- Registered owner
- Delta Air Lines Inc
- Location
- Atlanta, GA
- Owner type
- Corporation
- Serial number
- 38315
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- October 8, 2022
- Expires
- October 31, 2029
- Mode S code
- AD000D
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N937DZMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 737-9GPER aircraft
FAA incident reports
No FAA accident or incident reports matched to N937DZMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 737-9GPER aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2026072804364Control Rod · out of adjustCREW REPORTS L1 DOOR HANDLE POPPED UP AND INCH DURING TAKEOFF. ADJUSTED CONTROL ROD UPPER'S END FITTING. PRESSURIZED AIRCRAFT AGAIN, NO LONGER MOVES AND LATCHES REMAIN LOCKED. (1719591) AIRCRAFT WAS GROUNDEDSDR DALA2026032702026Handle · looseDURING TAXI IN 1L DOOR HANDLE POPPED UP. FWD ENTRY LIGHT ILLUMINATED. ADJUSTED CONTROL ROD AT UPPER LATCH TORQUE TUBE PER AMM 52-11. REPLACED FWD UPPER ROLLER PER CMM 52-16-12. PRESSURIZED A/C, DOOR CK OK.SDR DALA2025091506762Skin · damagedEXTERNAL FUSELAGE, PASSENGER WINDOW #32, 2 INCH ABOVE UPPER FRAME, FASTENER HAS LIGHTNING STRIKE DAMAGE (MARKED). LH SIDE. REPAIRED THE FUSELAGE EXTERNAL SKIN, 2" ABOVE #32 WINDOW UPPER FRAME IAW DELTA ER/A #629025-14, REV ORIGINAL AND ATS ER #25-02761, REV P1SDR DALA2025091006691Frame · corroded(LOG 1189449) REPAIR OF RIGHT-HAND STATION, 727 FRAME INNER CHORD. FABRICATED AND INSTALLED SHIM BETWEEN STA 727 FRAME INNER CHORD AND S-18A WEB, REPAIRED IN ACCORDANCE WITH 5311-01251-02B.SDR DALA2025091006690Frame · corroded(LOG 1189437) REPAIR OF LEFT-HAND STATION, 727 FRAME INNER CHORD. FABRICATED AND INSTALLED SHIM BETWEEN STA 727 FRAME INNER CHORD AND S-18A WEB, REPAIRED IN ACCORDANCE WITH CC#5311-01251-02A.SDR DALA2023091807641Unknown · unknown(LOG 8802008) EMERGENCY EXIT LIGHTS ON DURING FLT. ALSO BEEPING SOUND WHEN ILLUMINATED. R/R BATTERY CHARGER PACK M1673 PER B737 M/M 33-51 TASK 33-50-00. OPS NML.SDR DALA2023091807640Battery Pack · inoperative(LOG 8802006) DURING FLIGHT REAR EMERGENCY EXIT LIGHT ILLUMINATED. EMERG LTS NOT ILLUM. RESEATED AFT CABIN EMERG LTS BATT PACKS PER B737 AMM 33-51-06. PERFORMED OPS TEST PER B737 AMM 33-51-00.SDR DALA2023082206832Unknown · unknown(LOG 2927552) AFT CARGO FLOOR SUPPORT @ STA 797 S-26R HAS SINGS OF CORROSION AROUND FASTENER HOLE. LOCATED AND DRILLED NEW FLOOR SUPPORT PART # 146A7501-39 IAW B737 SRM 51-40-05. INSTALLED NEW AFT CARGO FLOOR SUPPORT AT RBL.13.84 FROM STA 727+4 TO STA 887 LAW SDR DALA2023081106555Unknown · unknown(LOG 2907257) FORWARD CARGO COMPARTMENT RH SIDEWALL GILLINER ATTACH ANGLE HAS CORROSION AT BS 500L BETWEEN STRINGERS 25R AND 26R. REMOVED AND REPLACED FWD CARGO COMPT RH SIDEWALL GILLINER ATTACH ANGLE AT BS 500L BETWEEN STRINGERS 25R AND 26R AND SUPPORT GUSSETSDR DALA2023081106551Unknown · unknown(LOG 2907474) FORWARD CARGO COMPARTMENT LH FLOOR TRANSITION PANEL UPPER SURFACE HAS AREAS OF CORROSION BETWEEN BS 500C + 15 TO BS 500L. REMOVED, FABRICATED, PERFORMED SPLICE REPAIR AND INSTALLED LH FLOOR TRANSITION PANEL BETWEEN BS 500C + 15 TO BS 500L AT FOWASDR DALA2023081106550Unknown · unknown(LOG 2907407) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL UPPER SURFACE HAS AREAS OF CORROSION BETWEEN BS 500A AND BS 500L. SECTION OF TRANSITION PANEL AT FWD CARGO R/H SIDE ,DIMENSIONS 94".750 AND 144".250, AND 1 SPLICE DIMENSIONS 8".750, AND 2EA DOUBSDR DALA2023081506644Slat · corroded(LOG 2841247) LT WING #2 SLAT TRAILING EDGE WEDGE HAS DAMAGE AT MID SECTION. REMOVED #2 SLAT IAW AMDS T/C: 2780-4522-02.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.