# Service difficulty reports: N747AX, cancelled May 7, 2021

A list on [N747AX, cancelled May 7, 2021](https://openairdocs.org/deregistered/N747AX-2021-05-07.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 · 77 reports

- [SDR ABXA20140527200](https://openairdocs.org/sdr/ABXA20140527200.md): Door Frame · corroded · May 27, 2014 · N747AX · Boeing 767232 · Fuselage Main, Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 549 INSIDE LOWER SEAL, FWD PART OF DOOR JAMB IS CORRODED. NEW OUTER CHORD PN 143T8004-1, INSTALLED ON NR 1071. SDR INFO CORRODED L2, PN 143T8004-1, SN NSN, PART NAME CHORD, FS & BS LOCATION ON ACFT 549 TO 593, STRINGER &
- [SDR ABXA20140527170](https://openairdocs.org/sdr/ABXA20140527170.md): Angle · corroded · May 27, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 544 AT FWD CORNER OF DOOR JAMB. UNDER THE THRESHOLD ARE TWO SPOTS OF CORROSION. REPLACE CORRODED ANGLE WITH A NEW PART PN 143T4003-3, INSTALL IAW SRM 51-40-02. CORRODED L2, PN 143T5003-3, SN NSN, PART NAME ANGLE, FS & BS
- [SDR ABXA20140523202](https://openairdocs.org/sdr/ABXA20140523202.md): Stringer · cracked · May 23, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > NEW STRINGER 24L PN 146T3002-55 NEEDS INSTALLED FROM FS 1307 - 1417. OLD STRINGER WAS REMOVED ON WORK ORDER 600324529 NR 0511. REMOVED STRINGER 24L AT FS 1307 - 1417. FABRICATED NEW STRINGER IAW REA 653-61024- MR. INSTALLED NEW STRINGER 24L AT FS 1307 - 14
- [SDR ABXA20140523201](https://openairdocs.org/sdr/ABXA20140523201.md): Stringer · cracked · May 23, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > NEW STRINGER 26L PN 146T3002-57 NEEDS INSTALLED FROM FS 1307 - 1417. THE OLD STRINGER WAS REMOVED ON WORK ORDER 600324529 NON-ROUTINE 0510. FABRICATED NEW STRINGER 26L IAW REA B653-61024-MR. R & R STRINGER 26L AT FS 1307 - 1417 IAW B767 SRM 51-40-02 PARA 7
- [SDR ABXA20140520169](https://openairdocs.org/sdr/ABXA20140520169.md): Floor Support · corroded · May 20, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO RT SIDE ABOVE STRINGER 35R BETWEEN STATION 1285 & 1307 UNDERNEATH THE PDU, THE FLOOR & SUPPORT IS CORRODED. R & R INTERCOSTAL ABOVE STRINGER 35R BETWEEN STATION 1285 & 1307 IAW 51-40-02 SRM. CORRODED L2, PN 146T5000-146, SN NSN, PART NAME: SU
- [SDR ABXA20140516165](https://openairdocs.org/sdr/ABXA20140516165.md): Floorbeam · corroded · May 16, 2014 · N747AX · Boeing 767232 · Fuselage Main, Floor Beam
  > AFT LOWER CARGO CTR BILGE AREA RT STATION 1263 AT STRINGER 35R AREA THERE IS CORROSION AT THE FLOORBEAM UPPER CHORD NUTPLATES. R & R UPPER CHORD IAW 51-40-02. CORRODED LEVEL 2, PN 146T1209-5146T5000-15 & 16, PART NAME INNER CHORD & SUPPORT, CARGO CONTAINER A
- [SDR ABXA20140515181](https://openairdocs.org/sdr/ABXA20140515181.md): Stiffener · cracked · May 15, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > VERTICAL STIFFENER ON FRAME AT FS 1480 ABOVE STRINGER 38R CRACKED AT UPPER ATTACHING HOLE. REMOVED DAMAGED STIFFENER AT STATION 1480 STRINGER 38R & INSTALLED NEW STIFFENER AT SAME LOCATION PN 146T1261-4 IAW SRM 51-40-02, SN N/A, PART NAME STIFFENER, CRACKED.
- [SDR ABXA20140515180](https://openairdocs.org/sdr/ABXA20140515180.md): Stiffener · cracked · May 15, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > FRAME VERTICAL STIFFENER AT FS 1480 ABOVE STRINGER 38L CRACKED AT UPPER HOLE. REMOVED DAMAGED STIFFENER AT STATION 1480 STRINGER 38L & INSTALLED NEW STIFFENER AT SAME LOCATION. PN 146T1261-3 IAW SRM 51-40-02 SN NA, PART NAME STIFFENER, CRACKED.340, FS & BS
- [SDR ABXA20140515175](https://openairdocs.org/sdr/ABXA20140515175.md): Channel · corroded · May 15, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > SECTION 43 AT DRAIN CHANNEL BEAM STATION 676 HAS SEVERAL AREAS OF CORROSION. REMOVED CORRODED DRAIN CHANNEL, FIVE EACH AT STATION 676. FABRICATED NEW CHANNEL IAW REA B563-60987 & B563-60967. INSTALLED NEW DRAIN CHANNEL IAW SRM 51-40-02. PN 368-53-33-90988-
- [SDR ABXA20140515172](https://openairdocs.org/sdr/ABXA20140515172.md): Stringer · corroded · May 15, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > BULK CARGO, CORROSION AT STRINGER 35L BETWEEN STATION 1480 & 1461. REMOVED DAMAGED SECTION AT STRINGER 35L FROM STATION 1447 - 1526 & ATTACHING STRUCTURE. INSTALLED STRINGER REPAIR IN AREA OF DAMAGE & REINSTALLED ATTACHING STRUCTURE IAW SRM 53-00-03 FIG 201
- [SDR ABXA20140515171](https://openairdocs.org/sdr/ABXA20140515171.md): Stringer · corroded · May 15, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > BULK CARGO, CORROSION AT STRINGER 35L BETWEEN STATION 1480 & 1502. REMOVED DAMAGED SECTION OF STRINGER 35L FROM STATION 1447 - 1526 & INSTALLED STRINGER REPAIR IN SAME LOCATION IAW SRM 53-00-03 FIG 201 REPAIR 2. PN 146T3003, SN NSN, PART NAME STRINGER, CORRO
- [SDR ABXA20140515157](https://openairdocs.org/sdr/ABXA20140515157.md): Skin · dented · May 15, 2014 · N747AX · Boeing 767232 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN BETWEEN BS 610 - BS 620, STRINGER 31R - STRINGER 32R HAS SEVERAL DENTS BETWEEN DOOR CUT OUT & EXTERNAL REPAIR DOUBLERS NOT RECORDED ON ACFT OPEN DENT REPORT. REPAIR DENT IN FUSELAGE SKIN AT BS 610 - 620, STRINGER 31R - STRINGER 32R IAW
- [SDR ABXA20140514177](https://openairdocs.org/sdr/ABXA20140514177.md): Stringer · corroded · May 14, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > STRINGER U17C HAS CORROSION TOP & BOTTOM LEGS. INSTALLED NEW SECTION OF STRINGER & SPLICE IAW B767-200 & 57-00-03 REPAIR 2, FIG 201. CORRODED L2, PN 111T3007, SN NSN, PART NAME U17 CTR WING UPPER STRINGER. FS & BS LOCATION ON AC FS 859, STRINGER & WS LOCATI
- [SDR ABXA20140514176](https://openairdocs.org/sdr/ABXA20140514176.md): Stringer · corroded · May 14, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO BETWEEN FUSELAGE STATIONS 478 & 500, STRINGER 36R IS CRACKED & CORRODED. R & R 536R AT STATION 487 TO 509 IAW SRM 51-40-02 & REA B653-60965 MR. CRACKED & CORRODED. PN 143T3001-70, PART NAME STRINGER, FS & BS LOCATION FROM 488 TP 517, STR
- [SDR ABXA20140513174](https://openairdocs.org/sdr/ABXA20140513174.md): Bulkhead · corroded · May 13, 2014 · N747AX · Boeing 767232 · Fuselage Main, Bulkhead
  > STATION 852 LT CORROSION ON A PREVIOUS REPAIR ON CANTED PRESS BULKHEAD. REPAIRED ON REA B653-60976-MR. CORRODED L2, PN 111T3012 & 1111T3013, NO SERIAL NR, PART NAME CTR TANK, UPPER SKINS, FS & BS LOCATION ON ACFT FS 859, LBL 60 - 97. ACFT WAS GNDED.
- [SDR ABXA20140512179](https://openairdocs.org/sdr/ABXA20140512179.md): Fitting · corroded · May 12, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > LEFT HAND ABOVE CTR TANK FS 859 LBL 97 STUB BEAM FITTING CORRODED AT ATTACH FASTENERS COMMON TO CTR TANK. REPAIRED STUB BEAM ON REA B653-60969-MR. CORRODED L2, PN 145T1903-5, SN NSN, PART NAME STUB BEAM FITTING, FS & BS LOCATION ON ACFT FS 858 TO 860, STRING
- [SDR ABXA20140512173](https://openairdocs.org/sdr/ABXA20140512173.md): Bulkhead · corroded · May 12, 2014 · N747AX · Boeing 767232 · Fuselage Main, Bulkhead
  > STATION 889 LT CORROSION ON CANTED PRESS BULKHEAD UNDER BEAM. REPAIRED ON REA B653-60977-MR. CORRODED L2, PN 111T3013-1, SN NSN, PART NAME UPPER CTR WING SKIN, FS & BS LOCATION ON ACFT FS 878 TO 889. ACFT WAS GNDED.
- [SDR ABXA20140509167](https://openairdocs.org/sdr/ABXA20140509167.md): Intercostal · corroded · May 9, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO CTR BILGE AREA, THE INTERCOSTAL ABOVE STRINGER 36R BETWEEN 1263 & 1285 IS CORRODED. R & R INTERCOSTAL ABOVE STRINGER 36R BETWEEN STATION 1263 - 1285 IAW SRM 51-40-02. CORRODED L2, PN 146T5000-8, SN NSN, PART NAME SUPPORT, FS & BS LOCATION ON
- [SDR ABXA20140509166](https://openairdocs.org/sdr/ABXA20140509166.md): Stringer · corroded · May 9, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > AFT LOWER CARGO CTR BILGE AREA, STRINGER 36R BETWEEN STATION 1263 & 1285 IS CORRODED. REMOVED DAMAGED STRINGER 36R & INSTALLED NEW REPAIR IAW SRM 53-00-03, REPAIR 2 NR 39 351070. CORRODED L2, PN 146T3003, SN NSN, PART NAME STRINGER, FS & BS LOCATION ON ACFT
- [SDR ABXA20140509164](https://openairdocs.org/sdr/ABXA20140509164.md): Intercostal · corroded · May 9, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > CENTER BILGE RT SIDE OTBD INTERCOSTAL CORRODED ABOVE STRINGER 35R AREA. R & R INTERCOSTAL IN CTR BILGE ABOVE STRINGER 35R IAW SRM 51-40-02. CORRODED L2, PN 146T5000-195, SN NSN, PART NAME SUPPORT, CARGO CONTAINER. FS & BS LOCATION ON ACFT STATION 1263 TO ST
- [SDR ABXA20140508168](https://openairdocs.org/sdr/ABXA20140508168.md): Beam · corroded · May 8, 2014 · N747AX · Boeing 767232 · Wing Miscellaneous Structure
  > LEFT WING INBD TE PANEL UPPER BEAM CAP IS CRACKED & CORRODED AT WS 280 JUST INBD OF LT MLG. REMOVED UPPER SKIN PANELS, REMOVED LT WING INBD TE UPPER BEAM CAP & REPLACED UPPER BEAM CAP IAW SRM 51-40-02 PARA 4 B & PARA 7D, REINSTALLED UPPER SKIN PANELS IAW SRM
- [SDR ABXA20140508160](https://openairdocs.org/sdr/ABXA20140508160.md): Stringer · cracked · May 8, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L BETWEEN STATION 1329 & 1353 IS CRACKED AT BOTH STRINGER TIES. NEW STRINGER WILL BE INSTALLED ON NR-0001 WORK ORDER 48362. CRACKED 24 INCHES, PN 146T3002-57, SN NA, PART NAME STRINGER, FS & BS LOCATION ON ACFT FS 1329 TO FS 1353, STRINGERS & WS L
- [SDR ABXA20140506156](https://openairdocs.org/sdr/ABXA20140506156.md): Seat Track · cracked · May 6, 2014 · N747AX · Boeing 767232 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAIN'S OTBD FWD SEAT TRACK CRACKED BETWEEN 2 BOLTS FOR FWD STOP. R & R CAPTAIN'S OTBD FWD SEAT TRACK IAW SRM 51-40-02. CRACKED IS 2.0 INCHES, PN 812175-7, PART NAME CAPTAIN & FIRST OFFICER SEAT TRACK, SN NSN, FS & BS LOCATION 196.5. ACFT WAS GNDED.
- [SDR ABXA20140505163](https://openairdocs.org/sdr/ABXA20140505163.md): Intercostal · corroded · May 5, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO FWD BILGE THE RT INTERCOSTAL BETWEEN STATION 1153 & 1175 IS CORRODED AT THE BACK CORNER. R & R INTERCOSTAL IN AFT LOWER CARGO BETWEEN STATION 1153 & 1175 IN FWD BILGE ON RT SIDE. CORRODED LEVEL 2, PN 146T5000-58, SN NSN, FS & BS LOCATION FROM
- [SDR ABXA20140502178](https://openairdocs.org/sdr/ABXA20140502178.md): Beam · corroded · May 2, 2014 · N747AX · Boeing 767232 · Main Landing Gear Attach Section
  > DURING CURSORY INSPECTION OF RT GEAR AUX BEAM WHERE BUSHING WAS REMOVED, FOUND CORROSION ON CIRCUMFERENCE OF BEAM WHERE BUSING WAS MOUNTED. REAMED HOLE CLEAN & ROUND TO 3.564 DIAMETER, CRO SPOT FACED THE DISCREPANT HOLE, MANUFACTURED & INSTALLED REPAIR BUSHIN
- [SDR ABXA20140501158](https://openairdocs.org/sdr/ABXA20140501158.md): Counterweight · corroded · May 1, 2014 · N747AX · Boeing 767232 · Ailerons
  > RIGHT OTBD AILERON, OTBD COUNTERWEIGHT HORN, IS CORRODED & CRACKED AT COUNTER WEIGHT. R & R CORRODED & CRACKED RT OTBD AILERON OTBD COUNTER WEIGHT HORN IAW DWG 113T7106, SRM 51-40-05 & 51-40-08, AMM 51- 21-10-7 & 51-31-01. CORRODED LEVEL 2 PN 1137106, PART N
- [SDR ABXA20140430159](https://openairdocs.org/sdr/ABXA20140430159.md): Skin Panel · corroded · Apr 30, 2014 · N747AX · Boeing 767232 · Wing, Plate/Skin
  > UPPER WING SURFACE PANEL SEPARATING ON LE JUST FWD OF NR 10 SPOILER, UPPER SURFACE OF THE WING. REMOVED TE WING PANEL TO FOM CORROSION ON WING SKIN IAW SRM 57-20-01 FIG 01 IAW REA B657-60934-MR. CORRODED LEVEL 2, PN 112T3101-6, PART NAME UPPER SKIN, SN N/A,
- [SDR ABXA2014042790](https://openairdocs.org/sdr/ABXA2014042790.md): Seat Track · corroded · Apr 27, 2014 · N747AX · Boeing 767232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FS 355 BL10 RT. R & R SEAT TRACK RBC10 IAW SRM 51-40-02. SDR INFO PN 368-53-11-90610, NSN, CORRODED L2, PART SEAT TRACK, FS & BS LOC FS 347 - FS 445. ACFT WAS GNDED.
- [SDR ABXA2014042593](https://openairdocs.org/sdr/ABXA2014042593.md): Stringer · cracked · Apr 25, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > DURING INSTALL OF STRINGER SPLICE ON STRINGER 32L AT STATION 434, STRINGER CRACKED WHILE INSTALLING FASTENERS & CORROSION WAS FOUND AT CRACK LOCATION. REPAIRED STRINGER 32L AT FS 434 IAW REA B653-60965-MR. SDR INFO CRACKED 1 INCH, CORRODED, PN 143T3001, PART
- [SDR ABXA2014042592](https://openairdocs.org/sdr/ABXA2014042592.md): Stringer · cracked · Apr 25, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > STRINGER CRACKED AT STATION 1520 LOCATED BY ANTENNA BRACKET APPROX STRINGER 2L OR 3L. INSTALLED NEW SECTION OF STRINGER & SPLICES IAW SRM 53-00-03 REPAIR 1 FIG 201 DETAIL 2. SDR INFO CRACKED 3 INCHES, PN 146T3002, PART NAME STRINGER 3L, SN NSN, FS & BS LOC 1
- [SDR ABXA2014042487](https://openairdocs.org/sdr/ABXA2014042487.md): Intercostal · corroded · Apr 24, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO RT SIDE, INTERCOSTAL ABOVE STRINGER 36R BETWEEN STATION 1329 & 1351 CORRODED AT NUTPLATE. R & R INTERCOSTAL IN AFT LOWER CARGO STATION 1329 & 1351, RT SIDE IAW SRM 51-40-02 & DWG 146T5000. SDR INFO PN 146T5000-39, NSN, SUPPORT INTERCOSTAL, CO
- [SDR ABXA20140423162](https://openairdocs.org/sdr/ABXA20140423162.md): Splice Plate · corroded · Apr 23, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > SEVERAL CORRODED NUTPLATES FOR FWD BILGE PANEL ON FLOORBEAM UPPER CHORD AT STATION 1175. REMOVED, MANUFACTURED & INSTALLED NEW SPLICE PLATE AT STATION 1175 IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 146T5000-92, SN NSN, PART NAME SPLICE PLATE, EXACT FS
- [SDR ABXA20140422161](https://openairdocs.org/sdr/ABXA20140422161.md): Intercostal · corroded · Apr 22, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO FWD BILGE AREA BETWEEN STATION 1153 & 1175. THE LT INTERCOSTAL BACK CORNER IS CORRODED. R & R NEW INTERCOSTAL IN FWD BILGE AREA BETWEEN STATION 1153 & 1175 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 146T5000-60, SN NSN, EXACT FS & BS LOCATION ON
- [SDR ABXA2014042186](https://openairdocs.org/sdr/ABXA2014042186.md): Stringer Clip · corroded · Apr 21, 2014 · N747AX · Boeing 767232 · Fuselage Main, Attach Fittings
  > FORWARD LOWER CARGO AFT SIDE OF REAR BULKHEAD FUSELAGE STATION 742 WHERE STRINGER 36R ATTACHES TO BULKHEAD CLIP IS CORRODED. FABRICATED NEW STRINGER CLIP FROM 1518-714-7075-T6511 INSTALLED NEW STRINGER CLIP IAW B65360890. SDR INFO CORRODED, PN 140T2101-413AX
- [SDR ABXA2014041791](https://openairdocs.org/sdr/ABXA2014041791.md): Stringer · corroded · Apr 17, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO FS 456 - 478, STRINGER 33L HAS EVIDENCE OF IMPACT DAMAGE TO SIDE OF STRINGER CAUSING IT NOT TO LAY FLAT AGAINST FUSELAGE SKIN ON LOWER SIDE OF STRINGER. R & R STRINGER AT FS 456 - 478, STRINGER 33L IAW SRM 51-40-02. R & R EQUIP COOLING DU
- [SDR ABXA2014041589](https://openairdocs.org/sdr/ABXA2014041589.md): Floor Support · corroded · Apr 15, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > BULK CARGO FLOOR SUPPORT ABOVE STRINGER 35R BETWEEN STATION 1417 & 1439 IS CORRODED BETWEEN NUTPLATE & SUPPORT. REPAIR FLOOR SUPPORT & REPLACED TRANSITION SUPPORT AT RBL 25 FS 1439 & 1417 IAW SRM 51-70-11. SDR INFO CORRODED L-2, PN 146T5004-21/146T5006-1, PA
- [SDR ABXA2014041588](https://openairdocs.org/sdr/ABXA2014041588.md): Web · corroded · Apr 15, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > STATION 1417 LBL 8 HAS CORRODED WEB. INSTALLED NEW WEB PN 452T3288-5AX IAW SRM 51-40-2. TWO INTERCOSTALS INSTALLED PN 482T3251-1 & 452T3252-2. SDR INFO CORRODED L2, PN 452T3288-5, 452T3252-2 & 452T3251-1, PART NAME WEB, SN NSN, FS & BS LOC STATION 1417 TO 14
- [SDR ABXA2014041584](https://openairdocs.org/sdr/ABXA2014041584.md): Attach Fitting · corroded · Apr 15, 2014 · N747AX · Boeing 767232 · Wing Miscellaneous Structure
  > REAR SPAR TO TE LOWER PANEL ATTACH CHORD ON WING AT INBD END OF INBD AILERON CORRODED. REMOVED PANEL 652JB, REMOVED REAR TE LOWER CHORD AT WS 431.97. INSTALLED NEW TE LOWER CHORD AT WS 431.97 IAW SRM 51-40-02 PARA 7 D & PAR 4 6. REINSTALLED PANEL 652JB IAW
- [SDR ABXA2014041481](https://openairdocs.org/sdr/ABXA2014041481.md): Skin · corroded · Apr 14, 2014 · N747AX · Boeing 767232 · Trailing Edge Flaps
  > LEFT WING INBD MID FLAP AREA UPPER SKIN HAS A CORROSION SPOT THAT HAS BEEN BLENDED BEYOND LIMITS & REQUIRES A COMPOSITE REPAIR IAW NR -1599, 30.5 INCHES FROM OTBD EDGE & 34 INCHES FROM AFT EDGE. REPAIRED CW INBD MID FLAP UPPER SKIN IAW SRM 57-53-01 & 51-70-10
- [SDR ABXA2014041076](https://openairdocs.org/sdr/ABXA2014041076.md): Stringer · cracked · Apr 10, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > STRINGER CRACKED AFT OF STATION 676 LT. REPAIRED STRINGER AT STATION 676 IAW B653-60928-MR. SDR INFO CRACKED 0.50, PN 143T3001-22, PART NAME STRINGER, EXACT FS & BS LOCATION ON ACFT FROM FS 676, STRINGER 12L. ACFT WAS GNDED.
- [SDR ABXA2014040983](https://openairdocs.org/sdr/ABXA2014040983.md): Swivel · gouged · Apr 9, 2014 · N747AX · Boeing 767232 · Wing, Landing Gear Attach Fittings
  > SIDE BRACE SPINDLE ON WING HAS CHAFE AREA. BLENDED AREA IS REPAIRED IAW B657-60955-MR. SDR INFO PN 113T1110-7, NSN, 1 INCH GOUGE, PART NAME LT LANDING GEAR SIDE, STRUT SWIVEL, GOUGE, INBD FWD OUTER RADIUS. ACFT WAS GNDED.
- [SDR ABXA2014040975](https://openairdocs.org/sdr/ABXA2014040975.md): Stringer · corroded · Apr 9, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > FS 452, STRINGER 37R CORRODED AROUND RIVET. FOUND STRINGER TO BE OUT OF LIMITS. R & R NEW STRINGER & REPAIR PARTS SRM 53-00-03. SDR INFO CORRODED, PN 143T3001-72, SN NONE, PART NAME STRINGER, EXACT FS & BS LOCATION ON ACFT FROM FS 434 TO FS 467, EXACT STRIN
- [SDR ABXA2014040974](https://openairdocs.org/sdr/ABXA2014040974.md): Stringer · corroded · Apr 9, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO FS 452, STRINGER 38R CORRODED AROUND RIVET. FOUND STRINGER TO BE OUT OF LIMITS. R & R NEW STRINGER & REPAIR PARTS IAW SRM 53-00-05. SDR INFO CORRODED, PN 143T3001, SN NONE, PART NAME STRINGER, EXACT FS & BS LOC ON ACFT FROM FS 445 TO FS
- [SDR ABXA2014040773](https://openairdocs.org/sdr/ABXA2014040773.md): Stringer · cracked · Apr 7, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > STRINGER CRACKED AT STATION 720, STRINGER 12R. REPAIRED AREA IAW B653-60931-MR. SDR INFO CRACKED 1 INCH & 1/4, PN 143T3001-8, NSN, STRINGER. ACFT WAS GNDED.
- [SDR ABXA2014040771](https://openairdocs.org/sdr/ABXA2014040771.md): Floor Support · corroded · Apr 7, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 742 AFT BULKHEAD LOWER FLANGE FOR FLOOR PANELS IS CORRODED, UPPER & LOWER SIDES. REPLACED AFT BULKHEAD LOWER FLANGE IAW SRM 51-40-02. SDR INFO PN 453T1637-3, NSN, SUPPORT FOR FLOOR, FS & BS LOC FS 742, CORRODED. ACFT WAS
- [SDR ABXA2014040480](https://openairdocs.org/sdr/ABXA2014040480.md): Stiffener · cracked · Apr 4, 2014 · N747AX · Boeing 767232 · Cargo/Baggage Doors
  > BULK CARGO DOOR INTERIOR VERTICAL STIFFENER PN 146T6348-2 IS CRACKED. FOUND WHILE DISASSEMBLING STRUCTURE FOR REPAIRS ON NR 0193. REMOVED DAMAGED CHORD. SABBED NEW CHORD & INSTALLED NEW CHORD IAW SRM 52-30-02 & 51-40-02. SDR INFO CRACKED 1 INCH, PN 146T634
- [SDR ABXA2014040472](https://openairdocs.org/sdr/ABXA2014040472.md): Floor Support · corroded · Apr 4, 2014 · N747AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO FUSELAGE STATION 720 - 742 LBL 7 FLOOR ANGLE CORRODED ON BOTTOM SIDE. REPLACED FLOOR SUPPORT IAW SRM 51-40-02. PN 451T1307, SUPPORT, CORRODED, FUSELAGE STATION 720 - 742. ACFT WAS GNDED.
- [SDR ABXA2014040470](https://openairdocs.org/sdr/ABXA2014040470.md): Support Angle · cracked · Apr 4, 2014 · N747AX · Boeing 767232 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB ACCESS 324CLX & 324AL, SUPPORT STRUCTURE BOX FWD LWR FLANGE CRACKED LT & RT OTBD EDGES. REMOVED CRACKED SUPPORT ANGLE. FABRICATED NEW SUPPORT IAW DWG 173T1215 & SAMPLE. PN 173T1302-1, NSN, SUPPORT ANGLE, CRACKED 2 INCHES & 1.5 INCHES, STATION
- [SDR ABXA2014040179](https://openairdocs.org/sdr/ABXA2014040179.md): Stiffener · cracked · Apr 1, 2014 · N747AX · Boeing 767232 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON INBD HYD BAY. AFT HORZ STIFFENER AT NAC 370 HAS DAMAGED HOLES COMMON TO THE LOWER DOOR FRAME CHANNEL. REMOVED DAMAGED STIFFENER IAW SRM 51-40-02. FABRICATED NEW STIFFENER IAW SRM 54-51-71 & 51-30-01, PERFORMED NDT IAW NDTM PART 6 51-00- 19, A
- [SDR ABXA2014032885](https://openairdocs.org/sdr/ABXA2014032885.md): Stringer Splice · cracked · Mar 28, 2014 · N747AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > FORWARD LOWER CARGO FUSELAGE STATION 437, STRINGER 31R AT STRINGER SPLICE IS CRACKED & CORRODED. REMOVED CORRODED STRINGER SPLICE AT FS 434, STRINGER 31R & INSTALLED NEW STRINGER SPLICE IAW SRM 51-40-02. SDR INFO CRACKED.050 INCHES, PN 140T0115-20, PART NAM

Next page: https://openairdocs.org/deregistered/N747AX-2021-05-07/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 = 'N747AX' AND deregistration_id = 'N747AX-2021-05-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N747AX-2021-05-07/reports

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