# Service difficulty reports: N775AX, cancelled Apr 9, 2024

A list on [N775AX, cancelled Apr 9, 2024](https://openairdocs.org/deregistered/N775AX-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 2 · 82 reports

- [SDR ABXA20170705082](https://openairdocs.org/sdr/ABXA20170705082.md): Shear Tie · corroded · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 720 STRINGES 37-38L. THE SHEAR TIE WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170705081](https://openairdocs.org/sdr/ABXA20170705081.md): Floorbeam · corroded · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Main, Floor Beam
  > CORROSION AROUND THE NUTPLATES AND NUTCLIP HOLES ON THE UPPER TEE OF THE FORWARD LOWER CARGO COMPARTMENT FLOOR BEAM AT BS 742. THE TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705080](https://openairdocs.org/sdr/ABXA20170705080.md): Structure · corroded · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Main, Structure
  > CORROSION ON UPPER STRUCTURE AT BS 1373 IN THE AFT LOWER CARGO COMPARTMENT. THE STRUCTURE WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170705079](https://openairdocs.org/sdr/ABXA20170705079.md): Bracket · cracked · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Main, Attach Fittings
  > CRACKED BRACKET AT THE UPPER AFT SECTION OF THE FORWARD LOWER CARGO DOOR CUTOUT. THE BRACKET WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170705078](https://openairdocs.org/sdr/ABXA20170705078.md): Skin · corroded · Jul 5, 2017 · N775AX · Boeing 767281 · Wing, Plate/Skin
  > CORROSION ON LEFT WING LEADING EDGE UPPER SPLICE PLATE AT LEADING EDGE LWS 456. THE SPLICE PLATE WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705077](https://openairdocs.org/sdr/ABXA20170705077.md): Rib · corroded · Jul 5, 2017 · N775AX · Boeing 767281 · Wing, Rib/Bulkhead
  > CORROSION ON LOWER AIR LOAD RIB AT LEFT WING LEADING EDGE STATION 938. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705076](https://openairdocs.org/sdr/ABXA20170705076.md): Skin · corroded · Jul 5, 2017 · N775AX · Boeing 767281 · Wing, Plate/Skin
  > CORROSION ON LOWER SIDE OF UPPER SKIN AT LT WS 410 TO 424. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705075](https://openairdocs.org/sdr/ABXA20170705075.md): Bracket · cracked · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CRACK IN TWO AFT ATTACH ANGLES FOR THE LOWER LONGITUDINAL BEAMS AT THE AFT SPAR IN THE CENTER TANK. ONE BRACKET WAS CRACKED 4.25 INCHES, THE OTHER WAS CRACKED 2.5 INCHES. THE TWO BRACKETS WERE REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705074](https://openairdocs.org/sdr/ABXA20170705074.md): Skin · cracked · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN AROUND A FASTENER AT BS 1678. SKIN WAS REPAIRED. ACFT WAS GROUNDED.
- [SDR ABXA20170705073](https://openairdocs.org/sdr/ABXA20170705073.md): Skin · dented · Jul 5, 2017 · N775AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE SKIN BS 325-347. THE FUSELAGE SKIN WAS REPAIRED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170114002](https://openairdocs.org/sdr/ABXA20170114002.md): Bolt · missing · Jan 14, 2017 · N775AX · Boeing 767281 · Fuel Heater
  > LEFT ENGINE FLAME OUT (SHUT DOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 10,000 FEET. THE QUICK REFERENCE HANDBOOK’S ENGINE FAILURE AND ENGINE IN FLIGHT START CHECK LIST WAS COMPLETED. THE ENGINE RESTART WAS SUCCESSFUL. THE AIRPLANE WAS REMOVED FROM
- [SDR ABXA20160916146](https://openairdocs.org/sdr/ABXA20160916146.md): Escape Reel · unwanted deploy · Sep 16, 2016 · N775AX · Boeing 767281 · Emergency Equipment
  > WHILE PERFORMING INSPECTION OF THE DESCENT DEVICES, TWO DESCENT DEVICES FELL TO THE FLOOR, BREAKING THE SEALS. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL THE DESCENT DEVICES WERE REWOUND, RESEALED, AND RESTOWED. THE CAUSE FOR THE DESCENT DEVICES FA
- [SDR ABXA20160812141](https://openairdocs.org/sdr/ABXA20160812141.md): Escape Rope · inoperative · Aug 12, 2016 · N775AX · Boeing 767281 · Emergency Equipment
  > ONE DESCENT DEVICE WAS FOUND NOT PROPERLY STOWED AND INOPERATIVE DURING THE FLIGHT CREW’S PRE-FLIGHT INSPECTION. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) UNTIL THE DESCENT DEVICE WAS DEFERRED. THE NEXT DAY, THE AIRPLANE WAS REMOVED FROM SERVICE (GROUND
- [SDR ABXA20160331048](https://openairdocs.org/sdr/ABXA20160331048.md): Tee Fitting · corroded · Mar 31, 2016 · N775AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > LEFT T FITTING IS CORRODED AT THE FWD BOLT HOLES. MATCH DRILLED THE NEW T FITTING IAW SRM 51-40-05. T FITTING TO BE INSTALLED ON JC DOCUMENT 47008ORD03. CORRODED LEVEL 2, PN 100T1440V3, PART NAME T FITTING, SN NSN, EXACT FS & BS LOCATION ON ACFT 955, EXACT
- [SDR ABXA20160331047](https://openairdocs.org/sdr/ABXA20160331047.md): Tee Fitting · corroded · Mar 31, 2016 · N775AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > RIGHT T FITTING IS CORRODED AT THE FWD BOLT HOLES. NEW T FITTING DRILLED IAW SRM 57-40-05. NEW T FITTING TO BE INSTALLED ON DOCUMENT 47008ORD04. CORRODED LEVEL 2, PN 100T1440V4, PART NAME T FITTING, EXACT FS & BS LOCATION ON ACFT 955, EXACT STRINGER & WS LO
- [SDR ABXA20160324049](https://openairdocs.org/sdr/ABXA20160324049.md): Failsafe · cracked · Mar 24, 2016 · N775AX · Boeing 767281 · Fuselage Main, Frame
  > LEFT WW FAILSAFE STRAP AT STATION 955 IS CRACKED AT LOWER FASTENER HOLE. REFERENCE DOCUMENT 47008ORD01 STEP 21. PERFORMED CUT OUT OF CRACKED FAILSAFE IAW DOCUMENT 47008ORD03. REASSEMBLY TO BE ACCOMPLISHED ON DOCUMENT 47008ORD03. CRACKED LENGTH.500". PN 1
- [SDR ABXA20160323046](https://openairdocs.org/sdr/ABXA20160323046.md): Failsafe · cracked · Mar 23, 2016 · N775AX · Boeing 767281 · Fuselage Main, Frame
  > RIGHT WW FAILSAFE STRAP AT STATION 955, IS CRACKED AT LOWER FASTENER HOLE. REFERENCE DOCUMENT 47008ORD02 STEP 21. PERFORMED CUT OUT OF FAILSAFE IAW DOC 47008ORD04. CRACKED LENGTH 1.100", PN 145T2524U22, SN NSN, PART NAME FAILSAFE STRAP, EXACT FS & BS LOCATI
- [SDR ABXA20150527067](https://openairdocs.org/sdr/ABXA20150527067.md): Smoke Detector · false activation · May 27, 2015 · N775AX · Boeing 767281 · Smoke Detection
  > SERVICE AREA SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. CLEANED GRILL & DETECTOR UNIT. OPERATION CHECKED GOOD.
- [SDR ABXA20150526066](https://openairdocs.org/sdr/ABXA20150526066.md): Smoke Detector · false activation · May 26, 2015 · N775AX · Boeing 767281 · Smoke Detection
  > LAVATORY SMOKE ALARM SOUNDED. NO SMOKE OBSERVED. LAVATORY SMOKE DETECTOR OPERATION CHECKED GOOD.
- [SDR ABXA20131113654](https://openairdocs.org/sdr/ABXA20131113654.md): Beam · cracked · Nov 13, 2013 · N775AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON SKIRT BEAM ON OTBD SIDE IS CRACKED & CHAFED AROUND FASTENER HOLES. R & R NR 1 PYLON SKIRT BEAM OTBD SIDE IAW B767 SRM 51-40-02, PN 313T1380-241, NSN. BEAM CHAFED 1/4 INCHES, BEYOND REPAIR & CRACKED, NAC 298.93 TO 365.4 NAC WL 120. ACFT WAS GN
- [SDR ABXA20131113653](https://openairdocs.org/sdr/ABXA20131113653.md): Gusset · corroded · Nov 13, 2013 · N775AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 ENG PYLON FWD EDGE UPPER STRUCTURE HAS CHAFED AREA TO BARE METAL, WITH INLET REMOVED. R & R -36 CHAFFED GUSSET ON NR 1 ENG PYLON FWD UPPER EDGE IAW B767 SRM 51-40-2, PN 311T1510-36, NSN, GUSSET CHAFED FROM NAC STATION 144.5. ACFT WAS GNDED.
- [SDR ABXA20131107652](https://openairdocs.org/sdr/ABXA20131107652.md): Stiffener · cracked · Nov 7, 2013 · N775AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON FWD OF PANEL 437DB INSIDE STRUCTURE LOWER CROSS BRACE HILOCK LOOSE. R & R NEW FABRICATED PADS ON ALL AREAS DAMAGED. PN 313T3380-303 WEB & FRAME 1INCH CRACK, PN 313T1355-169 SPLICE 2 1/2 INCHES CRACK, PN 313T1355-181 1 INCH CRACK 313T3380-244 & 31
- [SDR ABXA20131107651](https://openairdocs.org/sdr/ABXA20131107651.md): Skin Panel · corroded · Nov 7, 2013 · N775AX · Boeing 767281 · Wing, Plate/Skin
  > UPPER TRAILING PANELS FWD OF OTBD AILERON RAISED IN TWO SPOTS ON PANEL LE. R & R UPPER TE PANELS IAW B767 SRM 51-40-02 PARA 4 & PARA 7. REPAIRED CORRODED SKIN IAW ABX REA B657-60785-MR REV IR DATED 11-14- 13. PN 112T3101, PN SKIN PANEL, SN NSN, CORRODED, A/
- [SDR ABXA20131107650](https://openairdocs.org/sdr/ABXA20131107650.md): Channel · corroded · Nov 7, 2013 · N775AX · Boeing 767281 · Wing, Attach Fittings
  > REAR SPAR TO TE PANEL ATTACH CHANNEL AT WING STATION 1046 SPLIT ON EDGE. FABRICATED NEW CHORD ON RFA B657-60757 REMOVED OLD CHORD & INSTALLED NEW CHORD IAW B767-200 SRM 51-40-02. CORRODED PN 113T1683-14 PN CHORD RIGHT WING LOWER TE EXACT STRINGER & WS LOCATI
- [SDR ABXA20120225219](https://openairdocs.org/sdr/ABXA20120225219.md): Spar · corroded · Feb 25, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT ON TOP OF REAR SPAR OF LEFT HORIZ STAB STA 318 TO 335. REPAIRED ON REA B655-59696-MR, A/W/G.
- [SDR ABXA20120225214](https://openairdocs.org/sdr/ABXA20120225214.md): Spar · corroded · Feb 25, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT ON REAR SPAR UPPER CAP ON LT HORIZONTAL STAB AT SS 238. REPAIRED ON REA B655-59696-MR.
- [SDR ABXA20120225213](https://openairdocs.org/sdr/ABXA20120225213.md): Rib · corroded · Feb 25, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT ON TOP OF RIB AT LEFT HORIZ STAB REAR SPAR TO TRAILING EDGE AT STA 226. REPAIRED ON REA B7655-59696-MR, AWG.
- [SDR ABXA20120225212](https://openairdocs.org/sdr/ABXA20120225212.md): Spar · corroded · Feb 25, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT ON TOP OF REAR SPAR OF LEFT HORIZ STAB REPAIRED ON REA B655-59696-MR, AWG
- [SDR ABXA20120225211](https://openairdocs.org/sdr/ABXA20120225211.md): Spar · corroded · Feb 25, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > SPOT OF CORROSION ON TOP OF REAR SPAR OF LEFT HORIZ STAB REPAIRED ON REA B655-59696-MR, A/W/G.
- [SDR ABXA20120224220](https://openairdocs.org/sdr/ABXA20120224220.md): Spar · corroded · Feb 24, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT ON RIB OF LEFT HORIZ STAB FROM REAR SPAR TO TRAILING EDGE AT STA 335. REPLACED "T" CORD IAW B767 SRM 51-40-02, AWG.
- [SDR ABXA20120224218](https://openairdocs.org/sdr/ABXA20120224218.md): Rib · corroded · Feb 24, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT ON RIB AT REAR SPAR TO TRAILING EDGE OF LEFT HORIZ STAB AT STA 323. REPLACED "T" CORD B767 SRM 51-40-02, A/W/G.
- [SDR ABXA20120224217](https://openairdocs.org/sdr/ABXA20120224217.md): Spar · corroded · Feb 24, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > CORROSION SPOT MARKED NR 4 ON TRAILING EDGE UPPER SPAR OF LEFT HORIZ STAB AT STA 287. REPAIRED IAW REA B655-55695-MR, A/W/G.
- [SDR ABXA20120224209](https://openairdocs.org/sdr/ABXA20120224209.md): Splice Plate · cracked · Feb 24, 2012 · N775AX · Boeing 767281 · Wing Miscellaneous Structure
  > LEFT WING OUTBD UPPER L/E SPLICE PLATE CRACKED AT APPOX LWS 564. REPAIRED IAW REA B651-59661, AIRCRAFT WAS GROUNDED.
- [SDR ABXA20120220206](https://openairdocs.org/sdr/ABXA20120220206.md): Skin · gouged · Feb 20, 2012 · N775AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS GOUGED AT FLC DOOR CUTOUT AREA LOWER FWD. REPAIRED IAW REA B653-59680.
- [SDR ABXA20120216207](https://openairdocs.org/sdr/ABXA20120216207.md): Shim · corroded · Feb 16, 2012 · N775AX · Boeing 767281 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORZ STAB TRAILING EDGE UPPER SURFACE BONDED PANEL BULGED AROUND FASTENER, LOCATED AFT OF RIB 13. REPLACED CORRODED SHIM AT RIB 13 IAW B767-200 SRM 51-20-11. ELEVATOR STA 335.109 AIRCRAFT WAS GROUNDED.
- [SDR ABXA20120215208](https://openairdocs.org/sdr/ABXA20120215208.md): Fitting · dented · Feb 15, 2012 · N775AX · Boeing 767281 · Nacelle/Pylon, Attach Fittings
  > LEFT ENGINE BACK UP FITTING OUTBOARD OF RIB 8 HAS 3 SMALL TOOLING MARKS. REMOVED TOOLING MARKS IAW REA B657-59674, AIRCRAFT WAS GROUNDED.
- [SDR ABXA20120206210](https://openairdocs.org/sdr/ABXA20120206210.md): Web · cracked · Feb 6, 2012 · N775AX · Boeing 767281 · Vertical Stabilizer Miscellaneous Structure
  > VERT STAB PANEL 324CLX ACCESS, LWR LT FWD ANGLE CRACKED INSIDE AUX BOX. REMOVED WEB AND ANGLE, FABRICATED ANGLE IAW BOEING DWG 173T1215. RE-INSTALLED FABRICATED ANGLE AND ORIGINAL WEB IAW 767 SRM 51-40-2.
- [SDR ABXA20111117132](https://openairdocs.org/sdr/ABXA20111117132.md): Escape Reel · deployed · Nov 22, 2011 · N775AX · Boeing 767281 · Emergency Equipment
  > FOUR ESCAPE REELS DEPLOYED AFTER LANDING. INSTALLED 4 EMERGENCY ESCAPE REELS PER B767 AMM 25-61- 03-4. PART EFFECTIVITY VERIFIED, AIRCRAFT WAS NOT GROUNDED.
- [SDR ABXA2011071669](https://openairdocs.org/sdr/ABXA2011071669.md): Light · inoperative · Jul 16, 2011 · N775AX · Boeing 767281 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AT LOWER AFT CORNER OF MED DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS PLACED TO "ON". RELAMPED, OP CHECK GOOD.
- [SDR ABXA201012070167](https://openairdocs.org/sdr/ABXA201012070167.md): Smoke Detector · false activation · Dec 5, 2010 · N775AX · Boeing 767281 · Smoke Detection
  > DETECTED FIRE/SMOKE IN MAIN CARGO COMPARTMENT. DECLARED EMERGENCY AND RETURNED TO LAND AT CVG. COMPLIED WITH OVERWEIGHT LANDING INSPECTION IAW 05-51-35-2 PHASE 1 OPTION A. NO DEFECTS FOUND. INSPECTED MAIN AND LOWER CARGO COMPARTMENTS, NO DEFECTS OR SMOKE N
- [SDR ABXA201008090103](https://openairdocs.org/sdr/ABXA201008090103.md): Fire Warning · false activation · Aug 8, 2010 · N775AX · Boeing 767281 · Fire Detection
  > WHEEL WELL FIRE ANNUNCIATOR LIGHT ON FORWARD PANEL COME ON DURING CRUISE. COMPLIED WITH ABNORMAL, FIRE TEST NORMAL. DEFERRED. WHEEL WELL LIGHT WILL NOT STAY ON WITH WHEEL WELL FIRE TEST OR LAMP TEST. TRIED NEW KORRY SWITCH & RELAY K693 - NO HELP.
- [SDR ABXA201006010083](https://openairdocs.org/sdr/ABXA201006010083.md): Slat Track · corroded · May 29, 2010 · N775AX · Boeing 767281 · Leading Edge Devices
  > NR 11 SLAT I/B AND O/B MAIN TRACKS HAVE SURFACE CORROSION ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED NR 11 SLAT MAIN TRACKS IAW B767 AMM 27-81-54-4. REMOVED AND REPLACED NR 11 SLAT IAW B767 AMM 27-81-02-4, OPS CHECK GOOD.
- [SDR ABXA201006010086](https://openairdocs.org/sdr/ABXA201006010086.md): Support · damaged · May 26, 2010 · N775AX · Boeing 767281 · Trailing Edge Flaps
  > NR 2 FLAP SUPPORT ACTUATOR FASTENER HOLES 3 EACH, 2 FWD UPPER SMALL DIA AND 1 LARGE AFT UPPER CENTER HOLE HAVE EDDY CURRENT INDICATION USING HOLD SCAN IAW 50-04 AND 51-00-16 PART 6 767 NDT. REWORKED HOLES AND INSTALLED FREEZE PLUGS IAW REA B657-58806-MR.
- [SDR ABXA201006010085](https://openairdocs.org/sdr/ABXA201006010085.md): Channel · cracked · May 25, 2010 · N775AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR PANEL ATTACH HAT CHANNEL HAS VERTICAL ATTACH ANGLE CRACKED AT STA 1417 RBL 8. REMOVED AND REPLACED ATTACH ANGLE IAW B767 SRM 51-40-02.
- [SDR ABXA201006010084](https://openairdocs.org/sdr/ABXA201006010084.md): Support · corroded · May 25, 2010 · N775AX · Boeing 767281 · Wing Miscellaneous Structure
  > LT WING L/E SUPPORT CORRODED ABOVE WING FUEL PANEL. REMOVED CORROSION. FOUND LT WING L/E SUPPORT TO BE OUT OF LIMITS. REPAIRED LT WING L/E SUPPORT IAW 767-200 SRM 57-41-09.
- [SDR ABXA201005200082](https://openairdocs.org/sdr/ABXA201005200082.md): Structure · cracked · May 18, 2010 · N775AX · Boeing 767281 · Engine Thrust Reverser
  > #1 ENG I/B THRUST REVERSER #13 CASCADE HAS 3 CRACKS. REMOVED AND REPLACED #13 CASCADE IAW B767 AMM 78-31-16-4
- [SDR ABXA201005200081](https://openairdocs.org/sdr/ABXA201005200081.md): Rib · corroded · May 17, 2010 · N775AX · Boeing 767281 · Wing, Rib/Bulkhead
  > LT WING L/E SUPPORT HAS CORROSION JUST INBD OF OUTBD AUX TRACK NR 3 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-40-2
- [SDR ABXA201005200079](https://openairdocs.org/sdr/ABXA201005200079.md): Support · corroded · May 17, 2010 · N775AX · Boeing 767281 · Leading Edge Devices
  > LT WING LE NR 3 SLAT INBD AUX TRACK HAS CORROSION ON INBD & OUTBD SUPPORTS. REMOVED CORROSION ON I/B SUPPORT IAW SRM51-10-02. REMOVED AND REPLACED SUPPORT IAW SRM 51-47-02
- [SDR ABXA201005200080](https://openairdocs.org/sdr/ABXA201005200080.md): Rib · damaged · May 14, 2010 · N775AX · Boeing 767281 · Wing, Rib/Bulkhead
  > CLOSE OUT NOSE RIB AT LES 568 IS DAMAGED. REMOVED DAMAGED NOSE RIB FABRICATED NEW NOSERIB IAW B767 DWG 114T2512. INSTALLED NOSE RIB IAW B767-200 SRM 51-40-02
- [SDR ABXA201005140076](https://openairdocs.org/sdr/ABXA201005140076.md): Structure · cracked · May 13, 2010 · N775AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CRACK EMANATING FROM RIVET AT BS 1702 BETWEEN S7L TO S8L. CRACK IS.1250 INCH IN LENGTH. REPAIRED AREA IAW B767 SRM 53-80-01-FIG 201.

Next page: https://openairdocs.org/deregistered/N775AX-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 = 'N775AX' AND deregistration_id = 'N775AX-2024-04-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N775AX-2024-04-09/reports

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