N79279

Service difficulty reports · 63

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N79279' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2011110700716Transmitter · faultyON APPROACH TO LGA FLAPS 5 SPEED 180 SELECTED GEAR DOWN FLAPS 15 FLAPS WOULD NOT EXTEND FURTHER THAN 5 NOR RETRACT, ALT FLAP EXTENSION WORKED NORMALLY. R&R RT FLAP POSITION XMITTER AS PER MM 27-58-01 OPS CHECK GOOD. PERFORMED LAND VERIFY A/C REMAINS CAT IIIANov 5, 2011 · N79279 · Boeing 737824 · Trailing Flap Position Indicating SystemSDR CALA2011021400088Skin · crackedLT STAB CRACK INDICATION NOTED STA 1.1.90, MEASURES 1 INCH LONG AND LOCATED 19 INCHES FROM L/E (FRONT SPAR). REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN AT STA 101.9 IAW EC/RA 5510-02149. ISSUED DIP TO PERFORM DV & LFEC, REF SRM 55-10-01 REPAIR 11 TABLE 204Feb 13, 2011 · N79279 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2011021400087Skin · crackedRT STAB CRACK INDICATION NOTED AT STA 138.70, MEASURES .5 INCH LONG AND LOCATED 17.5 INCHES FROM T/E AFT SPAR REPAIRED STA 138.7 AT 10 INCHES AND 17.5 INCHES REF LP6112346 & 6112347 PER SRM 55-10-01 REP 11 & ECRA5510-02150.. REF ATTACHED 44.0008 FOR WK ACCP.. Feb 13, 2011 · N79279 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2010012500016Light · inoperativeLEFT FWD OVERWING EMERGENCY EXIT LIGHT INOP EXTERIOR. RELAMPED LEFT OVERWING EMERGENCY SLIDE LIGHT IAW B737-800 AMM 33-51-04, OPS CHECKED GOOD IAW B737-800 AMM 33-51-04 WORK ACCOMPLISHED BY TIMCO.Jan 16, 2010 · N79279 · Boeing 737824 · Emergency LightingSDR CALA2009101300621Check Valve · inoperativeUNABLE TO KEEP PRESSURIZATION ON AIRCRAFT. QRH WAS RUN. PACKS HIGH, STILL NO CABIN PSI. USED APU AIR NO PSI COULD ONLY GET 1 TO 2 CABIN DIFF PRESS IN AUTO/ALT/MAN BLEED AIR FLEXING 35 TO 42 PSI. NO WARNING LIGHTS CAME ON ALT / OVERHEAT ETC. REMOVED AND REOct 12, 2009 · N79279 · Boeing 737824 · Air Distribution SystemSDR CALA2008111901086Intercostal · crackedFORMED INTERCOSTAL BETWEEN STA 328 AND 344 AT LBL46 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.Nov 17, 2008 · N79279 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA0801083Intercostal · crackedINTERCOSTAL BETWEEN STA 344 AND 360 AT BL 0 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SRM 51-40-02.Nov 17, 2008 · N79279 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA0801082Intercostal · crackedINTERCOSTAL BETWEEN STA 344 AND 360 AT LBL 11 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SRM 51-40-02.Nov 17, 2008 · N79279 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA0801081Intercostal · crackedINTERCOSTAL BETWEEN STA 312 AND 328 AT RBL 31 IS CRACKED AT FASTENER HOLE. REMOVED INTERCOSTAL, INSTALLED NEW INTERCOSTAL PER BOEING DOC 141A5400 AND SRM 51-40-02.Nov 16, 2008 · N79279 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA0801080Intercostal · crackedINTERCOSTAL BETWEEN STA 277 AND 294.5 AT BL 0 IS CRACKED. REMOVED INTERCOSTAL, INSTALLED NEW INTERCOSTAL PER BOEING DRAWING DOC 141A5400 AND SRM 51-40-02.Nov 16, 2008 · N79279 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA0801079Intercostal · crackedINTERCOSTAL BETWEEN STA 312 AND 328 AT LBL 45 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW INTERCOSTAL PER SRM 51-40-02.Nov 16, 2008 · N79279 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA0800799Threshold · corrodedFORWARD CARGO DOOR CUTOUT THRESHOLD PLATE LIFTING DUE TO CORROSION AT TOP CENTER SURFACE. REMOVED THRESHOLD PLATE AND CORNERS, REMOVED CORRODED WEB SECTION TRANSFER HOLES TO NEW WEB P/N 143A8122-10, INSTALLED WEB, RECEIVED OK TO INSTALL THRESHOLD PLATES. INSAug 22, 2008 · N79279 · Boeing 737800* · Fuselage Miscellaneous StructureSDR CALA0700165Module · inoperativeTHE FORWARD CARGO FIRE LIGHT ILLUMINATED ON CLIMBOUT FROM EWR AT 17,000 FEET. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FORWARD CARGO COMPARTMENT AND FOUND NO EVIDENCE OApr 3, 2007 · N79279 · Boeing 737800* · Fire Detection
Back to N79279