeing 767281 · Trailing Flap Position Indicating System
  > AFTER TAKEOFF DURING CLIMB THE FOLLOWING LIGHTS ILLUMINATED; AMBER TE FLAP DISAGREE EICAS AMBER TRAILING EDGE DISCREET LIGHT PERFORMED NON-NORMAL PROCEDURE FOR TE FLAP DISAGREE AND LANDED BACK IN KILN WITH FLAPS 20 THE LIGHTS BEGAN ILLUMINATING WHILE FLAPS R
- [SDR ABXA202193087](https://openairdocs.org/sdr/ABXA202193087.md): Transmitter · faulted · Sep 3, 2021 · N795AX · Boeing 767281 · Elevator Control System
  > DURING CONTROL CHECK, RIGHT ELEVATOR FAILED TO MOVE FROM NEUTRAL POSITION. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE VERIFIED MOVEMENT OF RH ELEVATOR AND POSITION TRANSMITTER WAS AT FAULT.R/H POSITION INDICATOR DEFERRED IAW MEL 27-08-1. A
- [SDR ABXA202108053070](https://openairdocs.org/sdr/ABXA202108053070.md): Control Valve · intermittent · Aug 3, 2021 · N795AX · Boeing 767281 · Cabin Temperature Control System
  > CABIN ALT & CABIN ALTITUDE LIGHTS ILLUMINATED. EICAS MESSAGE CABIN ALTITUDE WAS DISPLAYED. UNABLE TO RESTORE CABIN PRESS. USING MANUAL MODE. DESCENDED TO FL 280 LIGHT WENT OUT. OXYGEN WAS USED. AICRAFT CONTINUED TO SCHEDULED ARRIVAL AIPORT. AIRCRAFT WAS GROUN
- [SDR ABXA2021710065](https://openairdocs.org/sdr/ABXA2021710065.md): Start Valve · faulted · Jul 10, 2021 · N795AX · Boeing 767281 · Engine Start Valves/Controls
  > DURING L ENG START, L ENG STARTER EICAS MSG. NO N2 ROTATION. AIRCRAFT RETURNED TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED #1 ENG. START VALVE IAW B767 AMM 80-11-02. AIRCRAFT RELEASED FOR FLIGHT
- [SDR ABXA2021619058](https://openairdocs.org/sdr/ABXA2021619058.md): Unknown · unknown · Jun 19, 2021 · N795AX · Boeing 767281 · Landing Gear Steering System
  > UPON ENTERING RUNWAY MAKING LEFT TURN NWS MAKING GRINDING SOUNDS AND BURNING RUBBER SMELLED. AIRCRAFT BTB. MAINTENANCE GROUNDED AIRCRAFT.INSPECTED NOSE WHEEL STEERING SYSTEM. NO FAULTS NOTED. GREASED STEERING ACTUATORS AND TORQUE LINKS IAW AMM 32-51-00. AIRCRA
- [SDR ABXA2021528054](https://openairdocs.org/sdr/ABXA2021528054.md): Shutoff Valve · leaking · May 27, 2021 · N795AX · Boeing 767281 · Hydraulic Power Accumulator, Main
  > THE CENTER HYDRAULIC QUANTITY EICAS MESSAGE DISPLAYED INDICATION. AN IN FLIGHT EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY WITH NO OTHER PROBLEMS. AIRCRAFT WAS THEN GROUNDED BY MAINTENANCE. A HYDRAULIC LEAK WAS FOUND ON THE CENTER FLAP/SLAT SHUT OFF VAL
- [SDR ABXA2021425028](https://openairdocs.org/sdr/ABXA2021425028.md): Warning Light · illuminated · Apr 25, 2021 · N795AX · Boeing 767281 · Cabin Cooling System
  > L PACK TEMP EICAS MESSAGE ON TAXI OUT. ACCOMPLISHED QRH PROCEDURE. AFTER 5 MINUTES IN STBY N PACK INOP LIGHT REMAINED ILLUMINATED. AIRCRAFT BACK TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. LEFT PACK DEFERRED. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021331020](https://openairdocs.org/sdr/ABXA2021331020.md): Door · unlatched · Mar 31, 2021 · N795AX · Boeing 767281 · Cargo/Baggage Doors
  > AFTER TAKE OFF, MX CARGO DOOR LIGHT ILLUMINATED.AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO ORIGIN. AIRCRAFT WAS GROUNDED BY MAINTENANCE. FOUND THE MCD DOOR DOOR NOT LATCHED LIGHT ON. OPERATED THE UNLOCK SWITCH UP, UNLOCKED DOOR AND POSITIONED THE CLOSED SW
- [SDR ABXA2021228017](https://openairdocs.org/sdr/ABXA2021228017.md): Pca · leaking · Feb 28, 2021 · N795AX · Boeing 767281 · Drag Control System
  > L HYD QTY LOW EICAS MSG,FLIGHT CREW DECLARED AN EMERGENCY AND EXECUTED AN AIR TURN BACK AND LANDED UNEVENTFULLY. MAINTENANCE DETERMINED #1 SPOILER WAS LEAKING HYDRAULIC FLUID AND AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED #1 SPOILER PCA OPS CHECK/RIG CHECK GO
- [SDR ABXA2021223016](https://openairdocs.org/sdr/ABXA2021223016.md): Fseu · faulted · Feb 23, 2021 · N795AX · Boeing 767281 · Trailing Edge Flap Control System
  > TE FLAPS DISAGREE CAUTION MESSAGE RAN THE QRH IN-FLIGHT. TRAILING EDGE DISCREET LIGHT. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED BY MAINTENANCE. BITE TESTED FSEU AS PER FIM 27-51 FT 809. EXTRACTED FAULT MSG NO. 27-51102 " L FLAP.STAB POS" PERFO
- [SDR ABXA20200803215](https://openairdocs.org/sdr/ABXA20200803215.md): Autothrottle Sys · malfunctioned · Nov 16, 2020 · N795AX · Boeing 767281 · Auto Throttle System
  > ON PUSH, AUTOTHROTTLES WENT INOPERABLE FOLLOWED BY LOSS OF THRUST SETTINGS BEING DELETED. WILL NOT TAKE ANY THRUST SETTINGS. AIRCRAFT BACK TO BLOCK. AIRCRAFT GROUNDED. ACCOMPLISHED OPERATIONS CHECK OF TMS DISPLAY AND TMC, REF AMM 22-31-01, C/W MCDP TESTS 0
- [SDR ABXA20200803210](https://openairdocs.org/sdr/ABXA20200803210.md): Line · leaking · Nov 7, 2020 · N795AX · Boeing 767281 · Hydraulic System, Main
  > ON TAXI OUT, LT HYDRAULIC SYSTEM LOW QTY EICAS MESSAGE IN VIEW STATUS PAGE SHOWS ZERO QTY. AICRAFT BACK TO BLOCK AND GROUNDED. UPON INSPECTION FOUND LEAKING RETURN LINE FROM EDP IN THE LT PYLON. REMOVED LINE, REPAIRED HYD LINE WITH RYNGLOK, REF B767 MM 20-1
- [SDR ABXA202009038169](https://openairdocs.org/sdr/ABXA202009038169.md): Seat Track · corroded · Aug 25, 2020 · N795AX · Boeing 767281 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS FOUND ON THE INBOARD FLANGE OF AFT LOWER CARGO COMPARTMENT SEAT TRACK (P/N: 96FS667842-107) AT STA 1307, RBL 15.01. THE DAMAGE WAS REMOVED BY BLENDING. ORIGINAL FLANGE THICKNESS IS.080 AND MINIMUM REMAINING THICKNESS IN THE BLENDED AREA IS.03
- [SDR ABXA20200903 172](https://openairdocs.org/sdr/ABXA20200903%20172.md): Panel · gouged · Aug 14, 2020 · N795AX · Boeing 767281 · Nacelle/Pylon, Main Frame
  > GOUGE DAMAGE WAS FOUND ON THE STRUT SKIN PANEL (P/N 311T1400-21) OF THE LT PYLON. THE GOUGE WAS REMOVED BY BLENDING, PER 767-200 SRM 51-10-02 EXCEEDING SRM LIMITS. ALL FASTENERS COMMON TO REWORKED AREAS, AS REQUIRED, WERE REMOVED AND HFEC OPEN-HOLE AND SURFA
- [SDR ABXA202009038173](https://openairdocs.org/sdr/ABXA202009038173.md): Support Fitting · corroded · Aug 13, 2020 · N795AX · Boeing 767281 · Wing Miscellaneous Structure
  > DURING AIRCRAFT C-CHECK AT TAMPA, AIRBORNE MAINTENANCE WAS REQUIRED TO INSPECT THE NR 8 FLAP SUPPORT 1-3 BEAM ASSEMBLY PER ABX WORK CARD ABX-57-796-28-02. INSPECTION REVEALED CORROSION WITHIN A HOLE LOCATION. THE SUBJECT HOLE WAS REWORKED TO A CLEAN AND ROUN
- [SDR ABXA20200803171](https://openairdocs.org/sdr/ABXA20200803171.md): Door Sill · corroded · Aug 13, 2020 · N795AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TPA), CORROSION WAS FOUND ON THE AFT LOWER CARGO DOOR CUTOUT LOWER SILL FAIL SAFE STRAP (P/N 146T8048-3), BETWEEN STA 1241 AND STA 1263 AT STRINGER S-33R. THE CORROSION WAS REMOVED AND EVALUATED PER 767-200 53-00-15
- [SDR ABXA202009038170](https://openairdocs.org/sdr/ABXA202009038170.md): Skin · corroded · Aug 6, 2020 · N795AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > WHILE PERFORMING THE SCRIBE LINE INSPECTION, PER ABX TASK CARD ABX-SCL-5330-0016-23145 REFERENCE AD 2010-06-16 AND BOEING SB 767-53A0193, CORROSION WAS FOUND ON THE FUSELAGE SKIN (P/N 146T3330-41 ASSY) IN ZONE A AT STRINGER S-17L BETWEEN STA 1395 AND STA 1417.
- [SDR ABXA2020062419070](https://openairdocs.org/sdr/ABXA2020062419070.md): Warning Message · illuminated · Jun 19, 2020 · N795AX · Boeing 767281 · Engine Starter
  > L ENG STARTER EICAS MESSAGE ILLUMINATED DURING ENGINE START. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20200603065](https://openairdocs.org/sdr/ABXA20200603065.md): Valve · malfunctioned · Jun 3, 2020 · N795AX · Boeing 767281 · Pneumatic Distribution System
  > LEFT BLEED AIR ISOLATION VALVE LIGHT STAYS ON. AIRCRAFT WAS GROUNDED.
- [SDR ABXA202004051051](https://openairdocs.org/sdr/ABXA202004051051.md): Escape Reel · deployed · Apr 1, 2020 · N795AX · Boeing 767281 · Emergency Equipment
  > INERTIAL ESCAPE REELS DEPLOYED. AIRCRAFT GROUNDED.
- [SDR ABXA20180828096](https://openairdocs.org/sdr/ABXA20180828096.md): Engine · making metal · Aug 28, 2018 · N795AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > ON CLIMB OUT AT APPROXIMATELY FLIGHT LEVEL 190, THE CREW HEARD A BOOM AND SMELLED A STRONG SMOKE ODOR. AT THE SAME TIME, THE AIRPLANE YAWED AND SHUTTERED. THE RIGHT ENGINE HAD HIGH EGT (1100 DEG) AND N2 INDICATION (113.1). THE RIGHT ENGINE WAS SHUT DOWN AND TH
- [SDR ABXA20180705075](https://openairdocs.org/sdr/ABXA20180705075.md): Stringer · corroded · Jul 5, 2018 · N795AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION ON THE UPPER NR 8 STRINGER COMMON TO THE UPPER SURFACE OF THE LOWER HORIZONTAL FLANGE JUST OUTBOARD OF RIB 2 (LBL 41.5 - RSS 0.00) OF THE LEFT HORIZONTAL STABILIZER. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20180705074](https://openairdocs.org/sdr/ABXA20180705074.md): Keelbeam · corroded · Jul 5, 2018 · N795AX · Boeing 767281 · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM LOWER INBOARD FLANGE AT BODY STATION 955 TO 1009. THE KEEL BEAM FLANGE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20180705073](https://openairdocs.org/sdr/ABXA20180705073.md): Structure · corroded · Jul 5, 2018 · N795AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON OUTBOARD LONGERON CHORD AT BODY STATION 1047 TO 1051 IN THE LEFT WHEEL WELL. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20170830096](https://openairdocs.org/sdr/ABXA20170830096.md): Carabiner · missing · Aug 30, 2017 · N795AX · Boeing 767281 · Emergency Equipment
  > THREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS U
- [SDR ABXA20170603070](https://openairdocs.org/sdr/ABXA20170603070.md): Container · unsecure · Jun 3, 2017 · N795AX · Boeing 767281 · Emergency Equipment
  > ON CLOSING THE L1 DOOR, TWO DESCENT DEVICES FELL OUT OF THE DESCENT DEVICE CONTAINER AND THEY UNWOUND TO THE FLOOR. WHILE THE AIRPLANE WAS GROUNDED, THE DESCENT DEVICES WERE REPLACED WITH SERVICEABLE DESCENT DEVICES. THE CAUSE FOR THE DESCENT DEVICES DROPPING
- [SDR ABXA20170225012](https://openairdocs.org/sdr/ABXA20170225012.md): Escape Rope · defective · Feb 25, 2017 · N795AX · Boeing 767281 · Emergency Equipment
  > WHILE THE AIRPLANE WAS REMOVED FROM SERVICE, TWO DESCENT DEVICES WERE FOUND PARTIALLY UNWOUND. THE DESCENT DEVICES WERE REPLACED. THE CAUSE FOR THE DESCENT DEVICES BECOMING UNWOUND IS UNKNOWN.
- [SDR ABXA20160830139](https://openairdocs.org/sdr/ABXA20160830139.md): Socket · inoperative · Aug 30, 2016 · N795AX · Boeing 767281 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. THE LAMP WAS REPLACED IN THE EMERGENCY LIGHT LAMPHOLDER ASSEMBLY. THE CAUSE OF THE INOPERATIVE LIGHT WAS A FAILED LAMP.
- [SDR ABXA20160830138](https://openairdocs.org/sdr/ABXA20160830138.md): Battery Pack · discharged · Aug 30, 2016 · N795AX · Boeing 767281 · Emergency Lighting
  > INTERIOR EMERGENCY LIGHTING SYSTEM INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED. THE CAUSE OF THE INOPERATIVE LIGHTS WAS A DISCHARGED BATTERY.
- [SDR ABXA20160613098](https://openairdocs.org/sdr/ABXA20160613098.md): Beam · corroded · Jun 13, 2016 · N795AX · Boeing 767281 · Wing, Attach Fittings
  > LEFT WING, T/E, STA WS 370, OTBD OF AFT CORNER OF PANEL 551XBX, FWD OF FLAP TRANSMISSION, MAJOR CORROSION. R & R BEAM, CHORD LT WING T/E STA WS 370 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 113T1407-5, SPOILERS BEAM CHORD, EXACT FS/BS LOCATION ON ACFT FROM STR,
- [SDR ABXA20160609100](https://openairdocs.org/sdr/ABXA20160609100.md): Stringer · cracked · Jun 9, 2016 · N795AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > AFT SIDE STA 676, STR 8L CRACKED IN RADIUS IN UPPER HAT FLANGE APPROXIMATELY 2" FROM FORWARD END. STR 8L AT STA 676 IAW ENGINEERING SKETCH ES 02821. CRACKED 2.0", PN 143T3001-6, STR 8L, LOCATION AT STA TO 709, STR LOCATION S8L. ACFT WAS GROUNDED.
- [SDR ABXA20160608099](https://openairdocs.org/sdr/ABXA20160608099.md): Attach Angle · corroded · Jun 8, 2016 · N795AX · Boeing 767281 · Wing, Attach Fittings
  > CORRODED LOWER T/E PANEL ATTACH ANGLE AT WS 364 AFT OF PANEL 651XBX. BLENDED AREA WITH THICKNESS OF.110" REMAINS.076" OUT OF LIMITS IAW SRM 57-51-02. R & R LOWER T/E PANEL ATTACH ANGLE AT WS 364 IAW SRM 51-40-02, SEC 9. CORRODED, PN 113T1407-6, SPOILER BE
- [SDR ABXA20160607096](https://openairdocs.org/sdr/ABXA20160607096.md): Stringer · corroded · Jun 7, 2016 · N795AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER BOX STR S-1U AFT HORIZONTAL LEG AT ATTACH POINT TO OTBD SIDE OF RIB 2R IS CORRODED, BLOWN OUT. REPAIRED STR 1 UPPER IN THE RT HORIZONTAL STABILIZER IAW REA B655-62090-MR. CORRODED LEVEL 2, PN: 182T3101-6, STRINGER, EXACT FS/BS LOCATION
- [SDR ABXA20160606097](https://openairdocs.org/sdr/ABXA20160606097.md): Stringer · corroded · Jun 6, 2016 · N795AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER BOX STR S-5L FORWARD VERTICAL LEG AT ATTACH POINT TO INBD SIDE OF RIB 2L IS CORRODED, BLOWN OUT. REPAIRED STRINGER 5 LOWER IN THE HORIZONTAL STABILIZER CENTER BOX IAW REA B655-62086-MR. 181T4100-5, STR, CORRODED: LEVEL 2, EXACT FS/BS LO
- [SDR ABXA20160603101](https://openairdocs.org/sdr/ABXA20160603101.md): Stringer · cracked · Jun 3, 2016 · N795AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > AFT SIDE STA 676, STR 11L CRACKED APPROXIMATELY 1.5" AROUND FORWARD HI-LOCK IN LOWER HAT FLANGE. REPAIRED STR 11L IAW SRM 53-0-03 AND ES 02821. CRACKED 1.5", PN 143T3001-7, STR 11L, EXACT FS/BS LOCATION ON AC FROM S11L, STA 676. ACFT WAS GROUNDED.
- [SDR ABXA20160602095](https://openairdocs.org/sdr/ABXA20160602095.md): Splice Plate · corroded · Jun 2, 2016 · N795AX · Boeing 767281 · Wing, Plate/Skin
  > LEFT WING L/E LOWER SPLICE PLATE IS CORRODED AT STA 627. REMOVED CORROSION IAW SRM 57-41-01 ON LOWER SPLICE PLATE AT STA 627 AND FOUND TO BE OUT OF LIMITS. REPAIRED ON REA NR B657-62081. CORRODED, LEVEL 2, PN 114T0222-9, PART NAME: SPLICE PLATE, EXACT STR/W
- [SDR ABXA20160601102](https://openairdocs.org/sdr/ABXA20160601102.md): Structure · cracked · Jun 1, 2016 · N795AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > INNER CHORD AT STA 883.5, RBL89 HAS CRACK INDICATION. REPAIR COMPLETED ON EA 53000050-101. CRACKED, PN 145T1004-2, INNER CHORD, EXACT FS/BS LOCATION ON ACFT AT STA 883.5, EXACT STR, WS LOCATION ON ACFT AT RBL 89. ACFT WAS GROUNDED.
- [SDR ABXA20140925311](https://openairdocs.org/sdr/ABXA20140925311.md): Channel · damaged · Sep 25, 2014 · N795AX · Boeing 767281 · Wing Miscellaneous Structure
  > WING TE PANEL ATTACH CHANNEL LOWER CHORD SPLIT ON EDGE AT WS 424.22 INCHES FROM REAR SPAR. INSTALLED NEW CHORD IAW REA B657-61210-MR & SRM 51-40-02. PANEL 552JB INSTALLED IAW SRM 51-40-02. SDR INFO PN 113T1407-1, PART NAME SPOILER BEAM CHORD, L2 CORROSION,
- [SDR ABXA20140924315](https://openairdocs.org/sdr/ABXA20140924315.md): Bushing · worn · Sep 24, 2014 · N795AX · Boeing 767281 · Trailing Edge Flaps
  > LEFT WING NR 2 FLAP HINGE 9 - 10 BEAM HAS LOOSE BUSHINGS IN CTR OF THE BEAM. REPLACED BUSHINGS IAW REA C027-61235-MR. PN 113T1347-7, PART NAME BUSHING, WORN & LOOSE BUSHING, EXACT FS & BS LOCATION ON ACFT LT WING, EXACT WS LOCATION ON ACFT WS 616. ACFT WAS
- [SDR ABXA20140924314](https://openairdocs.org/sdr/ABXA20140924314.md): Bearing · worn · Sep 24, 2014 · N795AX · Boeing 767281 · Trailing Edge Flaps
  > RIGHT FLAP HINGE POINT 9 - 10 BEAM HAS A LOOSE BEARING & A LOOSE BUSHING. R & R BEARING ON 9 - 10 BEAM AT FLAP SUPPORT NR 7 IAW CMM 27-51-97. THE 9 - 10 BEAM WILL BE INSTALLED ON NR 0037, SEE REACO27-61234-MR. PN 60B00180-236, PART NAME BEARING, WORN & LOOS
- [SDR ABXA201409243008](https://openairdocs.org/sdr/ABXA201409243008.md): Keelbeam · corroded · Sep 24, 2014 · N795AX · Boeing 767281 · Fuselage Main, Keel
  > CORROSION FOUND BETWEEN STATION 999 & 1021 IN LT WW CTR BEAM. REMOVED CORROSION IAW SRM 53-50-12 & COMPLIED WITH REA NR B653-61251-MR. CORRODED L2, PN 145T8612-1, PART NAME KEEL WEB, SN N/A, LOCATION STATION 999 LBL TO 1021 LBL. ACFT WAS GNDED.

Next page: https://openairdocs.org/deregistered/N795AX-2024-04-09/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 = 'N795AX' AND deregistration_id = 'N795AX-2024-04-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N795AX-2024-04-09/reports

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