Boeing 727-27

Aircraft model · Fixed wing multi engine · Airplane · registry code 138400K

Manufacturer (registry)
BOEING
Model
727-27
Registry code
138400K
Registered
0 aircraft
Type
Fixed wing multi engine
Engines
3 · Turbo-jet
Seats
134
Weight class
20,000 lb and over
Cruise speed
435 mph
Certification
Type certificated

Model codes come from the FAA registry’s reference file. ADs are matched to them by model name and maker.

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Airworthiness directives that may apply · 0

ADs whose products match this airframe model. Each AD’s applicability may narrow it by serial number, part number or configuration.

No ADs matched this model

Registered aircraft · 0

No aircraft currently registered with this model

NTSB investigations

No NTSB investigations matched to aircraft with this modelMatched through the registry by N-number, so foreign aircraft and some older cases aren’t counted.

FAA incident reports · 1

Matched to this model through the registry, by N-number and event date, checked against the reported make and model.

Query with SQL
duckdb -csv -c "SELECT report_number, event_date, event_type, city, state, aircraft_make, aircraft_model, aircraft_damage, fatal_injuries, n_number
  FROM 'https://openairdocs.org/data/latest/faa_incident_report.parquet'
  WHERE aircraft_model_code IN ('138400K')
  ORDER BY event_date DESC, report_number 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.

Service difficulty reports · 7

SDR C1HA200296002Bleed Valve · malfunctionedPOWER UP FOR TAKEOFF NR 2 ENGINE COMPRESSOR STALLED POWER WAS AT 1.6 EPR AND SPEED WAS BELOW 40 KTS. NR 2 PRBC WAS CHANGED AND OPS CHECK GOOD AND NR 2 GENERATOR PUT ON MEL. NR 2 COMP BLEED SYS OPS NORMAL REF: 75-31.Jan 6, 2002 · N696CA · Boeing 72727 · Compressor Bleed ValveSDR C1HA200296001Engine · malfunctionedON RUNWAY ADVANCED THROTTLE TO 1.4 CHECK PARAMETERS GOOD, CONTINUED THROTTLE ADVANCE FORFLEX POWER, LOUD BANG FROM NR 2 ENGINE, ENGINE FAIL LIGHT ILLUMINATED AND PACKS TRIPPED. ACCOMPLISHED THOROUGH EXAMINATION OF ENGINE NR 2 INTAKE AND EXHAUST WITH NO DAMAGEJan 6, 2002 · N696CA · Boeing 72727 · Engine (Turbine/Turboprop)SDR 98ZZZX2491Beam · corrodedDURING C-CHECK, EXFOLIATION CORROSION ON LEFT HORIZONTAL UPPER TRAILING EDGE BEAM BETWEEN STA 99.8 AND STA 136.5.Jun 2, 1998 · N16784 · Boeing 72727 · Horizontal Stabilizer StructureSDR 97FDEA00741Stringer · corrodedWHILE WORKING NR 0696 UPON REMOVAL OF STRINGER FROM BS 610 TO 624, STR 28 LT TO ACCESS KEEL BEAM CORROSION FOUND CORROSION IN BETWEEN SURFACES OF KEEL BEAM AND STRINGER. *S/D* MECHANICALLY REMOVED CORROSION ON STR 28 LT, BS 623, FOUND TO BE OUT OF LIMITS PEROct 14, 1997 · N146FE · Boeing 72727 · Fuselage Main, Longeron/StringerSDR 97FDEA00491Stringer · corrodedCORROSION (C53-224-012) ON STR 4 LT, BS 804 TO 870. *S/D* REPAIRED DAMAGED AREA OF STR 4 LT, BS 845 IAW FED-EX SRM 53-10-3.Jul 30, 1997 · N145FE · Boeing 72727 · Fuselage Main, Longeron/StringerSDR 96FDEA01414Acm · oil leakSMOKE IN CARGO COMPARTMENT. NOT RECOGNIZABLE ODOR. REQUIRED USE OF OXYGEN MASKS AND EMERGENCY DESCENT. FOUND OLD ACM LEAKING OIL AND BYPASSING INTERNALLY CAUSING SMOKE IN CARGO COMPARTMENT. REMOVED AND REPLACED RIGHT HAND A.C.M. PER MM 21-51 AS REQUIRED. Aug 27, 1996 · N145FE · Boeing 72727 · Cabin Cooling SystemSDR 96FDEA00242Skin · corrodedBS 720 O/B SIDE OF STR 28 RT, FUSELAGE SKIN IS BULGING. CUT OUT DAMAGE AREA 1 INCH BY 2 INCH AND INSTALLED DOUBLER PER SRM 51-0-6.Feb 1, 1996 · N494FE · Boeing 72727 · Fuselage Main, Plate/Skin
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 aircraft_model_key = '72727'
  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.