# N933FD: Boeing 757-21B - Status: Valid registration - Airframe: [Boeing 757-21B](https://openairdocs.org/model/boeing-757-21b) (registry code 1384917, 239 seats) - Serial number: 24330 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: July 18, 2008 - Expires: November 30, 2027 - Mode S code: ACF14F - Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=933FD - Page: https://openairdocs.org/aircraft/N933FD From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Boeing 757-21B) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N933FD. ## FAA accident and incident reports None matched to N933FD. ## Service difficulty reports (462, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA202205031109](https://openairdocs.org/sdr/FDEA202205031109), May 3, 2022: MECHANISM. WRONG PART. RIGHT SIDE DOOR SLIDE LIGHT NOT INDICATING ARMED AND ARMING HANDLE BINDING. FOUND R1 DOOR EMER OPERATION MECHANISM AT CENTER RANK HAD INCORRECT HARDWARE INSTALL - [SDR FDEA202108061968](https://openairdocs.org/sdr/FDEA202108061968), Aug 6, 2021: ACTUATOR. WORN. AT FLAPS 1 SELECTION FLAPS MOVED TO 1 POSITION & GOT EICAS MESSAGE LE SLAT DISAGREE. RAN QRH PROCEDURES, AFTER MOVED THE ALTERNATE FLAP SELECTOR THE EICAS MESSA - [SDR FDEA202108031925](https://openairdocs.org/sdr/FDEA202108031925), Aug 3, 2021: SLAT SYSTEM. LACK OF LUBE. LE SLAT DISAGREE BETWEEN UP AND 1 AT 225 KTS/3000 FEET. RAN QRH AND LANDED FLAPS 20 PER QRH. EMERGENCY DECLARED. LUBED LEFT AND RIGHT WING LEADING EDGE SLATS RE - [SDR FDEA202102020264](https://openairdocs.org/sdr/FDEA202102020264), Feb 2, 2021: ATTACH ANGLE. CRACKED. R/H WING I/B FLAP UPPER T/E PANEL ATTACK ANGLE IS CRACKED JUST ABOVE O/B END OF AFT FLAP. REMOVED AND REPLACED R/H WING I/B FLAP UPPER T/E PANEL ATTACH ANGLE IA - [SDR FDEA202101250186](https://openairdocs.org/sdr/FDEA202101250186), Jan 25, 2021: FLOORBEAM. CORRODED. FWD WET AREA STA 333.45 BETWEEN RBL 2.5-RBL 4.5 FLOOR SUPPORT CORRODED. EVALUATED FLOOR SUPPORT AT FWD WET STA 333.45 BETWEEN RBL 2.5-4.5, FOUND TO BE WITH OUT - [SDR FDEA202101110052](https://openairdocs.org/sdr/FDEA202101110052), Jan 11, 2021: FLOOR SUPPORT. PUNCTURED. MAIN DECK STA 1055 LBL 43 FLOOR SUPPORT HAS A PUNCTURE HOLES. EVALUATED FLOOR SUPPORT AT MAIN DECK STA 1055 LBL 43,FOUND DAMAGE ONLY ON CO COVER COVER PLATE IAW - [SDR FDEA202101090030](https://openairdocs.org/sdr/FDEA202101090030), Jan 9, 2021: SKIN. DAMAGED. FUSELAGE PLATE & SKIN STA 740 TO STA 760 STRINGER 26L REQUIRE REPLACE REPAIR DOUBLER. COMPLIED WITH EA # F-5330-131077 D P2 TITLE: FUSELAGE - PLATES AND SKIN - - [SDR FDEA202101080021](https://openairdocs.org/sdr/FDEA202101080021), Jan 8, 2021: SKIN. DAMAGED. FUSELAGE & SKIN STA 660 - 700,STRINGER 26R LOWER SKIN LAP JOINT - DOUBLER REPAIR - REQUIRE REPLACE. COMPLIED WITH EA # F-5330-131060 B P2 TITLE: FUSELAGE - PLAT - [SDR FDEA202012053041](https://openairdocs.org/sdr/FDEA202012053041), Dec 5, 2020: LAMP. INOPERATIVE. LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE WHEN EXTENDED PRIOR TO LANDING. FOUND BOTH LAMPS BURNED OUT IN LT GEAR POSITION LIGHT ASSEMBLY. RELAMPED WITH 2 - [SDR FDEA202007021433](https://openairdocs.org/sdr/FDEA202007021433), Jul 2, 2020: COVER. DAMAGED. THE L1 DOOR SLIDE COVER HAS ALL 4 FASTNERS PULLED THROUGH THE COMPOSITE THE FWD LATCH WILL NOT CONNECT TO THE DOOR. WILL NEED COMPOSITE SHOP. REMOVED AND PLACED - [SDR FDEA2019101082494](https://openairdocs.org/sdr/FDEA2019101082494), Oct 8, 2019: WARNING LIGHT. FALSE ACTIVATION. FWD ACCESS DOOR EICAS LIGHT ILLUMINATED WHEN AIRCRAFT ROTATED FOR TAKEOFF. OPS OK IAW FIM 52-71, FT 802 & AMM 52-70-00-5-0, GVI AND CHECKED FWD ACCESS DOOR TARG - [SDR FDEA2019032019672](https://openairdocs.org/sdr/FDEA2019032019672), Mar 19, 2019: GIRT BAR. FAILED. R1 ENTRY DOOR GIRT BAR STAYED ENGAGED. R1 DOOR ASSIST BOTTLE BLEW. SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED GIRT BAR IAW AMM 25-66-01-4. REPLACED SLIDE IA - [SDR FDEA201902210476](https://openairdocs.org/sdr/FDEA201902210476), Feb 21, 2019: SKIN. GOUGED. MAIN CARGO DOOR, UPPER SECTION SKIN, AT APPROXIMATE STATION 495, STRINGER S-6 LEFT, HAS GOUGE DAMAGE. REPAIRED PER SRM 52-30-01 FIG 201, REPAIR 4. - [SDR FDEA201901250204](https://openairdocs.org/sdr/FDEA201901250204), Jan 25, 2019: PROXIMITY SWITCH. OUT OF ADJUST. ON GEAR RETRACT RECEIVED EICAS "GEAR DISAGREE" MSG. AFTER 20 SEC MSG WENT AWAY. NOTE- GEAR SHOWED UP AMBER GEAR LIGHT WAS ILLUMINATED AND WENT AWAY AFTER 20 SEC - [SDR FDEA201901110091](https://openairdocs.org/sdr/FDEA201901110091), Jan 11, 2019: FRAME. GOUGED. FWD ACCESS. COMPT. FRAME AT STA. 231.25 BL.0 HAS GOUGE ON EXISTING REPAIR ANGLE ON INSIDE OF FRAME REMOVED DAMAGED EXISTING REPAIR ANGLE, CUT OUT AREA OF FRAME, - [SDR FDEA201809302752](https://openairdocs.org/sdr/FDEA201809302752), Sep 30, 2018: SLIDE. FAILED. ON ARRIVAL RAMP OPENED L1 DOOR AND SLIDE/RAFT MALFUNCTIONED AND DID NOT DISCONNECT FROM GIRT BAR ATTACHMENT POINTS. INSTALLED NEW L1 DOOR SLIDE IAW MM 25-66-01- - [SDR FDEA201808071936](https://openairdocs.org/sdr/FDEA201808071936), Aug 7, 2018: GIRT BAR. OBSTRUCTED. L1 DOOR ARMING LEVER EXTREMELY DIFFICULT TO MOVE INTO THE ARMED POSITION. REQUIRED MULTIPLE L1 DOOR OPENING/CLOSING TO GET ARM LEVER TO ENGAGE. FOUND THE D-RING - [SDR FDEA201804040844](https://openairdocs.org/sdr/FDEA201804040844), Apr 4, 2018: GIRT BAR. MALFUNCTIONED. L1 DOOR GIRT BAR FAILED TO DISCONNECT WHEN DOOR WAS MOVED TO DISARM. REMOVED AND REPLACE L1 DOOR EMERGENCY POWER RESERVOIR CYLINDER IAW MM 52-11-30-4. - [SDR FDEA201706201711](https://openairdocs.org/sdr/FDEA201706201711), Jun 20, 2017: YOKE. DAMAGED. LATERAL PLAY IN YOKE FOR AILERON INPUT. - [SDR FDEA201701130221](https://openairdocs.org/sdr/FDEA201701130221), Jan 13, 2017: ROLLER. DAMAGED. PRIOR TO PUSH BACK, AN EICAS LT FWD ENTRY DOOR EICAS ALERT. F/O OPENED AND SHUT DOOR AND EICAS WENT AWAY. SAME EICAS RETURNED AFTER ENGINE START. SAME PROCEDURE - [SDR FDEA201612234535](https://openairdocs.org/sdr/FDEA201612234535), Dec 23, 2016: DEPRESSOR. DENTED. CARGO DOOR LOWER AFT CORNER SEAL DEPRESSOR DENTED. REMOVED AND REPLACED IAW DWG 146N6603 REV. A. PERFORMED SATISFACTORY PRESSURIZATION LEAK CHECK, NO LEAKS NOTE - [SDR FDEA201612214517](https://openairdocs.org/sdr/FDEA201612214517), Dec 21, 2016: SHEAR TIE. CORRODED. FWD CARGO BAY BS 820 BL 0 HAS A SHEAR TIE CORRODED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A DET. V. REMOVED AND REPLACED - [SDR FDEA201612184488](https://openairdocs.org/sdr/FDEA201612184488), Dec 18, 2016: SKIN. CORRODED. FWD CARGO BAY FUSELAGE SKIN AND VHF ANTENNA DOUBLER ARE CORRODED BETWEEN BS 720 - 740, BL 0 BETWEEN STRINGERS 28L AND 28R. REMOVED CORROSION, CUTOUT DAMAGED SEC - [SDR FDEA201612074353](https://openairdocs.org/sdr/FDEA201612074353), Dec 7, 2016: SKIN. DEBONDED. DISBOND FOUND ON RIGHT INBOARD MAIN FLAP ON THE CORNER. ACCOMPLISHED PERMENENT REPAIR ON RIGHT INBD MAIN FLAP IAW 57-53-01-2R FIG. 201 AND SRM 51-70-10-2R REPAI - [SDR FDEA201612064339](https://openairdocs.org/sdr/FDEA201612064339), Dec 6, 2016: SKIN. DENTED. LEFT HORIZONTAL STAB UPPER SKIN HAS A DENT AT HSS 107.604. REPAIRED IAW SRM 55-10-01-1A FIG 101 NOTE 1, AND SRM 51-70-10-2R REPAIR NR 4 TAP TESTED IAW SRM 51-70 - [SDR FDEA201608042798](https://openairdocs.org/sdr/FDEA201608042798), Aug 4, 2016: WARNING LIGHT. FALSE ACTIVATION. REJECTED T/O AT 60 KTS FOR AN EICAS R HYD ENG PUMP AND PRESSURE LIGHT ILLUMINATED FOR RT ENG HYD PUMP AND ON THE OVERHEAD PANEL. QRH RTO AND HYDRAULIC ENGINE PU - [SDR FDEA201607142446](https://openairdocs.org/sdr/FDEA201607142446), Jul 14, 2016: BATTERY PACK. UNSECURE. L1 DOOR OVERHEAD EMERGENCY EXIT LT AND EXT SLIDE LIGHT INOPERATIVE. FOUND BATTERY PACK AT M731 UNSECURED, NOT SURE HOW LONG IT HAS BEEN IN THIS CONDITION. R & R - [SDR FDEA201607032248](https://openairdocs.org/sdr/FDEA201607032248), Jul 3, 2016: UNKNOWN. ODOR. DURING DESCENT THRU 11,000' AND LEVELING OFF AT 10,000' AND POWERING UP, AIR CONDITIONING PACKS CYCLED AND A FUME EVENT OCCURRED. DIRTY SOCK ODOR UNTIL ENGINE S - [SDR FDEA201602030437](https://openairdocs.org/sdr/FDEA201602030437), Feb 3, 2016: SLIDE. UNWANTED DEPLOY. SLIDE WAS UNARMED & WAS CRACKED OPEN WHEN RAMP FINISHED OPENING. DOOR SLIDE BAR WAS STILL ATTACHED & DOOR BLEW OPEN. SLIDE FELL ONTO AIRSTAIRS BEFORE LANYARD WA - [SDR FDEA201601060064](https://openairdocs.org/sdr/FDEA201601060064), Jan 6, 2016: LINE. OUT OF POSITION. RIGHT CREW ENTRY DOOR, SLIDE LIGHT DOES NOT ILLUMINATE WITH DOOR. FOUND GIRT BAR STATIC LINE OUT OF PLACE & NOT LETTING GIRT BAR LOCK GO FULL TRAVEL. REPOSITION - [SDR FDEA201506161822](https://openairdocs.org/sdr/FDEA201506161822), Jun 16, 2015: STOWAGE BOX. INOPERATIVE. FOUND COURIER O2 MASK BOX PRESS TO TEST BUTTON BROKEN. R & R O2 MASK STOWAGE BOX IAW AMM 35-11-51-4-99. OK FOR SERVICE. - [SDR FDEA201412274193](https://openairdocs.org/sdr/FDEA201412274193), Dec 27, 2014: FRAME. DENTED. AFT CARGO BAY LT SIDE FRAME DENTED AT BS 1420 BETWEEN STRINGERS 25 & 26L. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02 AND DRAWING 146N1012 REV C. - [SDR FDEA201412264191](https://openairdocs.org/sdr/FDEA201412264191), Dec 26, 2014: FRAME. GOUGED. FORWARD NOSE COMPARTMENT BILGE AREA BS 231 FRAME IS GOUGED AT BL 0. REPAIRED IAW EA F-5310-T0314177 P1. - [SDR FDEA201412264190](https://openairdocs.org/sdr/FDEA201412264190), Dec 26, 2014: SKIN. DENTED. SKIN DENTED AT BS 523 JUST BELOW STRINGER 26L. REPAIRED IAW EA F-5330-T0314272. - [SDR FDEA201412204158](https://openairdocs.org/sdr/FDEA201412204158), Dec 20, 2014: SHEAR TIE. CRACKED. SHEAR TIE HAS A CRACK AT BS 350 UPPER SIDE OF L1 DOOR FRAME. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, 51-40-05, 51-40-08 AND DRAWING 141N1318. - [SDR FDEA201412204157](https://openairdocs.org/sdr/FDEA201412204157), Dec 20, 2014: SKIN. DENTED. FUSELAGE HAS A DENT AT BS 609 BETWEEN STRINGERS 27 - 28L. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201 REP 7. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201 - [SDR FDEA201409152614](https://openairdocs.org/sdr/FDEA201409152614), Sep 15, 2014: LIGHT. INOPERATIVE. L1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. L1 DOOR EXTERNAL LIGHT FILAMENT REPLACED. - [SDR FDEA201401180136](https://openairdocs.org/sdr/FDEA201401180136), Jan 18, 2014: SKIN. CORRODED. RIGHT SIDE OF FUSELAGE, STRINGER 26R LAP SEAM HAS FASTENERS PULLING THRU SKIN LAP SEAM AT BS 1670. EVIDENCE OF CORROSION. CUT OUT DAMAGE AT RT SIDE AT FUSELAGE, - [SDR FDEA201311292893](https://openairdocs.org/sdr/FDEA201311292893), Nov 29, 2013: UNKNOWN. MALFUNCTIONED. PDIS 933 73-10 0004481 28NOV13 RSW CLOSE LOG PAGES 02099057. NORMAL START LT ENG. DURING RT ENG START, THE LT ENG FAILED. FUEL FLOW WAS ZERO, EICAS MESSAGE LT E - [SDR FDEA201310302656](https://openairdocs.org/sdr/FDEA201310302656), Oct 30, 2013: SLIDE. DISLODGED. RIGHT ENTRY DOOR SLIDE FELL OUT WHEN OPENING DOOR. PILOT THOUGHT DOOR WAS DISARMED. FOUND DOOR OPEN AND SLIDE ON CREW STAIRS. R1 DOOR WAS IN ARMED POSITION. SLI - [SDR FDEA201301080048](https://openairdocs.org/sdr/FDEA201301080048), Jan 8, 2013: SKIN. CHAFED. MAIN EQUIPMENT CENTER ACCESS DOOR EXTERIOR HANDLE CUTOUT IS DAMAGED REMOVED DOOR IAW MM 52-48-02-4. COMPLIED WITH EA F-5230-152474 "DOORS-E & E SERVICE DOOR GOU - [SDR FDEA201301050025](https://openairdocs.org/sdr/FDEA201301050025), Jan 5, 2013: FRAME. CORRODED. AFT PIT-CORROSION ON LOWER FLANGE OF FRAME AT BS 1600 (AFT SIDE) RBL 5 TO LBL 5. CUT OUT DAMAGED SECTION OF STA 1600 BOTTOM CHORD, FABRICATED AND INSTALLED. REP - [SDR FDEA201301040017](https://openairdocs.org/sdr/FDEA201301040017), Jan 4, 2013: STRINGER SPLICE. CORRODED. CORROSION ON STRINGER SPLICE, BS 1180, STRINGER 28R. REMOVED DAMAGED STRINGER SPLICE IAW SRM 51-40-02. FABRICATED NEW SPLICE IAW DWG 140N0103, REV P AND INSTALL - [SDR FDEA201301040019](https://openairdocs.org/sdr/FDEA201301040019), Jan 4, 2013: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE, BS 1200 BETWEEN STR 28 AND 29L. REMOVED DAMAGED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW DWG 140N2006, REV B AND SRM 51- - [SDR FDEA201212304402](https://openairdocs.org/sdr/FDEA201212304402), Dec 30, 2012: STRINGER. CORRODED. CORROSION ON STRINGER 28R AT BS 1180. CUT OUT DAMAGED SECT OF STRINGER BS 1180-1194, FABIRCATED, AND INSTALLED REPAIR PARTS IAW SRM 53-00-03 R2. - [SDR FDEA201212144301](https://openairdocs.org/sdr/FDEA201212144301), Dec 14, 2012: GOVERNOR. MALFUNCTIONED. ON TAKEOFF ROLL, RT ENGINE WASN'T PROPER POWER, WOULD NOT MAINTAIN 1.59 EPR. ROLLED BACK TWICE. ABORTED T/O AT APROX 60 KTS, KNOB SPLIT BETWEEN LT AND RT THROTT - [SDR FDEA201211244150](https://openairdocs.org/sdr/FDEA201211244150), Nov 24, 2012: ENGINE. ODOR. AFTER TAKEOFF HAD A STRONG PACK ODOR. WENT AWAY AFTER A COUPLE MINUTES. R & R LT ENGINE. - [SDR FDEA201211053833](https://openairdocs.org/sdr/FDEA201211053833), Nov 5, 2012: GIRT BAR. LACK OF LUBE. RT CREW ENTRY DOOR SLIDE LIGHT INOPERATIVE. FOUND RT DOOR GIRT BAR SLIDERS WITH ALMOST NO GREASE ON SLIDERS CAUSING TO DRAG. LUBERCATED BOTH RT DOOR GIRT BAR SL - [SDR FDEA201209253425](https://openairdocs.org/sdr/FDEA201209253425), Sep 25, 2012: OXYGEN MASK. FAILED. CAPTAIN'S PRESS TO TEST AND RESET LEVER ON O2 BOX FAILS TO GIVE PROPER TEST NR O2 FLOW OR INTERMITTENT FLOW TO IRIS. SWAPPED CAPTAIN'S AND NR 2 COURIER O2 MASK - [SDR FDEA201205111791](https://openairdocs.org/sdr/FDEA201205111791), May 11, 2012: LAMP. INOPERATIVE. L1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD. All 462: https://openairdocs.org/aircraft/N933FD/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-21B aircraft: https://openairdocs.org/model/boeing-757-21b/aircraft.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.