# Boeing 757-2S7 - Type: Aircraft model (FAA registry) - Registry code: 1384962 - Manufacturer (registry): BOEING - Model: 757-2S7 - 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-757-2s7 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) - [N926FD](https://openairdocs.org/aircraft/N926FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1985, S/N 23323 ## NTSB investigations (4) 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 LAX99FA315](https://openairdocs.org/ntsb/LAX99FA315), Sep 20, 1999: Boeing 757-2S7 (N904AW), Agua Caliente, AZ, no damage. Probable cause: the systemic failure of the airline's maintenance department to identify and correct the long standing history of intermittent faults, nuisance warnings, and erratic behavior in this airplane's GPWS… - [NTSB FTW97IA112](https://openairdocs.org/ntsb/FTW97IA112), Mar 2, 1997: Boeing 757-2S7 (N902AW), Denver, CO, incident, minor damage. Probable cause: the pilot-in-command's failure to comply with company procedures/directives to not taxi the aircraft beneath the bridge/overpass, and his misjudgment of clearance between the vertical stabilizer and… - [NTSB LAX94LA333](https://openairdocs.org/ntsb/LAX94LA333), Aug 19, 1994: Boeing 757-200 (N901AW), Phoenix, AZ, no damage. Probable cause: the failure of the headset operator to adhere to established company safety procedures when he diverted his attention during pushback. A factor in the accident was the airline's failure to modify its… - [NTSB LAX90LA021](https://openairdocs.org/ntsb/LAX90LA021), Nov 6, 1989: Boeing 757-2S7 (N902AW), Phoenix, AZ, no damage. Probable cause: THE GROUND HANDLER IMPROPERLY CROSSING UNDER THE AIRCRAFT WHILE IT WAS MOVING. ## FAA accident and incident reports (15) 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 20130608017639I](https://openairdocs.org/incident/20130608017639I), Jun 8, 2013: Boeing 757-2S7 (N904AW), Kailua Kona, HI, No damage. On June 8th our a/c tail number N904AW in koa at gate was ready to push back when APU failed internally thus inducing some smoke/fumes entering cabin through… - [Incident 20030629013149I](https://openairdocs.org/incident/20030629013149I), Jun 29, 2003: Boeing 7572S7 (N904AW), Phoenix, AZ, Minor damage. (-23) On climb out from Phoenix Sky Harbor International Airport to minneapolis, Minnesota at flight level 190 there was a loud bang and an airframe shudder.… - [Accident 19990920043369A](https://openairdocs.org/incident/19990920043369A), Sep 20, 1999: Boeing 7572S7 (N904AW), Agua Caliente, AZ, No damage. (-23) GPWS gave false warning while aircraft was descending in IMC conditions. Crew performed the escape manuever. Four flight attendants standing in the rear… - [Incident 19990713025889I](https://openairdocs.org/incident/19990713025889I), Jul 13, 1999: Boeing 7572S7 (N902AW), Columbus, OH. Flight crew reported that the left hand hyd. Qty. Dropped to .11. Awxa maintenance found the lft. Engine driven pump case drain quick disconnect backed off at… - [Accident 19970302001939A](https://openairdocs.org/incident/19970302001939A), Mar 2, 1997: Boeing 7572S7 (N902AW), Denver, CO, Substantial damage. Aircraft was taxiing inbound on ramp to gate, tail struck a pedestrian bridge. - [Accident 19940819026649A](https://openairdocs.org/incident/19940819026649A), Aug 19, 1994: Boeing 7572S7 (N901AW), Phoenix, AZ. During tug pushback ramp agent hooked to 727 transcier was run over by nose ear. Lost a leg. In charge of pushback. - [Incident 19920720034309I](https://openairdocs.org/incident/19920720034309I), Jul 20, 1992: Boeing 7572S7 (N902AW), Newark, NJ. Woman passenger was observed exiting lavatory on two occasions followed by a trail of smoke. Police met aircraft. - [Incident 19920115016369I](https://openairdocs.org/incident/19920115016369I), Jan 15, 1992: Boeing 7572S7 (N902AW), Wichita, KS. Passenger became unruly and threatening. Unscheduled landing at Wichita. Passenger taken under custody by police. - [Accident 19891106044619A](https://openairdocs.org/incident/19891106044619A), Nov 6, 1989: Boeing 757200 (N902AW), Phoenix, AZ. Aircraft nose wheel rolled over ground crewmans legs on push back. Crewman was passing under aircraft and fell. - [Incident 19891030055479I](https://openairdocs.org/incident/19891030055479I), Oct 30, 1989: Boeing 7572S7 (N902AW), Santa Ana, CA. Loud bang after takeoff. Aircraft yawed right. Right engine EGT red lined. Returned and landed. Cause not stated. - [Incident 19890406050139I](https://openairdocs.org/incident/19890406050139I), Apr 6, 1989: Boeing 7572S7 (N905AW), Phoenix, AZ. On climbout saw Learjet come into view over cockpit about 200 feet away. No traffic advisory. Learjet unidentified. - [Incident 19890326011899I](https://openairdocs.org/incident/19890326011899I), Mar 26, 1989: Boeing 7572S7 (N904AW), Salina, KS. 3000 Lb fuel imbalance. Shut engine down and diverted. No fuel leak found. Cleaned crossfeed valve. - [Incident 19881012058959I](https://openairdocs.org/incident/19881012058959I), Oct 12, 1988: Boeing 7572S7 (N904AW), Kansas City, MO. Lost pressurization. Deployed masks,descended,diverted to Kansas City. Faulty 02 system,exhaust valve,engine bleed. - [Incident 19880111003679I](https://openairdocs.org/incident/19880111003679I), Jan 11, 1988: Boeing 7572S7 (N901AW), Baltimore, MD. Lost cabin pressure on climbout. Returned to airport. Found faulty cabin out-flow valve. - [Incident 19871229077799I](https://openairdocs.org/incident/19871229077799I), Dec 29, 1987: Boeing 7572S7 (N901AW), Las Vegas, NV. Auto cabin pressure inop light on in climb. Auto pressurization inoperative, returned. Found faulty outflow valve. ## Service difficulty reports (1,282, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA202108202048](https://openairdocs.org/sdr/FDEA202108202048), Aug 20, 2021: FRAME. DAMAGED. REPAIR INSTRUCTIONS REQUIRED FOR THE ACCOMPLISHMENT OF FEDEX E.A. F-5310-147693, PART 10, SPLICE REPAIR AT STA 1640, S9R TO S20R COMPLIED WITH E.A F-5310-147693 - [SDR FDEA202108112001](https://openairdocs.org/sdr/FDEA202108112001), Aug 11, 2021: SKIN. DENTED. FUSELAGE SKIN @ STA 1730, BETWEEN STR 29L - STR 29R, HAS 2EA DENTS. REPAIRED SKIN IAW FEDEX EA # F-5330-146539-P3 - [SDR FDEA202105081161](https://openairdocs.org/sdr/FDEA202105081161), May 8, 2021: LINE. LEAKING. A SLOW LOSS OF RIGHT HYDRAULIC SYSTEM FLUID LED TO RIGHT HYDRAULIC SYSTEM FAILURE. COMPLIED WITH QRH, DECLARED AN EMERGENCY. AIRCRAFT WAS AIRBORNE FOR APPROXIMA - [SDR FDEA202103090608](https://openairdocs.org/sdr/FDEA202103090608), Mar 9, 2021: DRIVE UNIT. FAILED. WHEN CONFIGURING TO LAND AT SLC IT WAS VERY DIFFICULT TO MOVE FLAP LEVER FROM 20 TO 25 DETENT. WHEN I FINALLY WAS ABLE TO MOVE FLAP LEVER TO 25, WE RECEIVED A T - [SDR FDEA202101290236](https://openairdocs.org/sdr/FDEA202101290236), Jan 29, 2021: ACTUATOR. INOPERATIVE. MAIN CARGO DOOR WILL NOT CLOSE. FOUND BOTH LINKS ON AFT MAIN CARGO DOOR ACTUATOR BROKEN. RAISED CARGO DOOR WITH SLING REF B757 AMM CH 52-32-00-4 SO CARGO COULD - [SDR FDEA202012063050](https://openairdocs.org/sdr/FDEA202012063050), Dec 6, 2020: SKIN. DAMAGED. LOWER FUSELAGE SKINS BETWEEN STA 1540 AND STA 1640 STRINGERS S-30 TO S-26L HAS NUMEROUS PLACES OF DAMAGE. COMPLIED WITH EA F-5330-T0358203 TITLED: FUSELAGE-SECT - [SDR FDEA202012063049](https://openairdocs.org/sdr/FDEA202012063049), Dec 6, 2020: STRAP. DAMAGED. AFT CARGO COMPARTMENT FUSELAGE CIRCUMFERENTIAL STRAP AT STA 1620 FROM STRINGER S-28L TO S-29R PUNCTURED, DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED C - [SDR FDEA202012063048](https://openairdocs.org/sdr/FDEA202012063048), Dec 6, 2020: STRINGER CLIP. DAMAGED. AFT CARGO COMPARTMENT STRINGER CLIP AT S30 STA 1616 TO STA 1623 SEPARTED FROM SKIN AND HAS SHEARED FASTENERS AND SURFACE CORROSION. REMOVED AND REPLACED SPLICE - [SDR FDEA202012063047](https://openairdocs.org/sdr/FDEA202012063047), Dec 6, 2020: STRINGER SPLICE. DAMAGED. AFT CARGO COMPARTMENT STRINGER S-29L STRINGER SPLICE AT STA 1620 PUNCTURED AND STRINGER FROM STA 1623 TO STA 1630 DEFORMED. REMOVED AND REPLACED STRINGER SPLICE - [SDR FDEA202012053034](https://openairdocs.org/sdr/FDEA202012053034), Dec 5, 2020: STRINGER. BENT. AFT CARGO COMPARTMENT STRINGER S-27L BETWEEN STA 1588 TO STA 1600 BENT AND DEFORMED. REPAIRED STRINGER S-27L AT STA 1570, IAW SRM 53-00-03-2R. REPAIR BETWEEN ST - [SDR FDEA202012043030](https://openairdocs.org/sdr/FDEA202012043030), Dec 4, 2020: SKIN. DAMAGED. FUSELAGE SKIN HAS DENT AND CREASE DAMAGE BETWEEN STA 1520 AND STA 1540 STRAINGERS S-25L TO S-26L. COMPLIED WITH EA F-5330-T0358196 PART 1 TITLE: FUSELAGE-SECTIO - [SDR FDEA202012043029](https://openairdocs.org/sdr/FDEA202012043029), Dec 4, 2020: SHEAR TIE. CRACKED. AFT CARGO COMPARTMENT SHEAR TIE AT STA 1600 STRINGER S-27L TO S-28L SHEARED/CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1600 S-27L TO S-28L, IAW SRM 51-40-02. F - [SDR FDEA202012043028](https://openairdocs.org/sdr/FDEA202012043028), Dec 4, 2020: SHEAR TIE. CRACKED. AFT CARGO COMPARTMENT SHEAR TIE AT STA 1620 FROM STRINGER S-28L TO S-29L SHEARED, CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1620 S-28L TO S-29L, IAW SRM 51-40 - [SDR FDEA202012043027](https://openairdocs.org/sdr/FDEA202012043027), Dec 4, 2020: SHEAR TIE. BENT. AFT CARGO COMPARTMENT SHEAR TIE AT STRINGER S-29L TO S-30 DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED SHEAR TIE, IAW SRM 51-40-02. FABED ON VTMAE TRAV - [SDR FDEA2020030970501](https://openairdocs.org/sdr/FDEA2020030970501), Mar 7, 2020: UNKNOWN. MALFUNCTIONED. PDIS 926 27-50 8236 07MAR20 RNO FACT U LOGPAGES:3215684 EXTENDING FLAPS FROM 15*- 20* RECEIVED TE FLAP DISAGREE CAUTIN MESSAGE. FLAPS STOPPED MOVING AT 17*. COM - [SDR FDEA202001110158](https://openairdocs.org/sdr/FDEA202001110158), Jan 11, 2020: SKIN. DAMAGED. THE LH SIDE OF THE FUSELAGE FROM STA 510-515 2"-4" DOWN FROM STR 26L HAS SEVERAL DEEP PITS FROM LIGHTNING STRIKE. REPAIRED DAMAGE IN FUSELAGE SKIN CAUSED BY LIG - [SDR FDEA201907241678](https://openairdocs.org/sdr/FDEA201907241678), Jul 24, 2019: DOOR. CRACKED. POSSIBLE CRACK ON L2 DOOR UPPER HINGE CUTOUT ALL WORK ACCOMPLISHED IAW EA F-5210-T0348085 P1 DOORS - PASSENGER/CREW - CARGO - L -2 DOOR FORWARD FRAME UPPER HING - [SDR FDEA201907231668](https://openairdocs.org/sdr/FDEA201907231668), Jul 23, 2019: FILLER. CORRODED. AFT CARGO COMPT STA 1440 AT STR 29R TAPERED FILLER ON STRINGER HAS EXFOLIATING CORROSION. FOUND TAPERED FILLER AT STA 1440 STR 29R OUT OF LIMITS DUE TO 100% MAT - [SDR FDEA201907111527](https://openairdocs.org/sdr/FDEA201907111527), Jul 11, 2019: STRINGER. CORRODED. AFT PIT - BS 1440, STR. 29 RT HAS CORROSION ON I/B SIDE. - [SDR FDEA201907101520](https://openairdocs.org/sdr/FDEA201907101520), Jul 10, 2019: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA 1180-1200 LBL44.5 SEAT TRACK FANGE CORRODED EVALUATED SEAT TRACK STA 1180-1200 LBL 44.5 ORIG MAT .070 REM .00 LOSS .070 OUT OF LIMITS IAW - [SDR FDEA201907101519](https://openairdocs.org/sdr/FDEA201907101519), Jul 10, 2019: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA 1040-1055 BLO CORROSION ON SEAT TRACK FLANGE. REMOVED CORR ON SEAT TRACK (FLANGE) SUPPORT STA 1040-1055 BL0 IAW SRM 51-10- 02. ORIG MAT.0 - [SDR FDEA201907101521](https://openairdocs.org/sdr/FDEA201907101521), Jul 10, 2019: SEAT TRACK. CORRODED. MAIN CABIN STA 1195 BL0 SEAT TRACK FLANGE CORRODED. - [SDR FDEA201907091513](https://openairdocs.org/sdr/FDEA201907091513), Jul 9, 2019: SKIN. DENTED. LT FUSELAGE OUTER SKIN AT FS 215 AROUND S-21L HAS A DENT. EVALUATED DENT ON SKIN STA. 215 AROUND S-21L A\Y FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A. HFEC IAW N - [SDR FDEA201907061494](https://openairdocs.org/sdr/FDEA201907061494), Jul 6, 2019: SHEAR PLATE. CORRODED. MAIN CABIN BETWEEN STA. 1680 - 1720, BL0 RBL53 FLOOR WEB CORRODED ALL WORK ACCOMPLISHED IAW EA F-5310-T0348184 P1 FUSELAGE - MAINFRAME - AFT SHEAR DECK PLATE CO - [SDR FDEA201907061492](https://openairdocs.org/sdr/FDEA201907061492), Jul 6, 2019: FLOORBEAM. CORRODED. MAIN CABIN BETWEEN STA. 920 - 1040 RBL 24.75 FLOOR BEAM T CHORD CORRODED REMOVED CORR ON T-CHORD STA 920-1040 RBL 24.75 IAW SRM 51-10-02. ORIG MAT .090 REM .045 - [SDR FDEA201907061491](https://openairdocs.org/sdr/FDEA201907061491), Jul 6, 2019: SEAT TRACK. CORRODED. MAIN CABIN BETWEEN STA. 1620 - 1640 RBL 44.5 SEAT TRACK FLANGE CORRODED REMOVED CORR ON SEAT TRACK FLANGE STA 1620-1640 RBL 44.5 IAW SRM 51-10-02. ORIG MAT. .07 - [SDR FDEA201907061493](https://openairdocs.org/sdr/FDEA201907061493), Jul 6, 2019: FLOORBEAM. CORRODED. MAIN CABIN BETWEEN STA. 1015 - 1021 BLB 24.75 FLOORBEAM T CHORD CORRODED. - [SDR FDEA201901120106](https://openairdocs.org/sdr/FDEA201901120106), Jan 12, 2019: SEAT TRACK. GOUGED. REMOVE AND REPLACE LBL 45.50 SEAT TRACK FROM BS440 TO BS680 COMPLIED WITH - EQUIP AND FURNISH - CARGO - LOADING SYSTEM - INTERIM REPAIR FOR DAMAGE SEAT TRACK LO - [SDR FDEA2018080321896](https://openairdocs.org/sdr/FDEA2018080321896), Aug 2, 2018: THERMAL SWITCH. FAILED. LT ENG STRUT OH DET 1 EICAS MESSAGE ON STATUS PAGE DURING CLIMB OUT TO 360. FOUND THERMAL SWITCH S10196 GIVING AN OVERHEAT DETECTION INDICATION BEFORE TEMPERATU - [SDR FDEA2018080311873](https://openairdocs.org/sdr/FDEA2018080311873), Aug 1, 2018: CIRCUIT CARD. FAILED. WHILE CLIMBING THROUGH FL340 TO 360, LT ENGINE OVHT EICAS MESSAGE ON. PERFORMED QRH, LIGHT EXTINGUISHED AT 1.28 EPR. IAW FIM R&R AFOLDS CARD IAW AMM 26-10-01-4 - [SDR FDEA201808171644](https://openairdocs.org/sdr/FDEA201808171644), Jul 7, 2018: UNKNOWN. MALFUNCTIONED. AT SPEEDBRAKE DEPLOYMENT A ROLE TO THE LEFT OCCURS WITH A DISPLACEMENT OF THE YOKE TO THE RIGHT. AT DEPLOYMENT YOKE DISPLACES 1.5 UNITS ON AILERON TRIM INDICATO - [SDR FDEA201806071417](https://openairdocs.org/sdr/FDEA201806071417), Jun 7, 2018: POWER SUPPLY. INOPERATIVE. RT R1 DOOR EXTERIOR SLIDE LIGHT INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY M00730 PER MM CH 33-51-07-2. A/C READY FOR CONT SERVICE. - [SDR FDEA201708172251](https://openairdocs.org/sdr/FDEA201708172251), Aug 17, 2017: BRACKET. LOOSE. FLAP FAIRING BRACKET FOR 573HB IS LOOSE. REPAIRED THE LT, INBD MAIN FLAP IAW SRM 57-53-02-2R, REPAIR 3, AND EA F-5750-T0334988, PI. - [SDR FDEA201708082146](https://openairdocs.org/sdr/FDEA201708082146), Aug 8, 2017: SKIN. DENTED. LEFT WING NR 3 SLAT UPPER SURFACE HAS A DENT AT CENTER OF SLAT AT T\E. REPAIRED THE LT WING SLAT IAW SRM 51-70-10-2R, PARAG 8 AND 20. - [SDR FDEA201708082142](https://openairdocs.org/sdr/FDEA201708082142), Aug 8, 2017: SEAT TRACK. CORRODED. MAIN CABIN, BS 1640 - 1680, LBL45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED THE CORROSION IAW SRM 51-10-02 WITH 100 PERCENT MATERIAL LOSS. FABRICATED A NEW S - [SDR FDEA201708082141](https://openairdocs.org/sdr/FDEA201708082141), Aug 8, 2017: SEAT TRACK. CORRODED. MAIN CABIN, BS 1640 - 1660, RBL 45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED CORROSION IAW SRM 51-10-02-0G, 100 PERCENT LOSS. FABRICATED A NEW SEAT TRACK IAW - [SDR FDEA201708082140](https://openairdocs.org/sdr/FDEA201708082140), Aug 8, 2017: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BS 365 - 345, LBL 6 HAS CORROSION. REMOVED THE CORROSION AND FOUND 100% LOSS IAW SRM 51-10-02, & 53-00-52-1A. REMOVED AND REPLACED THE SEA - [SDR FDEA201705191457](https://openairdocs.org/sdr/FDEA201705191457), May 19, 2017: SIGHT GAUGE. CLOUDY. LEFT ENTRY DOOR INSPECTION WINDOW FOR SLIDE PRESSURE GAUGE IS HAZED, MAKING IT DIFFICULT TO READ. CLEANED THE SIGHT WINDOW IAW AMM: 20-30-02-2. OK FOR SERVICE. - [SDR FDEA201702020380](https://openairdocs.org/sdr/FDEA201702020380), Feb 2, 2017: COMPUTER. OUT OF ADJUST. AIRCRAFT PITCH CONTROL HAS LAG ON PREFLIGHT CONTROL CHECK AND ON ARRIVAL PITCH AXIS WAS STIFF AND SEEMED TO HAVE A DELAY IN CONTROL. ADJUSTED AND TESTED OF ELEV - [SDR FDEA201701050053](https://openairdocs.org/sdr/FDEA201701050053), Jan 5, 2017: WARNING BELL. FALSE ACTIVATION. TRIED TO SWITCH TO GROUND POWER AFTER BLOCKIN, THE FIRE BELL SOUNDED FOR 10 SECONDS. NO FIRE LIGHTS ILLUMINATED. NO OTHER INDICATIONS OF FIRE OR ANY OTHER MALFU - [SDR AALA201606209001](https://openairdocs.org/sdr/AALA201606209001), Jun 16, 2016: ACTUATOR. DEFECTIVE. AIRCRAFT WAS NOT GROUNDED, R4 DOOR GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. REPLACED PROXIMITY SENSOR AND ACTUATOR, TARGET, AT THE R4 DOOR. A SATISFACTORY OPS CHE - [SDR AALA201606179008](https://openairdocs.org/sdr/AALA201606179008), Jun 16, 2016: PROXIMITY SENSOR. DEFECTIVE. AIRCRAFT WAS NOT GROUNDED: R4 DOOR GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. REPLACED PROXIMITY SENSOR AND ACTUATOR, TARGET, AT THE R4 DOOR. A SATISFACTORY OPS CHE - [SDR AALA201605289002](https://openairdocs.org/sdr/AALA201605289002), May 27, 2016: RESERVOIR. LOW PRESSURE. AIRCRAFT WAS NOT GNDED. L2 DOOR EMER POWER RESERVOIR PRESS IS 0. REPLACED L2 DOOR EMER POWER RESERVOIR IAW AMM 52-11-30. - [SDR AALA201602099006](https://openairdocs.org/sdr/AALA201602099006), Feb 6, 2016: PUMP. INOPERATIVE. AIRCRAFT WAS NOT GNDED. LT CTR TANK FUEL PUMP, PRESS LIGHT & CTR LT FUEL PUMP, EICAS MSG APPEARED AFTER ENG START. ASSOCIATED CB FOUND TRIPPED ON P6 3 PANEL F14 - [SDR AALA201602019009](https://openairdocs.org/sdr/AALA201602019009), Jan 30, 2016: TRIM SWITCH. DEFECTIVE. RETURNED & EMER DECLARED. ACFT WAS GNDED. RUDDER & RUDDER TRIM CONTROL. RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. REPLACED RUDDER TRIM SWITCH & ACCOMPLISH - [SDR AALA201601259005](https://openairdocs.org/sdr/AALA201601259005), Jan 23, 2016: SENSOR. CONTAMINATED. AIRCRAFT WAS NOT GNDED. R2 SLIDE LIGHT ILLUMINATED WITH DOOR DISARMED. REMOVED EXCESSIVE AMOUNT OF DOOR LUBE FROM SENSORS. ACCOMPLISHED A SATISFACTORY OPERATION - [SDR AALA201601109002](https://openairdocs.org/sdr/AALA201601109002), Jan 9, 2016: WIRE HARNESS. LOOSE. AIRCRAFT WAS NOT GNDED. R2 DOOR SLIDE LIGHT REMAINS ON WHEN HANDLE IS IN THE DISARM POSITION. SECURED WIRE HARNESS TO SLIDE LIGHT AT THE R2 DOOR. ACCOMPLISHED A - [SDR AALA201601109001](https://openairdocs.org/sdr/AALA201601109001), Jan 9, 2016: BATTERY. DISCHARGED. AIRCRAFT WAS NOT GNDED. INBD FLASHLIGHT AT L2 DOOR, FLIGHT ATTENDANT SEAT NOT CHARGING. SECOND FLASHLIGHT AT LOCATION CHARGING. REPLACED FLASHLIGHT BATTERY & AC - [SDR AALA201512239007](https://openairdocs.org/sdr/AALA201512239007), Dec 21, 2015: GIRT BAR. OBSTRUCTED. AIRCRAFT WAS GNDED. DOOR 4R WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR TRACKS IAW MM 52-11-00. 4R DOOR NOW ARMS PROPERLY. - [SDR AALA201512139001](https://openairdocs.org/sdr/AALA201512139001), Dec 12, 2015: SLIDE. DISLODGED. AIRCRAFT WAS NOT GNDED. FOUND L4 DOOR SLIDE DISLODGED. TIGHTENED HARNESS ON SLIDE PACK TO REPOSITION SLIDE IAW AMM 25-66-01. All 1,282: https://openairdocs.org/model/boeing-757-2s7/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.