# Service difficulty reports: N1181A

A list on [N1181A](https://openairdocs.org/aircraft/N1181A.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 9 · 435 reports

- [SDR 21GA0260904001](https://openairdocs.org/sdr/21GA0260904001.md): None · pilot error · Sep 4, 2026 · N1181A · Boeing 7673Y0 · Standard Practices/Structures
  > DURING CRUISE, THE FLIGHT CREW EXPERIENCED A SHUTDOWN OF THE LEFT ENGINE AND SUBSEQUENTLY DIVERTED THE AIRCRAFT TO PUNTA CANA (PUJ). THE AIRCRAFT LANDED SAFELY IN PUJ AT APPROXIMATELY 1256Z. PRELIMINARY INFORMATION RECEIVED FROM THE CREW INDICATES THAT THE FU
- [SDR ABXR2026042900008](https://openairdocs.org/sdr/ABXR2026042900008.md): Structure · cracked · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT SIDE OF CHORD AT STA. 1809 TENSION FITTING FORWARD BOLT HOLE HAS CRACK
- [SDR ABXR2026042900007](https://openairdocs.org/sdr/ABXR2026042900007.md): Skin Panel · delaminated · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL INBD UPPER FIXED L/E IS DELAMINATED.
- [SDR ABXR2026042900006](https://openairdocs.org/sdr/ABXR2026042900006.md): Skin · cracked · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Fuselage Main, Plate/Skin
  > FOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2
- [SDR ABXR2026042900005](https://openairdocs.org/sdr/ABXR2026042900005.md): Angle · cracked · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous Structure
  > VERTICAL ANGLE CRACKED AT STA. 1085 LBL 26. CLIP MONOCOQUE
- [SDR 21GA20250906018](https://openairdocs.org/sdr/21GA20250906018.md): Warning Message · false activation · Aug 29, 2025 · N1181A · Boeing 7673Y0 · Trailing Flap Position Indicating System
  > ON APPROACH, SELECTED FLAPS TO 20. RECEIVED TE FLAP DISAGREE EICAS MESSAGE. DID GO AROUND, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURE. NO DEFECTS NOTED.
- [SDR UIEA2024072400743](https://openairdocs.org/sdr/UIEA2024072400743.md): Escape Reel · unwanted deploy · Jul 24, 2024 · N1181A · Boeing 7673Y0 · Emergency Equipment
  > 1 EA ESCAPE INERTIAL REEL DEVICE FULL OUT(<P>TRANSFER TO DMI 213408 PER MEL 25-61-01-01 CAT C DUE DATE 4AUG2024. PN 379103D-29</P> / <P>LP 1239968 ITEM 5 / ONT / 27JUL24: INSTALLED 1 EA INERTIA REEL IAW B767 AMM 25-61-01. NO FUTHER DEFECTS NOTED. THIS CLEARS M
- [SDR UIEA2024033000230](https://openairdocs.org/sdr/UIEA2024033000230.md): Escape Reel · unwanted deploy · Mar 30, 2024 · N1181A · Boeing 7673Y0 · Emergency Equipment
  > INERTIAL ESCAPE REEL DROPPED DURING DESCENT(<P>REVOVED AND REPLACED EMERGENCY DESCENT DEVICE IAW AMM 25-51-05. THIS CLEARS MDDR 205698. PLACARD REMOVED.</P>)
- [SDR UIEA2024032300207](https://openairdocs.org/sdr/UIEA2024032300207.md): Escape Reel · unwanted deploy · Mar 23, 2024 · N1181A · Boeing 7673Y0 · Emergency Equipment
  > INERTIAL REEL DEPLOYED ON TAKE-OFF ROLL(<P>R/R DEPLOYER DESCENT DEVICE IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2024031900161](https://openairdocs.org/sdr/UIEA2024031900161.md): Target · out of adjust · Mar 18, 2024 · N1181A · Boeing 7673Y0 · Landing Gear Position and Warning
  > NOSE AIR/GRND STATUS MESSAGE(<P>INSTALLED TARGET AND ADJUSTMENT BRACKET INSTALLED IAW BOEING AMM 32-61-03 AND OPS CHECK CARRIED OUT IAW AMM 32-61-03, OPS CHECK GOOD.</P>)
- [SDR UIEA2024022800135](https://openairdocs.org/sdr/UIEA2024022800135.md): Escape Reel · unknown · Feb 28, 2024 · N1181A · Boeing 7673Y0 · Emergency Equipment
  > ONE ESCAPE REEL REMOVED FROM AIRPLANE ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} INERTIAL ESCAPE REELS)(<P>REMOVED AND REPLACED ESCAPE REEL IAW AMM 25-61-04. NO FURTHER DEFECTS NOTED. THIS CLEARS MDDR 203776. PLACARDS REMOVED. MCC NO
- [SDR UIEA2024010800008](https://openairdocs.org/sdr/UIEA2024010800008.md): Escape Reel · unknown · Jan 9, 2024 · N1181A · Boeing 7673Y0 · Emergency Equipment
  > ONE INERTIA DESCENT REEL FELL OUT OF HOLDER AND UNWOUND ON CLIMBOUT(<P>REPLACED THE SECOND AFT INERTIA DESCENT REEL DEVICE IAW AMM 25-61-05. THIS CLEARS MDDR 200637. MCC NOTIFIED.</P>)
- [SDR UIEA2023121500998](https://openairdocs.org/sdr/UIEA2023121500998.md): Escape Reel · unknown · Dec 15, 2023 · N1181A · Boeing 7673Y0 · Emergency Equipment
  > ESCAPE REELS REQUIRE INSPECT/STOWING MULTIPLE UNLOCKED DURING TAKEOFF(<P>R/R INERTIAL ESCAPE REEL IAW AMM 25-61-05. OPS CHECK GOOD. DMI 199173 CLOSED.</P>)
- [SDR UIEA2023060800611](https://openairdocs.org/sdr/UIEA2023060800611.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT, FLOOR LEVEL, CORROSION ON FRAME WEB UPPER CHORD AT STA 654+44 LBL20(<P>AFFECTED ITEM WAS REPAIRED IAW B767 SRM 53-00-07-2R-4. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060700607](https://openairdocs.org/sdr/UIEA2023060700607.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Spoilers
  > LH INBD FLAP, SUPPORT RIB AT IFS 129 APPROX INNER SKIN WITH DENT(<P>AFFECTED AREA WAS REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060700606](https://openairdocs.org/sdr/UIEA2023060700606.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 632 AND STRINGER S-25LH(<P>AFFECTED AREA WAS REPAIRED PER TRE6753601 (IAI CUSTOMER SERVICE #CS-26206-003). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2023060700605](https://openairdocs.org/sdr/UIEA2023060700605.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 500 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2023060700604](https://openairdocs.org/sdr/UIEA2023060700604.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Main, Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2023060700603](https://openairdocs.org/sdr/UIEA2023060700603.md): Linkage · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Structure
  > VERTICAL STABILIZER REAR SPAR, UPPER PCA LINKAGE, RH HINGE WITH FREE PLAY(<P>UPPER PCA LINKAGE WAS REPLACED PER AMM 27-21-02-022-035 / -038. OPS CHECK GOOD</P>)
- [SDR UIEA2023060700602](https://openairdocs.org/sdr/UIEA2023060700602.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Aircraft Fuel System
  > FUEL LEAK AT BODY SPLICE OF STGR L-6 AND RBL 97.42, WING CENTER SECTION(<P> </P> / <P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER </SPAN><SPAN>L-6 AND RBL 97.42 WING CENTER SECTION </SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P>)
- [SDR UIEA2023060700601](https://openairdocs.org/sdr/UIEA2023060700601.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Aircraft Fuel System
  > FUEL LEAK AT BODY SPLICE OF STGR L-10 AND LBL 97.42, WING CENTER SECTION(<P><SPAN>FUEL LEAK AT BODY SPLICE OF STRINGER </SPAN><SPAN>L-10 AND LBL 97.42, WING CENTER SECTION </SPAN><SPAN>WAS REPAIRED AND TEST WAS SATISFACTORY</SPAN></P> / <P> </P>)
- [SDR UIEA2023060700600](https://openairdocs.org/sdr/UIEA2023060700600.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Aircraft Fuel System
  > FUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION(<P>FUEL LEAK AT BODY SPLICE OF STGR L-6 AND LBL 97.42, WING CENTER SECTION WAS REPAIRED AND TEST WAS SATISFACTORY.</P>)
- [SDR UIEA2023060700599](https://openairdocs.org/sdr/UIEA2023060700599.md): Pca · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Flight Control System
  > RUDDER UPPER PCA WITH FREE PLAY OUT OF LIMITS(<P>RUDDER UPPER PCA WAS REPLACED PER AMM 27-21-02-422-038. OPS CHECK GOOD</P>)
- [SDR UIEA2023060600595](https://openairdocs.org/sdr/UIEA2023060600595.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN SURFACE WITH CORROSION DAMAGE BETWEEN RBL13.833 / RBL 32.67 AND STGR 3.(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6755054 (BOEING SR 3-5632149492). NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2023060600594](https://openairdocs.org/sdr/UIEA2023060600594.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Vertical Stabilizer
  > VERTICAL STABILIZER, RH SURFACE, COMPOSITE PANEL DESBONDED BETWEEN AUXILIARY SPAR TO FRONT SPAR BETWEEN FSS 220.521 / FSS 321.046(<P>REPAIRED PER SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600593](https://openairdocs.org/sdr/UIEA2023060600593.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Main, Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 174.5 AND 5 INCH ABOVE OF STRINGER S-27LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2023060600592](https://openairdocs.org/sdr/UIEA2023060600592.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+44 / STA 654+66 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600591](https://openairdocs.org/sdr/UIEA2023060600591.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654+22 / STA 654+44 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600590](https://openairdocs.org/sdr/UIEA2023060600590.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 654 AND STRINGER S-25LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600589](https://openairdocs.org/sdr/UIEA2023060600589.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Main, Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 325 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600588](https://openairdocs.org/sdr/UIEA2023060600588.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Main, Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 412 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600587](https://openairdocs.org/sdr/UIEA2023060600587.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Main, Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 390 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600586](https://openairdocs.org/sdr/UIEA2023060600586.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Main, Structure
  > LIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 196.5 AND 8.5 INCH LOWER OF STRINGER S-21LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060600585](https://openairdocs.org/sdr/UIEA2023060600585.md): Hinge Fitting · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Structure
  > STABILIZERS - HORIZONTAL STABILIZER - RH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755055 REV 1. NO FURTHER DEFECTS N
- [SDR UIEA2023060600584](https://openairdocs.org/sdr/UIEA2023060600584.md): Hinge · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Structure
  > STABILIZERS - HORIZONTAL STABILIZER - LH HINGE FITTING BUSHING AND PIVOT BEARING CORROSION / SCRATCH DAMAGES(<P>THE HINGE FITTINGS WERE REPLACED / REPAIRED AND THE PIVOT FITTING WAS REWORKED WITH A SPECIAL TOOL PER MXA EO TRE6755056. NO FURTHER DEFECTS NOTED.
- [SDR UIEA2023060600583](https://openairdocs.org/sdr/UIEA2023060600583.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1562 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753595 REV 1 ISSUED ON MAY 15, 2023 (FVCI PROJECT NO. 23088-6). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500580](https://openairdocs.org/sdr/UIEA2023060500580.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE BEARSTRAP BETWEEN STA 1540 AND STRINGER S-10RH / S-11RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753594 ISSUED ON MAY 09, 2023 (FVCI PROJECT NO. 23088-5). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500579](https://openairdocs.org/sdr/UIEA2023060500579.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 654+110 AND STRINGER S-9RH / S-10RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753589 (FVCI PROJECT NO. 23088-7). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500578](https://openairdocs.org/sdr/UIEA2023060500578.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-14RH / S-15RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753590 ISSUED ON MAY 04, 2023 (FVCI PROJECT NO. 23088-1). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500577](https://openairdocs.org/sdr/UIEA2023060500577.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-12RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753591 (FVCI PROJECT NO. 23088-2). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500576](https://openairdocs.org/sdr/UIEA2023060500576.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-8RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753592 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-3). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500575](https://openairdocs.org/sdr/UIEA2023060500575.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Structure (General)
  > CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1480 / DSTA 876.3 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753593 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-4). NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500574](https://openairdocs.org/sdr/UIEA2023060500574.md): Panel · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > CORROSION ON PANEL UNDER ROLLER TRAYS BETWEENÂ STA 564+66 AND STA 564+88 FROMÂ FWD CARGO COMPARTMENT, FLOOR LEVEL.(<P>PANEL WAS REPLACED PER SRM 51-10-02-0G PAR.9. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500573](https://openairdocs.org/sdr/UIEA2023060500573.md): Unknown · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE ON FASTENER OF FUSELAGE EXTERNAL SKIN BETWEEN STA 566 AND STRINGERS S-27LH AND S-28LH.(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023060500572](https://openairdocs.org/sdr/UIEA2023060500572.md): Bushing · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Wing Structure
  > CORROSION ON BUSHINGS FROM RH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757194 (CMM 57-54-13 REPAIR 2-1)</P> / <P>MAJOR REPAIR PN: 113T1108-17 AND 113T1108-23</P>)
- [SDR UIEA2023060500571](https://openairdocs.org/sdr/UIEA2023060500571.md): Bushing · unknown · Jun 10, 2023 · N1181A · Boeing 7673Y0 · Wing Structure
  > CORROSION ON BUSHINGS FROM LH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757193 (CMM 57-54-13 REPAIR 2-1) MAJOR REPAIR. PN: 113T1108-17 AND 113T1108-23</P>)
- [SDR UIEA2023032400282](https://openairdocs.org/sdr/UIEA2023032400282.md): Hpc · unknown · Mar 24, 2023 · N1181A · Boeing 7673Y0 · Pneumatic System
  > ON TAXI OUT R ENG BLEED LIGHT AND EICAS MESSAGE ON FOLLOWED STEP 3 OF APPLICABLE DDG 36-11-02 LIGHT AND DID NOT CLEAR PER MCC GUIDANCE RH ENGINE TO 70 PERCENT AND MESSAGE DID NOT CLEAR(<P>REMOVED AND REPLACED THE RH ENGINE HIGH PRESSURE CONTROLLER IAW B767 AMM
- [SDR UIEA2023030300201](https://openairdocs.org/sdr/UIEA2023030300201.md): None · none · Mar 3, 2023 · N1181A · Boeing 7673Y0 · Cabin Equipment/Furnishings
  > ESCAPE REEL HANDLE FELL OUT AFTER LANDING(<P>R/R DESCENT DEVICE "B" IAW AMM 25-61-05. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023011100014](https://openairdocs.org/sdr/UIEA2023011100014.md): None · none · Jan 11, 2023 · N1181A · Boeing 7673Y0 · Standard Practices/Structures
  > DURING DEPARTURE IN CLIMB OUT, ACFT ENTERED AREA OF SEVERE TURBULENCE & W/S, ACFT INDICATED O/S OF 285, SPEED TAPE WITH NO ASSOCIATED OVERSPEED WARNINGS IAW 05-51-04, DATA FROM OUR ENGINEERING TEAM SHOWS AIRCRAFT DID NOT SHOW "G" LOADS OF SEVERE TURBULENCE. NO
- [SDR UIEA2022112101199](https://openairdocs.org/sdr/UIEA2022112101199.md): Guard · damaged · Nov 19, 2022 · N1181A · Boeing 7673Y0 · Emergency Lighting
  > EMERGENCY LIGHT GUARD INOP WITH GUARD CLOSED, EMER LIGHT REMAIN UNARMED. R/R EMERGENCY LIGHT GUARD IAW AMM 33-51-00. OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N1181A/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 = 'N1181A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N1181A/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.