# Boeing 757-2G7 - Type: Aircraft model (FAA registry) - Registry code: 1384963 - Manufacturer (registry): BOEING - Model: 757-2G7 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 178 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-757-2g7 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 (1) - [N910AW](https://openairdocs.org/aircraft/N910AW): [Sundown Aircraft LLC](https://openairdocs.org/faa-owner/SUNDOWN%20AIRCRAFT%20LLC), [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville), built 1989, S/N 24523 ## NTSB investigations (3) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX00LA146](https://openairdocs.org/ntsb/LAX00LA146), Apr 3, 2000: Boeing 757-2G7 (N910AW), Dallas, TX, no damage. Probable cause: The en route cruise encounter with forecast moderate turbulence. - [NTSB LAX00LA072](https://openairdocs.org/ntsb/LAX00LA072), Jan 12, 2000: Boeing 757-2G7 (N909AW), Las Vegas, NV, no damage. Probable cause: Encounter with Clear Air Turbulence. Poor communication between the captain and flight attendants as to the urgency for the flight attendants to take their seats was a contributing factor. - [NTSB LAX99LA322](https://openairdocs.org/ntsb/LAX99LA322), Jul 24, 1999: Boeing 757-2G7 (N910AW), Phoenix, AZ, substantial damage. Probable cause: The failure of the flight crew and the tug driver to verify that the aircraft was properly configured for pushback. Factors in the accident were the left wing walker's failure to notify the tug… ## FAA accident and incident reports (6) 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 20100917046029I](https://openairdocs.org/incident/20100917046029I), Sep 17, 2010: Boeing 757-2G7 (N908AW), San Francisco, CA, Minor damage. Us airways, flight 432 from phoenix, AZ (phx) to maui, hi (ogg) diverted to San Francisco, CA due to smoke in the cabin and flight deckaircraft at cruise just… - [Incident 20030426009729I](https://openairdocs.org/incident/20030426009729I), Apr 26, 2003: Boeing 7572G7 (N908AW), Ontario, CA, Minor damage. (-23) America west airlines flight 35 from phoenix, AZ (phx) to los angeles, CA (lax) while cruising at FL350 had the captains windshield crack in a pattern… - [Incident 20010925025709I](https://openairdocs.org/incident/20010925025709I), Sep 25, 2001: Boeing 7572G7 (N908AW), Kansas City, MO. (-23) On September 25, 2001, at 1256 CDT, america west flt. 807 a B757, N908AW, enroute from bwi to phx diverted to Kansas City International Airport, Kansas… - [Accident 20000402006529A](https://openairdocs.org/incident/20000402006529A), Apr 2, 2000: Boeing 7572G7 (N910AW), Las Vegas, NV, No damage. (-23) Awe 563 B757-200, 910AW, orlando, FL. To Las Vegas encountered severe turbulence at FL350 over abilene, TX at 022100 PDT. 190 passengers, no injuries.… - [Accident 20000111006349A](https://openairdocs.org/incident/20000111006349A), Jan 11, 2000: Boeing 7572G7 (N909AW), Las Vegas, NV, No damage. (-23) While in cruise flight at FL 350 in the vicinity of alamosa, CO. The flight crew received reports from ATC of light to moderate chop in their flight… - [Incident 19940601023119I](https://openairdocs.org/incident/19940601023119I), Jun 1, 1994: Boeing 757225 (N909AW), St Louis, MO, Minor damage. Fire warning right engine. Shut down. Used fire bottles. Engine fuel nozzle loose. Leaked fuel. Cowl wiring damaged. ## Service difficulty reports (502, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR AALA201609029015](https://openairdocs.org/sdr/AALA201609029015), Sep 1, 2016: SLIDE. LOW PRESSURE. AIRCRAFT WAS GROUNDED, R4 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED R4 DOOR SLIDE TASK CARD 19L80025002. - [SDR AALA201608299005](https://openairdocs.org/sdr/AALA201608299005), Aug 28, 2016: SLIDE. DISLODGED. AIRCRAFT WAS NOT GROUNDED: CABIN SERVICE REPORTS L4 DOOR HARD TO CLOSE. FOUND SLIDE PACK TO BE DISLODGED. SAFETY PIN INSTALLED ON INFLATION CYLINDER, REINSTALLE - [SDR AALA201606289003](https://openairdocs.org/sdr/AALA201606289003), Jun 27, 2016: CONTROL VALVE. DEFECTIVE. AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A RT ENGINE BLEED OFF EICAS MESSAGE AND A RT ENGINE BLEED EICAS MESSAGE DURING TAKEOFF ROLL AND ABORTED THE TAKEOFF - [SDR AALA201604289010](https://openairdocs.org/sdr/AALA201604289010), Apr 27, 2016: FLASHLIGHT. INOPERATIVE. AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANTS FLASHLIGHT AT 1L DOOR INOPERATIVE. REPLACED FLASHLIGHT & ACCOMPLISHED AS SATISFACTORY OPERATIONAL CHECK IAW AMM 25-60- - [SDR AALA201604199008](https://openairdocs.org/sdr/AALA201604199008), Apr 18, 2016: EEC. DEFECTIVE. AIRCRAFT WAS GNDED. RT ENG SLOW TO ACCELERATE TO TAKEOFF POWER. TARGET EPR 1071 RT ENG STOPPED ACCELERATING AT 1.65 EPR. MANUALLY SET 1.71 EPR. REPLACED THE RT - [SDR AALA201604169002](https://openairdocs.org/sdr/AALA201604169002), Apr 15, 2016: WIRE HARNESS. DEFECTIVE. AIRCRAFT WAS NOT GNDED. EMER PATH LIGHT INOPERATIVE AT ROW 22. REPLACED ROW 22ABC EMER LIGHT PATH HARNESS & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AM - [SDR AALA201603299007](https://openairdocs.org/sdr/AALA201603299007), Mar 28, 2016: UNKNOWN. ODOR. AIRCRAFT WAS GNDED. DURING DESCENT THE AFT CABIN FLIGHT ATTENDANT REPORTED SMELL OF SMOKE, NO SOURCE FOUND. DISAPPEARED AFTER 30 SECONDS. DECLARED AN EMER & LAN - [SDR AALA201603219002](https://openairdocs.org/sdr/AALA201603219002), Mar 17, 2016: CONTROL LEVER. DEFECTIVE. AIRCRAFT WAS GNDED. DURING THE APPROACH, THE GEAR DISAGREE LIGHT ILLUMINATED & THE CREW PERFORMED A GO AROUND & ACCOMPLISHED THE QRH CHECKLIST. THE ACFT LANDED - [SDR AALA201603159019](https://openairdocs.org/sdr/AALA201603159019), Mar 14, 2016: FLASHLIGHT. DEFECTIVE. AIRCRAFT WAS NOT GNDED. AFT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT. - [SDR AALA201602229020](https://openairdocs.org/sdr/AALA201602229020), Feb 19, 2016: LIGHT. INOPERATIVE. AIRCRAFT WAS NOT GNDED. R3 DOOR SLIDE LIGHTS DID NOT COME ON DURING INFLATION SDR REQUIRED. REPLACED SLIDE IAW TASK CARD 19L83525001. - [SDR AALA201602229019](https://openairdocs.org/sdr/AALA201602229019), Feb 19, 2016: SLIDE. FAILED. L1 SLIDE DID NOT DEPLOY DURING TEST. REPLACED SLIDE IAW TASK CARD 18L80025002. - [SDR AALA201602229014](https://openairdocs.org/sdr/AALA201602229014), Feb 18, 2016: PROXIMITY SENSOR. LOOSE. AIRCRAFT WAS NOT GNDED. DOOR L1 FWD SLIDE, ARMED INDICATION PROXIMITY SENSOR S10214 LOOSE. REPLACED L1 DOOR GIRT BAR PROXIMITY SENSOR IAW TR25-017AW. SYS OPERAT - [SDR AALA201602199002](https://openairdocs.org/sdr/AALA201602199002), Feb 18, 2016: LENS. BROKEN. AIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER LIGHT LENS BROKEN AT SEAT 33ABC. REPLACED LENS AT SEAT 33ABC. - [SDR AALA201602169005](https://openairdocs.org/sdr/AALA201602169005), Feb 15, 2016: SLIDE. UNSECURE. AIRCRAFT WAS GNDED. L1 DOOR SLIDE ASSEMBLY FELL OUT OF DOOR, DID NOT DEPLOY. REPLACED L1 DOOR SLIDE IAW TASK CARD 19L80025002. - [SDR AALA201602159004](https://openairdocs.org/sdr/AALA201602159004), Feb 12, 2016: WIRE HARNESS. DAMAGED. RETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, R ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS - [SDR AALA201602159003](https://openairdocs.org/sdr/AALA201602159003), Feb 12, 2016: DETECTOR. DEFECTIVE. RETURNED, ACFT WAS GNDED. CREW NOTED A STATUS MSG, RT ENG OH LP1, RESULTING IN THE ACFT RETURNING WHERE IT LANDED SAFELY WITH NO INCIDENTS REPORTED. NO EMER WAS - [SDR AALA201512189003](https://openairdocs.org/sdr/AALA201512189003), Dec 17, 2015: WARNING LIGHT. FALSE ACTIVATION. GEAR DISAGREE MESSAGE & FWD LIGHT APPEARED DURING GEAR EXTENSION. ABORTED APPROACH. RETRACTED GEAR, DURING GO AROUND MSG WENT OUT & DID NOT REAPPEAR. PREFORMED - [SDR AALA201512169005](https://openairdocs.org/sdr/AALA201512169005), Dec 15, 2015: CONNECTOR. DISCONNECTED. SEAT MOUNTED EMERGENCY LIGHT AT SEAT 18C INOPERATIVE. CONNECTED LOOSE CONNECTOR AT 18C. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA201512169001](https://openairdocs.org/sdr/AALA201512169001), Dec 15, 2015: WIRE HARNESS. DAMAGED. SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13C INOPERATIVE. REPAIRED HARNESS AT 13C. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA201511239006](https://openairdocs.org/sdr/AALA201511239006), Nov 20, 2015: BATTERY. DISCHARGED. FLASHLIGHT AT L2 DOOR INOPERATIVE, NO FLASHING RED INDICATOR. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA201510159009](https://openairdocs.org/sdr/AALA201510159009), Oct 13, 2015: SLAT. DELAMINATED. LEFT WING NR 4 SLAT HAS DELAMINATION AT INBD TE BOTTOM SIDE. REPLACED SLAT IAW 19L52027002. - [SDR AALA201510159008](https://openairdocs.org/sdr/AALA201510159008), Oct 13, 2015: SLAT. DELAMINATED. RIGHT WING NR 8 SLAT HAS DELAMINATION AT PREVIOUS REPAIRS, 3 EACH, AREA 1. APPROX 70" FROM INBD EDGE. AREA 2, 19" FROM INBD EDGE. AREA 3, 13" FROM OTBD END & 2" - [SDR AALA201509309011](https://openairdocs.org/sdr/AALA201509309011), Sep 28, 2015: WIRE. BROKEN. FLIGHT 583 SEAT MOUNTED EMER LIGHT INOPERATIVE AT SEAT 19C. FOUND WIRE BROKEN. R & R SEAT MOUNTED EMER LIGHT ASSEMBLY AT SEAT 19C. OPERATIONAL CHECKED GOOD. - [SDR AALA201508149001](https://openairdocs.org/sdr/AALA201508149001), Aug 13, 2015: FLASHLIGHT. INOPERATIVE. AFT GALLEY FLIGHT ATTENDANT EMER FLASHLIGHT NO LED FLASH. REPLACED FLASHLIGHT. - [SDR AALA201507069001](https://openairdocs.org/sdr/AALA201507069001), Jul 3, 2015: LATCH. OUT OF ADJUST. FORWARD LAVATORY O2 DOOR LATCH ACTUATOR FAILED TEST, COULD NOT RESET. ADJUSTED LATCH MECHANISM AS REQUIRED. OPERATIONS OK. - [SDR AALA201506059009](https://openairdocs.org/sdr/AALA201506059009), Jun 2, 2015: PIN. WORN. NOSE LANDING GEAR RT TRUNNION PIN WORN. REPLACED TRUNNION PIN. - [SDR AALA201506059008](https://openairdocs.org/sdr/AALA201506059008), Jun 2, 2015: PIN. WORN. NOSE LANDING GEAR LT TRUNNION PIN WORN. REPLACED TRUNNION PIN. - [SDR AALA201505229005](https://openairdocs.org/sdr/AALA201505229005), May 21, 2015: MODULE. FAULTY. FLIGHT 663 EN-ROUTE, EICAS MSG & AUDIO ALARM. GEAR NOT DOWN RED CONFIGURATION LIGHT, RED WARNING LIGHT ON GLARE SHIELD. GEAR HANDLE UP & OFF, NO CHANGE. PRESSED - [SDR AALA201504229008](https://openairdocs.org/sdr/AALA201504229008), Apr 21, 2015: LIGHT. INOPERATIVE. ROW 26 LT EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT 26 LT EMERGENCY LIGHT. - [SDR AALA201504149030](https://openairdocs.org/sdr/AALA201504149030), Apr 11, 2015: ACCESS PANEL. CRACKED. RIGHT WING FUEL ACCESS PANEL 641GB CRACKED & LEAKING FUEL. REPLACED RT WING FUEL ACCESS PANEL 641GB IAW AMM 28-11-00. LEAK CHECKED GOOD. - [SDR AALA201504209016](https://openairdocs.org/sdr/AALA201504209016), Apr 10, 2015: SHEAR TIE. CRACKED. C4 CHECK, L4 DOOR FUSELAGE UPPER LOBE INTERIOR FRAME & SKIN SHEAR TIE HAS 0.5 INCH CRACK NEXT TO RADIUS AT STATION 1661 BETWEEN STRINGER 5L & 6L. R & R SHEAR TI - [SDR AALA201504209015](https://openairdocs.org/sdr/AALA201504209015), Apr 10, 2015: STRINGER. CRACKED. C4 CHECK, STRINGER AT STRINGER 13R CRACKED AT BS 619. REPAIRED CRACKED STRINGER IAW EA 250005. - [SDR AALA201505049005](https://openairdocs.org/sdr/AALA201505049005), Apr 8, 2015: INTERCOSTAL. CRACKED. C4 CHECK, CRACK IN INTERCOSTAL BETWEEN STATION 680 & 685 BELOW STRINGER 11L, FWD OF L2 DOOR IN RADIUS NEXT TO SKIN. R & R CRACKED INTERCOSTAL IAW SRM 51-10-02 & - [SDR AALA201505049004](https://openairdocs.org/sdr/AALA201505049004), Apr 5, 2015: SUPPORT ANGLE. CRACKED. C4 CHECK, FLOORBOARD SUPPORT ANGLE CRACKED BETWEEN STATION 780 & 800 AT BL 0. FABRICATED & INSTALLED NEW ANGLE IAW DWG 143N5140.040 7075 T6 FROM BAC1493-412. - [SDR AALA201504209014](https://openairdocs.org/sdr/AALA201504209014), Apr 4, 2015: CHANNEL. CORRODED. C4 CHECK, CORROSION ON GALLEY AREA FLOOR STRUCTURE AT STATION 398, RBL 20. R & R CHANNEL IAW DWG 141N5186 & SRM 51-10-02 51-40-02. - [SDR AALA201504209013](https://openairdocs.org/sdr/AALA201504209013), Apr 4, 2015: SUPPORT FITTING. CORRODED. C4 CHECK, CORROSION ON GALLEY SUPPORT FITTING AT STATION 398, RBL 14. R & R SUPPORT FITTING IAW DWG 141N5186 & SRM 51-10-02 51-40-02. - [SDR AALA201505079001](https://openairdocs.org/sdr/AALA201505079001), Apr 3, 2015: KEELBEAM. CORRODED. C4 CHECK, CORROSION ON INNER ATTACH FLANGE OF KEEL BEAM IN RT WW AT APPROX STATION 1120 & RBL 10. REPAIRED IAW EA 106566. - [SDR AALA201504209017](https://openairdocs.org/sdr/AALA201504209017), Mar 28, 2015: FLOORBEAM. CORRODED. C4 CHECK, CORROSION ON FLOORBEAM T CAP AT BS 365 & RBL 45.5. REPAIRED FLOORBEAM T CAP IAW SRM 53-00-51-2R PROCEDURE 10. - [SDR AALA201505049003](https://openairdocs.org/sdr/AALA201505049003), Mar 26, 2015: FRAME. CRACKED. C4 CHECK, CRACK FOUND ON FRAME AT BS 1400, LT STRINGER 24. REMOVED DAMAGED AREAS OF FRAME. FABRICATED REPAIR SECTION OF FRAME & TWO DOUBLERS. INSTALLED REPAIR & - [SDR USAA2015012300002](https://openairdocs.org/sdr/USAA2015012300002), Jan 22, 2015: LOCK. LACK OF LUBE. EN-ROUTE, CAPTAIN`S SEAT TRACK LOCK FAILED ON TAKEOFF, SEAT ROLLED BACK. LUBED THE SEAT TRACK LOCK MECHANISM. - [SDR USAA2015011200012](https://openairdocs.org/sdr/USAA2015011200012), Dec 26, 2014: AILERON. DEBONDED. C2 CHECK, DISBONDING ON LT AILERON AT MOST INBD END & 12 INCHES FWD OF TE. REPLACED LT AILERON IAW JOB CARD 19L56827001. - [SDR USAA2015011200013](https://openairdocs.org/sdr/USAA2015011200013), Dec 24, 2014: SKIN PANEL. DELAMINATED. C2 CHECK, DELAMINATION ON APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6. REPAIRED APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6 IAW - [SDR USAA2014122600003](https://openairdocs.org/sdr/USAA2014122600003), Dec 24, 2014: SKIN PANEL. DELAMINATED. C2 CHECK DELAMINATION & CRACK AT APU COMPARTMENT TAIL CONE RT INTERIOR FUSELAGE SKIN PANEL AT STATION 1925 ON BACK SIDE OF ELEVATOR INDEX. ACCOMPLISHED TIME LIM - [SDR USAA2014122200003](https://openairdocs.org/sdr/USAA2014122200003), Dec 20, 2014: MONITOR. FAULTY. 2 HRS INTO FLIGHT, FLIGHT ATTENDANT NOTICED A SLIGHT BURNING SMELL IN FWD GALLEY AREA, SHE & ANOTHER FLIGHT ATTENDANT TRACED IT TO THE LT FWD VIDEO MONITOR IN 1 - [SDR USAA2015011200014](https://openairdocs.org/sdr/USAA2015011200014), Dec 11, 2014: PANEL. CRACKED. C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 3 LE COVE PANEL AT APPROX 354 INCHES FROM INBD EDGE & 14 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL - [SDR USAA2015011200016](https://openairdocs.org/sdr/USAA2015011200016), Dec 10, 2014: PANEL. CRACKED. C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 30 INCHES FROM OTBD EDGE & 13 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL - [SDR USAA2015011200015](https://openairdocs.org/sdr/USAA2015011200015), Dec 10, 2014: PANEL. CRACKED. C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 54 INCHES FROM INBD EDGE & 11.250 INCHES DOWN FROM TE. REPLACED LT WING 1 LE COVE PANEL - [SDR USAA2014121200002](https://openairdocs.org/sdr/USAA2014121200002), Dec 10, 2014: SLIDE. UNSERVICEABLE. R4 DOOR SLIDE OUT OF GREEN BAND. R & R R4 DOOR EVACUATION SLIDE. REPAIRED SLIDE. UNIT WAS PARTIALLY DISASSEMBLED, CLEANED & INSPECTED, REPLACING ALL PARTS NECES - [SDR USAA2014120100015](https://openairdocs.org/sdr/USAA2014120100015), Nov 30, 2014: WINDOW. DELAMINATED. RON REPLACE THE CAPTAINS NR 3 WINDOW FOR DELAMINATION. R & R CAPTAINS NR 3 WINDOW IAW AMM 56-11-10-424-015. PERFORMED WINDOW HEAT TEST IAW AMM 30-11-00-715-001. - [SDR USAA2014101600024](https://openairdocs.org/sdr/USAA2014101600024), Oct 15, 2014: KNOB. MISSING. UPPER EMER EXIT PANEL ON FLIGHT DECK DOOR IS MISSING THE LT PIN SO IT CANNOT BE OPENED. KNOB WAS MISSING FROM PIN, INSTALLED KNOB ON PIN ON UPPER EXIT PANEL ON All 502: https://openairdocs.org/model/boeing-757-2g7/reports.md --- 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.