# Boeing 737-2T7 - Type: Aircraft model (FAA registry) - Registry code: 1384482 - Manufacturer (registry): BOEING - Model: 737-2T7 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 149 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-737-2t7 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19840723041819I](https://openairdocs.org/incident/19840723041819I), Jul 23, 1984: Boeing 7372A9C (N131AW), Phoenix, AZ, Minor damage. Ramp agent directed aircraft into a parked baggage cart. No wing walker. ## Service difficulty reports (23) As reported by operators and repair stations, by the model named in the report. - [SDR CA030505003](https://openairdocs.org/sdr/CA030505003), May 3, 2003: WINDOW. CRACKED. (CAN) F/O,S NR 1 WINDOW OUTER (POSS MIDDLE) PANE CRACKED AT 31000 WINDOW SLOWLY DELAMINATED AND AFTER WE TURNED HEAT OFF WINDOW CRACKED. WINDOW REPALCED AS PER - [SDR CA030327003](https://openairdocs.org/sdr/CA030327003), Mar 12, 2003: BEARING. FAILED. (CAN) DURING CLIMB IN MANUAL FLIGHT , BEOND 5 DEG. LT WHEEL DEFLECTION AILERONS FELT VERY HEAVY 9 AS IF IN MANUAL REVERSION ) AT THIS POINT IN TIME RUDDER TRIM - [SDR CA020731013](https://openairdocs.org/sdr/CA020731013), Jul 9, 2002: CONTROL CABLE. FAILED. (CAN) NR 5 FLAP ACTUATOR ROLLER TRACK DISENGAGED AND WENT THROUGH THE INBOARD SIDE OF NR 5 FLAP FAIRING. NR 5 FLAP TRACK FITTING FOUND DAMAGED (SNAPPED) DUE BOO - [SDR CA020725004](https://openairdocs.org/sdr/CA020725004), Jun 4, 2002: WINDSHIELD. ARCED. (CAN) FIRST OFFICER NR 1 WINDSHIELD ARCING, UPPER MID SECTION DISCOLOURED BY WIRING LEADS REPLACED WINDSHIELD - [SDR CA010924006](https://openairdocs.org/sdr/CA010924006), Sep 9, 2001: ACTUATOR. FAILED. (CAN) ON DEPARTURE YYZ ATTEMPTED FORWARD HORIZONTAL STAB TRIM USING CONTROL WHEEL SWITCHES. NO FORWARD TRIM AVAILABLE, FULL AFT TRIM OK. AUTO PILOT SEEMED ABLE - [SDR CA010924004](https://openairdocs.org/sdr/CA010924004), Aug 24, 2001: CONNECTOR. FAILED. (CAN) ON APPROACH TO YVR NR 2 ENGINE FIRE WARNING INDICATED. BOTH FIRE BOTTLE FIRE DISCHARGED. FIRE WARNING REMAINED ILLUMINATED. NO EXTERNAL EVIDENCE OF FIRE O - [SDR CA010910009](https://openairdocs.org/sdr/CA010910009), Aug 10, 2001: SEAL. LEAKING. (CAN) NR 2 LOW OIL PRESSURE FLICKERING FOR THE LAST 4 MINUTES OF FLIGHT WITH THE PRESSURE GAUGE IN AND OUT OF CAUTION RANGE. TEMPERATURE NORMAL, ENGINE OPERATED - [SDR CA010910008](https://openairdocs.org/sdr/CA010910008), Aug 9, 2001: RELAY. FAILED. (CAN) DURING SRVICE CHECK, WITH NO A/C POWER & BATTERY SELECTED TO DC, THE AMP METER WENT TO 40 AMPS, AFTER APU START, THE D.C. AMPS METER STOCKED AT 100 AMPS. - [SDR CA000110017](https://openairdocs.org/sdr/CA000110017), Dec 20, 1999: FITTING. DAMAGED. (CAN) REMOVED FITTING FOR BEARING REWORK AND FOUND HIDDEN DAMAGE. THREE OF FOUR BOLTS FROZEN IN BORES, TWO BOLTS SHEARED, EVIDENCE OF EXTENSIVE CORROSION TO SHE - [SDR CA000110016](https://openairdocs.org/sdr/CA000110016), Dec 20, 1999: WINDOW POST. CRACKED. (CAN) INSP REVEALED CRACKS OF C-D WINDOW POST UPPER OTBD CORNERS OF LT AND RT WINDOWS. ROUTED OUT TO REVEAL UNDER SKIN ALSO CRACKED FROM SITE MARKS. REPAIRED PE - [SDR CA990416013](https://openairdocs.org/sdr/CA990416013), Mar 30, 1999: TRUNNION. DAMAGED. (CAN) FOUND MLG OUTER TRUNNION ATTACHMENT LINK SHEARED. GEAR REPLACED. - [SDR CA990416007](https://openairdocs.org/sdr/CA990416007), Mar 25, 1999: PCU. FAILED. (CAN) PILOT REPORTED VIBRATION THROUGHOUT THE AIRCRAFT WITH B-PUMPS ON. RUDDER OBSERVED TO OSCILLATE 1 TO 1.5 INCH RANGE, RUDDER FUNCTIONED, VIBRATION QUIT. RUD - [SDR CA990330008](https://openairdocs.org/sdr/CA990330008), Mar 4, 1999: TIRE. FAILED. (CAN) NR 4 TIRE TREAD SEPARATED AND FRAGMENTS DAMAGED. THE RIGHT INBOARD FLAP, REPLACED. - [SDR CA990310057](https://openairdocs.org/sdr/CA990310057), Jan 23, 1999: FRAME. CORRODED. (CAN) DURING INSPECTION OF FUSELAGE DENT, THE FORWARD LEFT LAVATORY WAS REMOVED FOR ACCESS. THE CHORD AT STA 245 AND STA 260 FOUND CORRODED, REPLACED. - [SDR CA980317039](https://openairdocs.org/sdr/CA980317039), Mar 16, 1998: VALVE. DIRTY. (CAN) AT TAKEOFF, PRESSURIZATION SYSTEM AUTO FAIL LIGHT CAME ON. THROUGH 5,000 FEET, RESET SYSTEM AND OPERATED NORMALLY FOR REST OF FLIGHT. OUTFLOW VALVE REPLAC - [SDR CA971113019](https://openairdocs.org/sdr/CA971113019), Oct 27, 1997: HOSE ASSEMBLY. RUPTURED. (CAN) AIRCRAFT DIVERTED DUE TO EXCESSIVE LEAKAGE IN CREW OXYGEN SYSTEM. HOSE RUPTURED. REPLACED. - [SDR CA970922016](https://openairdocs.org/sdr/CA970922016), Aug 28, 1997: CSD. FAILED. (CAN) CLIMBING THROUGH 8000 FEET, THE NR2 GENERATOR "HIGH OIL TEMPERATURE LIGHT" CAME ON. COMPLETED CHECK LIST AND SHUTDOWN CONSTANT SPEED DRIVE (CSD) AND START - [SDR CA970904011](https://openairdocs.org/sdr/CA970904011), Aug 13, 1997: STROBE. BURNT. (CAN) AIRCRAFT DIVERTED DUE TO SMOKE IN CABIN. UPPER ANTI COLLISION BEACON BURNT OUT. CIRCUIT BREAKER PULLED AND COLLARED. TERMINAL STRIP CHECKED FOR ARCING. - [SDR CA961216002](https://openairdocs.org/sdr/CA961216002), Dec 6, 1996: DETECTOR. DAMAGED. (CAN) ON CLIMB #2 ENGINE FIRE WARNING, AIRCRAFT RETURNED, FIRE WARNING STAYED ON FOR SEVERAL SECONDS, ENGINE SHUT DOWN AND FIRE BOTTLE FIRED. CONDITION REMAINED - [SDR CA960925005](https://openairdocs.org/sdr/CA960925005), Sep 13, 1996: GYRO. JAMMING. (CAN) F/OS A.D.I. HORIZON CARD KEEPS JAMMING. VG CHANGED AND RESET OF C/B HAD NO EFFECT. F/OS A.D.I. AND GYRO REPLACED. #2 VG TRANSFER RELAY REPLACED AS PER MAI - [SDR CA960723003](https://openairdocs.org/sdr/CA960723003), Jul 18, 1996: STRUCTURE. DAMAGED. (CAN) AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED. EXTENSIVE DAMAGE TO LEADING EDGES, HORIZONTAL STAB, VERTICAL STAB, RADOME, #1 WINDSHIELD CRACKED. ALL SLATS R - [SDR CA960625001](https://openairdocs.org/sdr/CA960625001), Jun 19, 1996: SEAL. LEAKING. (CAN) AIRCRAFT DIVERTED DUE TO LOSS OF HYDRAULIC FLUID. ATTENUATOR SEAL REPLACED. - [SDR CA960604016](https://openairdocs.org/sdr/CA960604016), May 20, 1996: SEAL. LEAKING. (CAN) AFTER TAKEOFF WITH THE LANDING GEAR AND FLAPS UP, THE HYDRAULIC QUANTITY WAS 3.0 GALLONS. ONE HOUR INTO FLIGHT HYDRAULIC QUANTITY WAS 1.8 GALLONS. SEVENTE --- 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.