# Service difficulty reports: N429US, cancelled Sep 8, 2017 A list on [N429US, cancelled Sep 8, 2017](https://openairdocs.org/deregistered/N429US-2017-09-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAASB03099](https://openairdocs.org/sdr/USAASB03099.md): Charger · failed · Jul 3, 2003 · N429US · Boeing 7374B7 · Emergency Lighting > MAINTENANCE REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY EXIT LIGHT AT SEAT ROW 11, LEFT SIDE, ALONG WITH THE FLOOR PATH EMERGENCY LIGHTS FROM SEAT ROWS 7 THROUGH 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 2013-1A, AND CHARGER AS - [SDR USAASB02208](https://openairdocs.org/sdr/USAASB02208.md): Warning Light · illuminated · Nov 21, 2002 · N429US · Boeing 7374B7 · Engine Oil Indicating System > PBI - FLT 1246 - ON CLIMB-OUT FROM MIA, EN ROUTE TO PIT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW OPERATED THE NR 2 ENGINE AT REDUCED THRUST BUT THE LIGHT STILL FLICKERED OFF AND ON. FLIGHT DIVERTED - [SDR USAASB01249](https://openairdocs.org/sdr/USAASB01249.md): Downlock Sensor · Sep 8, 2001 · N429US · Boeing 7374B7 · Landing Gear System > SDF - FLT 1144 - IN PREPARATION FOR LANDING AT SDF, THE CREW RECEIVED A RIGHT MAIN LANDING GEAR UNSAFE LIGHT DURING GEAR EXTENSION. CAPTAIN ACCOMPLISHED A FLYBY AT SDF TOWER FOR VISUAL THAT GEAR WAS DOWN. TOWER CONFIRMED GEAR WAS DOWN. CAPTAIN ALSO REPORTED - [SDR USAA010763](https://openairdocs.org/sdr/USAA010763.md): Skin · cracked · Jun 28, 2001 · N429US · Boeing 7374B7 · Fuselage Structure (General) > CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-60-03. (M) - [SDR USAA010472](https://openairdocs.org/sdr/USAA010472.md): Bulkhead · cracked · Apr 27, 2001 · N429US · Boeing 7374B7 · Fuselage Main, Bulkhead > CLT - FOUND PRESSURE WEB WITH 5 CRACKS, TWO.250 INCH, TWO.150 INCH AND ONE.100 INCH, BS 178, WL 195, 198, 201.5, 206.6; LBL 5 TO RBL 7. DAMAGE CUTOUT, REPAIR DOUBLER INSTALLED PER EO 5300V153 AND EA 69566. (M) - [SDR USAA000712](https://openairdocs.org/sdr/USAA000712.md): Skin · cracked · May 15, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED.250 INCH, EXT SKIN AFT ENTRANCE DOOR LOWER HINGE UPPER CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01. (M) - [SDR USAA000701](https://openairdocs.org/sdr/USAA000701.md): Frame · cracked · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 440, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000699](https://openairdocs.org/sdr/USAA000699.md): Frame · cracked · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 787, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000698](https://openairdocs.org/sdr/USAA000698.md): Frame · cracked · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 440, STRINGER 8R. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000697](https://openairdocs.org/sdr/USAA000697.md): Frame · cracked · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED 1 INCH, BS 296, STRINGER 17R FORWARD SERVICE DOOR CUTOUT. INSTALLED DOUBLER AND FILLER ANGLE PER SRM 51-70-11. (M) - [SDR USAA000696](https://openairdocs.org/sdr/USAA000696.md): Frame · cracked · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED 2 INCHES, BS 601 RT, WL 202. INSTALLED STIFFENER AND FILLER PER EA 67119. (M) - [SDR USAA000703](https://openairdocs.org/sdr/USAA000703.md): Floor Support · corroded · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Miscellaneous Structure > CLT - FOUND FLOOR SUPPORT BEAM CORRODED 1 INCH BY 2 INCH, 9 INCHES INBOARD OF AFT ENTRY DOOR STATION 986.5. INSTALLED NEW T-CAP PER TR 53-60-01. CORROSION LEVEL 2. (M) - [SDR USAA000700](https://openairdocs.org/sdr/USAA000700.md): Frame · cracked · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 747, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M) - [SDR USAA000695](https://openairdocs.org/sdr/USAA000695.md): Floorbeam · corroded · May 11, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 70 INCHES, FS 328 BETWEEN RBL 56 AND RBL 14. INSTALLED NEW T-CAP PER SRM 53-10-51. CORROSION LEVEL 2. (M) - [SDR USAA000668](https://openairdocs.org/sdr/USAA000668.md): Skin · cracked · May 4, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED.25 INCH, OUTBOARD EDGE OF PANEL 5727L CUTOUT. INSTALLED DOUBLER PER TR 54-30-07. (M) - [SDR USAA000655](https://openairdocs.org/sdr/USAA000655.md): Floor Support · corroded · May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Miscellaneous Structure > CLT - FOUND FLOOR SUPPORT CORRODED, RIGHT AFT DOOR Z-ANGLE. LEVEL 1 CORROSION. INSTALLED DOUBLER PER SRM 51-70-11. (M) - [SDR USAA000656](https://openairdocs.org/sdr/USAA000656.md): Floorbeam · corroded · May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Floor Beam > CLT - FOUND BEAM CRACKED 2 INCHES BY 55 INCHES, NUMEROUS CORROSION LEVEL 2, FLOORBEAM AT FS 344 BETWEEN RBL 11 AND LBL 44. INSTALLED NEW T-CAP AND SPLICE PER SRM 53-10-51. (M) - [SDR USAA000657](https://openairdocs.org/sdr/USAA000657.md): Angle · corroded · May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Miscellaneous Structure > CLT - FOUND Z-ANGLE CORRODED.250 INCH BY.250 INCH, FORWARD SERVICE DOOR JAM. INSTALLED NEW Z-ANGLE PER SRM 53-10-13. (M) - [SDR USAA000658](https://openairdocs.org/sdr/USAA000658.md): Frame · cracked · May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED 2 INCHES, BS 601 LT AT WL 202. INSTALLED DOUBLER PER EA 67119 AND TR 53-62-01. (M) - [SDR USAA000659](https://openairdocs.org/sdr/USAA000659.md): Bulkhead · cracked · May 1, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Bulkhead > CLT - FOUND WEB CRACKED 1 INCH, 178 BULKHEAD, LBL 5.7 AND WL 202 AND 199. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M) - [SDR USAA000612](https://openairdocs.org/sdr/USAA000612.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 727D, STRINGER 8 RT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000613](https://openairdocs.org/sdr/USAA000613.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 727D, STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000614](https://openairdocs.org/sdr/USAA000614.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 380 STRINGER 8 RIGHT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000615](https://openairdocs.org/sdr/USAA000615.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 380 STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000616](https://openairdocs.org/sdr/USAA000616.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 400 STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000617](https://openairdocs.org/sdr/USAA000617.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 867, STRINGER 8 LEFT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000618](https://openairdocs.org/sdr/USAA000618.md): Frame · cracked · Apr 28, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.25 INCH, BS 907 STRINGER 8 RIGHT. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA000423](https://openairdocs.org/sdr/USAA000423.md): Skin · cracked · Mar 21, 2000 · N429US · Boeing 7374B7 · Fuselage Main, Plate/Skin > CLT - FOUND FUSELAGE SKIN CRACKED 1 INCH, LEFT SIDE FUSELAGE AFT OF LT WING BODY FAIRING. REPAIRED DOUBLER AND FILLER PER TR 53-60-03. (M) - [SDR USAASB00031](https://openairdocs.org/sdr/USAASB00031.md): Circuit Breaker · tripped · Feb 2, 2000 · N429US · Boeing 7374B7 · Landing Gear Position and Warning > BOS - FLT 2030 - CREW RECEIVED A GEAR INDICATION WARNING FOR THE NOSE GEAR WHILE PREPARING TO LAND AT BOS. CAPTAIN ACCOMPLISHED A FLYBY THE TOWER TO VERIFY THE GEAR WAS DOWN. AFTER CONFIRMATION, CREW ALSO VERIFIED THE NOSE GEAR WAS DOWN THROUGH THE VIEWFINDE - [SDR USAA991425](https://openairdocs.org/sdr/USAA991425.md): Skin · cracked · Dec 18, 1999 · N429US · Boeing 7374B7 · Passenger/Crew Doors > TPA - DURING AC-5 CHECK VISUAL INSPECTION, FOUND THE DOOR SKIN BENT AND CRACKED JUST ABOVE LOWER HINGE CUTOUT. REPAIRED PER EA 66130. (M) - [SDR USAASB98302](https://openairdocs.org/sdr/USAASB98302.md): Light · inoperative · Nov 15, 1998 · N429US · Boeing 7374B7 · Emergency Lighting > TPA - MAINTENANCE FOUND THE FORWARD ENTRY EGRESS EMERGENCY LIGHT AND THE RIGHT AFT FUSELAGE EGRESS EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR ASSEMBLIES AT BOTH LOCATIONS. OPERATIONAL CHECK GOOD. (M) - [SDR USAA980549](https://openairdocs.org/sdr/USAA980549.md): Skin · cracked · Oct 19, 1998 · N429US · Boeing 7374B7 · Horizontal Stabilizer, Plate/Skin > TPA - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK ELEVATOR STATION 81.54 AT STAB STATION 67.54 HORIZ STAB SKIN. CUTOUT CRACK AND INSTALLED DOUBLER PER TR 55-10-07. (M) - [SDR USAA980525](https://openairdocs.org/sdr/USAA980525.md): Skin · cracked · Oct 19, 1998 · N429US · Boeing 7374B7 · Horizontal Stabilizer, Plate/Skin > TPA - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK ELEV STATION 51-54 AT STAB STATION 67.54 HORIZONTAL STABILIZER SKIN. CUTOUT CRACK AND INSTALLED DOUBLER PER TR 55-10-07. (M) - [SDR USAASB97011](https://openairdocs.org/sdr/USAASB97011.md): Battery Pack · discharged · Jan 8, 1997 · N429US · Boeing 7374B7 · Emergency Lighting > CLE - MX FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) - [SDR usaasb96139](https://openairdocs.org/sdr/usaasb96139.md): Coalescer Bag · failed · Jul 25, 1996 · N429US · Boeing 7374B7 · Humidity Control System > DEN-PIT - FLT 132 - CREW REPORTED A SMOKE TYPE SMELL IN THE COCKPIT AND FORWARD CABIN. SMELL IS STRONGEST IN THE COCKPIT. HAPPENS AT DIFFERENT FLIGHT CONDITIONS. SUSPECT LEFT PACK. MAINTENANCE REPLACED THE LEFT PACK SECONDARY (REAR) WATER EXTRACTOR. RAN P - [SDR USAASB96116](https://openairdocs.org/sdr/USAASB96116.md): Fan · failed · Jun 25, 1996 · N429US · Boeing 7374B7 · Air Distribution Fan > MCO - FLT 1981 - ON DESCENT TO MCO, CREW NOTICED A VERY STRONG ODOR. SMELLED LIKE HYDRAULIC FLUID ON A HOT DUCT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING RECIRCULATING FAN. OPS - [SDR USAA950759](https://openairdocs.org/sdr/USAA950759.md): Circuit Breaker · failed · Jul 20, 1995 · N429US · Boeing 7374B7 · Landing Gear Position and Warning > LGA - FLT 2235 - THE 'NOSE GEAR UNSAFE' LIGHT ILLUMINATED WHEN THE POWER WAS BROUGHT TO IDLE. VISUALLY VERIFIED GEAR POSITION AND PERFORMED TOWER FLYBY. FLIGHT CREW FOUND AIR/GRD RELAY AND LANDING GEAR LIGHTS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. ## 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 = 'N429US' AND deregistration_id = 'N429US-2017-09-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N429US-2017-09-08/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.