# Boeing 737-76Q - Type: Aircraft model (FAA registry) - Registry code: 13845AA - Manufacturer (registry): BOEING - Model: 737-76Q - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 149 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 2 - Page: https://openairdocs.org/model/boeing-737-76q 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 (2) - [N7815L](https://openairdocs.org/aircraft/N7815L): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2003, S/N 30288 - [N997AM](https://openairdocs.org/aircraft/N997AM): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 30283 ## 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 DCA16CA133](https://openairdocs.org/ntsb/DCA16CA133), Apr 14, 2016: Boeing 737 76Q (N565WN), San Diego, CA, no damage. Probable cause: the ramp agents failure to keep his right hand at a safe distance from the underside of the moving belt. - [NTSB ENG08IA042](https://openairdocs.org/ntsb/ENG08IA042), Oct 1, 2008: Boeing 737 (N551WN), Chicago, IL, incident, minor damage. Probable cause: The right nose landing gear axle's failure from intergranular and fatigue cracking due to an earlier bearing failure. - [NTSB NYC08CA115](https://openairdocs.org/ntsb/NYC08CA115), Feb 23, 2008: Boeing 737-700 (N551WN), Valdosta, GA, no damage. Probable cause: An unexpected encounter with turbulence, while on approach for landing. ## FAA accident and incident reports (2) 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 20110409010549I](https://openairdocs.org/incident/20110409010549I), Apr 9, 2011: Boeing 737-76Q (N550WN), Chicago, IL, Minor damage. N550WN departed ft. meyers (rsw) Florida as southwest flight #3588. Passing through FL200, crew heard a load pop, all other parameters normal. Aircraft… - [Incident 20080222839409I](https://openairdocs.org/incident/20080222839409I), Feb 22, 2008: Boeing 73776Q (N551WN), Orlando, FL, No damage. (-23) While at 30000' descending on the PICLT1 into mco, aircraft encountered turbulence. Flight attendant [privacy data omitted] thought he had a sprain in… ## Service difficulty reports (1,627, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR SWAA2026042890560](https://openairdocs.org/sdr/SWAA2026042890560), Apr 18, 2026: WEB. CRACKED. APB APEX DOME HAS SURFACE WEB CRACK AT STR23R FROM UPPER LH RIVET GOING TO CENTER EDGE OF DOME. REPAIRED PER EA 26-153-01061 WITH AN INSPECTION THRESHOLD DEFINE - [SDR SWAA2025122955746](https://openairdocs.org/sdr/SWAA2025122955746), Dec 26, 2025: REGULATOR. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09 - [SDR SWAA2025122956227](https://openairdocs.org/sdr/SWAA2025122956227), Dec 26, 2025: REGULATOR. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09 - [SDR SWAA2025122956228](https://openairdocs.org/sdr/SWAA2025122956228), Dec 26, 2025: VALVE. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI, ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09 - [SDR SWAA2025122956229](https://openairdocs.org/sdr/SWAA2025122956229), Dec 26, 2025: VALVE. LOW PRESSURE. AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09 - [SDR SWAA2025121651775](https://openairdocs.org/sdr/SWAA2025121651775), Dec 12, 2025: SCREW. MISSING. LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW. REPLACED LT OVERWING EMERGENCY EX - [SDR SWAA2025090912957](https://openairdocs.org/sdr/SWAA2025090912957), Sep 8, 2025: FSEU. FAULTED. TRAILING EDGE FLAPS INOPERATIVE. FIM 27-59 TASK 808 CARRIED OUT. OHMED FOR CONTINUITY, SHORTS, INSULATION RESISTANCE & DAR TEST IAW WDM 27-53-21. NO FINDINGS. R - [SDR SWAA2025090210292](https://openairdocs.org/sdr/SWAA2025090210292), Sep 1, 2025: SENSOR. FAULTED. AFTER PUTTING FLAP LEVER TO 5 THE FLAPS DID NOT EXTEND. WE NOTICED A VERY SMALL SPLIT IN THE TRAILING EDGE FLAPS. LE DEVICES WERE EXTENDED WITH THE ALTERNATE FL - [SDR SWAA2025082606374](https://openairdocs.org/sdr/SWAA2025082606374), Aug 20, 2025: CAP. MISSING. FORWARD CARGO DOOR HANDLE HAS MISSING STUD CAP. INSTALLED STUD CAP IAW AMM 52-31-14. - [SDR SWAA2025082206375](https://openairdocs.org/sdr/SWAA2025082206375), Aug 20, 2025: HANDLE. MISSING. AFT CARGO DOOR HANDLE HAS MISSING STUD CAP<[01] REMOVED AND REPLACED AFT CARGO DOOR HANDLE STUD CAP REFERENCE AMM52-31-14. - [SDR SWAA2025081804438](https://openairdocs.org/sdr/SWAA2025081804438), Aug 14, 2025: FLAP SYSTEM. FAULTED. AS WE WERE ABOUT TO SELECT FLAPS 1 (210KTS) WE NOTICED THE FLAP GAUGE INDICATING ZERO - ONE ON RT SIDE. WHEN WE SELECTED F1 THE FLAPS/SLATS DID NOT EXTEND. SELE - [SDR SWAA2025081299599](https://openairdocs.org/sdr/SWAA2025081299599), Aug 8, 2025: GIRT BAR. DAMAGED. FWD ENTRY DOOR GURT BAR HOOK HAS MISSING RIVET. INSTALLED NEW RIVET IN FWD ENTRY GURT BAR HOOK REF SIP - [SDR SWAA2025062785458](https://openairdocs.org/sdr/SWAA2025062785458), Jun 25, 2025: SKIRT. OUT OF POSITION. AFT ENTRY DOOR SLIDE EXCESSIVE FABRIC<[01] REPOSITIONED AFT ENTRY SKIRT SLIDE PER AMM 25-66-01 AND TASK MT 725-61-06. - [SDR SWAA2025060276185](https://openairdocs.org/sdr/SWAA2025060276185), May 28, 2025: GIRT BAR. LOOSE. R1 DOOR GIRT BAR LOOSE <[01]. RE-SECURED R1 DOOR GIRT BAR RETAINER CLIPS PER AMM 25-66-01. OPS CHK GOOD. - [SDR SWAA2025051971778](https://openairdocs.org/sdr/SWAA2025051971778), May 15, 2025: SLIDE. LOOSE. R1 SLIDE CAME LOOSE. REINSTALLED SLIDE PER MT#25-66-01. - [SDR SWAA2025050667536](https://openairdocs.org/sdr/SWAA2025050667536), May 4, 2025: SIGN. INOPERATIVE. CREW REPORTS OVER WING EMERGENCY EXIT INDICATOR LIGHT INOP. REMOVED AND REPLACED EXIT INDICATOR SIGN PER AMM 33-51-01. - [SDR SWAA2025050622175](https://openairdocs.org/sdr/SWAA2025050622175), Apr 7, 2025: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY BAT - [SDR SWAA2025050608576](https://openairdocs.org/sdr/SWAA2025050608576), Mar 23, 2025: STRIP. CRACKED. FWD CARGO BAY SIDEWALL PNL 122AW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE7;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; - [SDR SWAA2025050615939](https://openairdocs.org/sdr/SWAA2025050615939), Mar 23, 2025: STRIP. CRACKED. FWD CARGO BAY SIDEWALL PNL 122EW CAPSTRIP CRACKED<[01] RECEIVED NEW CAPSTRIP; CAPSTRIP WILL BE INSTALLED ON TTG8Q00YJCE1;[02] VERIFIED CORRECTIVE ACTION ENTRY 1 - [SDR SWAA2025050615928](https://openairdocs.org/sdr/SWAA2025050615928), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02;[02] OK TO INSTALL;[03] REMOVED AND REPLACED NEW STRINGE - [SDR SWAA2025050615929](https://openairdocs.org/sdr/SWAA2025050615929), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02;[02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S-7L - [SDR SWAA2025050615930](https://openairdocs.org/sdr/SWAA2025050615930), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-4R. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP BS727D S-4R PER DWG 146A1111 - [SDR SWAA2025050615931](https://openairdocs.org/sdr/SWAA2025050615931), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727A S-5R. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02. REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A S-5R PER DWG 146A1 - [SDR SWAA2025050606638](https://openairdocs.org/sdr/SWAA2025050606638), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727B S-5R. MARKED. REMOVED AND REPLACED NEW STRINGER CLIP BS727B S-5R PER DWG 146A1103 REV D AND SRM 51-40-02. CORRECTIVE ACTION - [SDR SWAA2025040906636](https://openairdocs.org/sdr/SWAA2025040906636), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED <[01]. REMOVED STR CLIP AT BS727D S-6L IAW SRM 51-40-02; [02] OK TO INSTALL; [03] REMOVED AND REPLACED NEW STR - [SDR SWAA2025040906637](https://openairdocs.org/sdr/SWAA2025040906637), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED <[01]. REMOVED SRT CLIP AT BS727C S-7L IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727C S- - [SDR SWAA2025040906639](https://openairdocs.org/sdr/SWAA2025040906639), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED <[01]. REMOVED STR CLIP AT BS727D S-4R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP BS727D S- - [SDR SWAA2025040906640](https://openairdocs.org/sdr/SWAA2025040906640), Mar 18, 2025: STRINGER CLIP. CRACKED. CRACKED STR CLIP AT PAX CABIN BS727A S-5R. MARKED <[01]. REMOVED STR CLIP AT BS727A S-5R IAW SRM 51-40-02; [02] REMOVED AND REPLACED NEW STRINGER CLIP AT BS727A - [SDR SWAA2025050606464](https://openairdocs.org/sdr/SWAA2025050606464), Mar 17, 2025: SKIN. CORRODED. CORROSION ON UPPER FUSELAGE SKIN UNDER VERTICAL STAB LBL12 TO RBL12 BS1016 - BS1078 WL308.5. MARKED<[01] UPDATED TABLE; COMPLETED STEP 9.;[02] ' AS PER EA 25-15 - [SDR SWAA2025040906466](https://openairdocs.org/sdr/SWAA2025040906466), Mar 17, 2025: ANGLE. CORRODED. CORROSION ON ANGLE UNDER VERTICAL STAB BS1036 LBL2 WL308.5. MARKED <[01]. ADDED DIMENSIONS TO STEP 2. - [SDR SWAA2025050615901](https://openairdocs.org/sdr/SWAA2025050615901), Mar 15, 2025: PLATE. CRACKED. WIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4. VERIFIED CORRECTIVE ACTION - [SDR SWAA2025040905686](https://openairdocs.org/sdr/SWAA2025040905686), Mar 15, 2025: PLATE. CRACKED. WIGGLE PLATE ON L/W T/E ORSS 261 IS CRACKED <[01]. REMOVED AND REPLACED WIGGLE PLATE ON L/W T/E AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA. 4.; [02] VERIFIED CORREC - [SDR SWAA2025050605541](https://openairdocs.org/sdr/SWAA2025050605541), Mar 14, 2025: SCUFF PLATE. CRACKED. ACB FWD CORNER SCUFF PLATE CRACKED(MARKED)<[01] 04 - REPAIRED PER [SRM 53-60-15-2R-1-A00967 (REPAIR 1 - AFT CARGO DOOR SURROUND STRUCTURE - PERMANENT)] - [SDR SWAA2025050639172](https://openairdocs.org/sdr/SWAA2025050639172), Mar 13, 2025: ATTACH FITTING. CORRODED. CORROSION ON LEFT WING FRONT SPAR AROUND BOOST PUMP UPPER BONDING STRAP ATTACHMENT POINT - IFSS 121.<[01] REPAIRED CORROSION ON LEFT WING FRONT SPAR BOOST PUMP - [SDR SWAA2025050615880](https://openairdocs.org/sdr/SWAA2025050615880), Mar 13, 2025: PRESSURE DECK. CRACKED. CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED)<[01] REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT BS - [SDR SWAA2025040905218](https://openairdocs.org/sdr/SWAA2025040905218), Mar 13, 2025: PRESSURE DECK. CRACKED. CRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+8' RBL 40 L: 0.6'( MARKED) <[01]. REMOVED AND REPLACED BEADED PRESSURE DECK WEB SECTION AT - [SDR SWAA2025050604854](https://openairdocs.org/sdr/SWAA2025050604854), Mar 12, 2025: STRUT. CRACKED. L/H MLG GEAR STRUT DOOR IS CRACKED<[01] UPDATED STEPS 1;2 FOR REMOVAL L/H MLG SHOCK STRUT DOORS;[02] COMPLETED STEPS 2;4;[03] COMPLETED STEP 1 INSTALL L/H MLG S - [SDR SWAA2025022699482](https://openairdocs.org/sdr/SWAA2025022699482), Feb 24, 2025: LENS. MISSING. L/H OVER WING EMERGENCY EXIT LIGHT LENS COVER MISSING<[01] INSTALLED L/H OVER WING EMERGENCY EXIT LUGHT LENS COVER PER SIP - [SDR SWAA2025022699061](https://openairdocs.org/sdr/SWAA2025022699061), Feb 23, 2025: CONTROL UNIT. MALFUNCTIONED. INTERMITTANT RIGHT WING/BODY OVERHEAT LIGHT ON APPROACH LIGHT EXTINGUISHED SHORT AFTER ILLUMINATION<[01] PERFORMED COMPARTMENT OVERHEAT DETECTION CONTROL UNIT B - [SDR SWAA2025012789283](https://openairdocs.org/sdr/SWAA2025012789283), Jan 24, 2025: SHROUD. MISINSTALLED. FWD ENTRY DOOR SLIDE SHROUD NOT INSTALLED PROPERLY AT BOTTOM CENTER OF SHROUD<[01] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01-400-801.;[02] INSTA - [SDR SWAA2025012788590](https://openairdocs.org/sdr/SWAA2025012788590), Jan 22, 2025: LIGHT. INOPERATIVE. EMERGENCY LIGHT L1065 INOP APROX STA 480 LEFT<[01] RELAMPED EMERGENCY LIGHT L1065 APROX STA 480 LEFT; PERFORMED GOOD TEST PER AMM 33-51-03-960-801;[02] VERIFIED - [SDR SWAA2025012388436](https://openairdocs.org/sdr/SWAA2025012388436), Jan 22, 2025: ELEC CONNECTOR. DISCONNECTED. EMERGENCY EXIT CEILING LIGHT L1419 INOP.<[01] PERFORMED TROUBLESHOOTING FOUND CONNECTOR D40038J DISCONNECT. RECONNECTED CONNECTOR D40038P FOR THE EMERGENCY LIGH - [SDR SWAA2025012385910](https://openairdocs.org/sdr/SWAA2025012385910), Jan 14, 2025: SEAT TRACK. CRACKED. PASSENGER CABIN SEAT TRACK AFT FASTENER HEAD HAS A CRACK AT BS 727B; RBL 24.75. (MARKED)<[01] FINISHED PER EA-25-153-00101;[02] VERIFIED CORRECTIVE ACTION COMPL - [SDR SWAA2025012884184](https://openairdocs.org/sdr/SWAA2025012884184), Jan 8, 2025: TRACK. CRACKED. RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT IAW AMM 27-41-31-400-802.; [02] VER - [SDR SWAA2025012283949](https://openairdocs.org/sdr/SWAA2025012283949), Jan 7, 2025: SCUFF PLATE. CRACKED. FCB FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED IAW SRM 53-30-15-2R-1; NDI CRACK FREE; FCB FWD CORNER SCUFF PLATE;[02] VERIFIED ALL STEPS; CORRECTION ACTION IT - [SDR SWAA2025012283947](https://openairdocs.org/sdr/SWAA2025012283947), Jan 7, 2025: SCUFF PLATE. CRACKED. ACB AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIED - [SDR SWAA2025012283948](https://openairdocs.org/sdr/SWAA2025012283948), Jan 7, 2025: SCUFF PLATE. CRACKED. ACB FWD CORNER SCUFF PLATE CRACKED<[01] VERIFIED - [SDR SWAA2025012283447](https://openairdocs.org/sdr/SWAA2025012283447), Jan 6, 2025: FLOORBEAM. CRACKED. BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED RBL1; WL208<[01] REOMOVED AND REPLACED NEW FLOOR SUPPORT (PANEL BREAK) BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG - [SDR SWAA2025012283452](https://openairdocs.org/sdr/SWAA2025012283452), Jan 6, 2025: FLOORBEAM. CRACKED. BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED LBL1; WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT (PANEL BREAK) BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A - [SDR SWAA2025012083130](https://openairdocs.org/sdr/SWAA2025012083130), Jan 5, 2025: FLOOR PANEL. PULLED. PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABR All 1,627: https://openairdocs.org/model/boeing-737-76q/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.