N932DS
Registered owner: BOEING CO, WA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
21 reports on file, 2022-06-08 – 2022-12-24.
Part: LIGHT — MISSING (CABIN) · airframe 23,608 hrs · 16,894 cycles
DURING THE 121 PRE-WALK FOR A/C 3935 IT WAS NOTICED THAT THERE WAS A FLOOR PROXIMITY EMERGENCY LIGHT LOCATED ON THE INBD EDGE OF THE G7 WINDSCREEN. LIGHT WAS MISSED ON THE INITIAL SURVEY OF THIS AIRCRAFT. ENGINEERING BULLETIN (EB) PROVIDES INSTRUCTIONS TO REMOVE & DEACTIVATE THE EXISTING EMERGENCY LIGHTS AS PART OF THE INSTALLATION. ER/A INSTRUCTS MAINTENANCE TO CAP AND STOW WIRING FOR THIS EMERGENCY LIGHTS AND INSTALL AN INOPERATIVE PLACARD ADJACENT TO THE LIGHT AS DIRECTED BY THE EB. THIS ALSO ELIMINATES THE NEED TO MAINTAIN THE ONE REMAINING EMERGENCY LIGHT.
Part: INTERCOSTAL — CORRODED (BS 492-500A S26R) · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
DURING INSPECTION FOUND CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS492 TO BS500A AT LEVEL STR26R AT FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL (SHIELD) LOCATED BETWEEN BS492 TO BS500A AT LEVEL STR26R AT FWD CARGO COMPARTMENT AS PER B737-900ERSRM 51-40-02 AND DRAWING 143A0080 SHEET 39.
Part: INTERCOSTAL — CORRODED (BS 500F-500G) · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
(LOG 2548136) DURING INSPECTION FOUND CORROSION WEB - INTERCOSTAL LOCATED FROM BS500F TO BS500G AND STR26R AT FWD CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL LOCATED FROM BS500F TO BS500G AND STR26R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-40-02, AND DWG 143A7505 SHEET 105.
Part: SUPPORT FITTING — CORRODED (BS 500I S19-13R) · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
(LOG 2548163) DURING INSPECTION FOUND CORROSION ANGLE - SUPPORT LOCATED AFT BULKHEAD BS500L AND FROM STR19R TO STR26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED AFT BULKHEAD BS500L AND FROM STR19R TO STR26R AT FWD CARGO COMPARTMENT AS PER B737-900 SRM51-10-02-0G ITEM 9 AND DWG:143A7902.
Part: CARGO TRACK — CRACKED (BS 727E-767) · airframe 23,608 hrs · 16,894 cycles
(LOG 2548120) DURING INSPECTION FOUND CRACK TRACK RBBL 13.84 LOCATED BTW BS 727E TO BS 767 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS SECTION I ON TRACK RBBL 13.84 LOCATED BTW BS 727E TO BS 767 ATAFT CARGO COMPARTMENT AS PER ER/A 603026-14.
Part: STRINGER — CRACKED (RT FUEL CELL) · airframe 23,608 hrs · 16,894 cycles
DURING INSPECTION FOUND CRACK FUEL TANK STRINGER U9 LOCATED BTW RIB 21 AND RIB 22 AT RT WING. PERFORMEDREPAIR INSTRUCTIONS ON FUEL TANK STRINGER U9 LOCATED BTW RIB 21 AND RIB 2 AT RT WING AS PER ER/A 602650-14.
Part: WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
(LOG 2548146) DURING INSPECTION FOUND CORROSION FLOOR STRUCTURE ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED FLOOR STRUCTURE WEB ASSY LOC BTW BS 767 TO BS 787 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT AS PER B737-900 SRM51-40-02 AND 51-10-02-0G ITEM 9 AND DWG 146A0081 SHEET 4 REV C.
Part: ANGLE — CORRODED · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
(LOG 2541302) DURING INSPECTION FOUND CORROSION FLOOR STRUCTURE TE ANGLE LOC. FLOOR BEAM BS 947.6 PLUS 4 INCHES AT LEVEL RBL 23 INCHES AT AFT GALLEY AREA. REPLACED TE ANGLE AT LEVEL OF FLOOR STRUCTURE LOC. FLOOR BEAM BS 947.6 PLUS 4 INCHES AT LEVEL RBL 23 INCHES AT AFT GALLEY AREA AS PER B737-900 SRM 51-40-02-0G, 51-10-02-0G ITEM 9, AND DWG 147A5650 SHEET 54 REV: A.
Part: SUPPORT FITTING — CRACKED (BS 727I-767 S25R) · airframe 23,608 hrs · 16,894 cycles
(LOG 2512944) DURING INSPECTION FOUND CRACK SUPPORT ZEE BTW BS 727I TO BS 767 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE BTW BS 727I TO BS 767 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT AS PER B737-900 SRM 51-42-00-0G, SRM 51-40-02-0G, ITEM 9, SRM 51-40-03 AND DWG 146A7500 SHEET 205 REV- 146A7502, SHEET 51 REV-0.
Part: GUSSET — CRACKED · airframe 23,608 hrs · 16,894 cycles
(LOG 2512930) DURING INSPECTION FOUND CRACKED BRACKET GUSSET LOCATED BS500L AND STR19R AT FWD CARGO COMPARTMENT. REPLACED BRACKET GUSSET LOCATED BS500L AND STR 19R AT FWD CARGO COMPARTMENT AS PER B737-900 ER SRM 51-10-02, ITEM 9 AND DWG 143A7902, SHEET 256/257 REV.B.
Part: PLATE — CORRODED · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
(LOG 2482311) DURING INSPECTION FOUND CORROSION FLOOR STRUCTURE SHIELD PLATE BTW BS 767 TO BS 791 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED FLOOR STRUCTURE SHIELD PLATE BTW BS 767 TO BS 791 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT AS PER B737-900ER 51-10-02ITEM 9 AND DWG 146A0081 SHEET 46.
Part: STRAP — CORRODED (BS 887 S25R-26L) · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
DURING INSPECTION FOUND CORROSION STRAP LOCATED ON BS 887 BTW STR 25R TO STR 26L AT AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED ON BS 887 BTW STR 25R TO STR 25R TO STR 26L AT AFT CARGO COMPARTMENT AS PER B737-900 SRM 51-40-02 AND SRM 51-10-02, ITEM 9 AND DWG 146A7500.
Part: WEB — CRACKED (FWD GALLEY) · airframe 23,608 hrs · 16,894 cycles
(LOG 2472318) DURING INSPECTION FOUND CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOC. BS 270 TO BS 294.5 BL 0 AT FWD GALLEY AREA. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOC. BS 270 TO BS 294.5 BL 0 AT FWD GALLEY AREA AS PER B737-900 SRM 51-10-02-0G ITEM 9 AND DWG 141A5410.
Part: NONE — NONE (NONE) · airframe 23,608 hrs · 16,894 cycles
(LOG 2472323) EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. BS 500B TO BS 500C BTW STR 24R TO STR 26R AT LOWER FUSELAGE. VERIFIED THAT REPAIR ON EXTERNAL LOC SKIN BS 500B TO BS 500C BTW STR 24R TO STR 26R AT LOWER FUSELAGE WELL MEETS THE GENERALREQUIREMENTS AS PER ER/A 598771-14AD REV.A.
Part: SUPPORT ANGLE — CRACKED (BS 500I-500J) · airframe 23,608 hrs · 16,894 cycles
(LOG 2459763) DURIN INSPECTION FOUND CRACK ANGLE-SUPPORT LOCATED FWD FACE OF FRAME FROM BS500I TO BS500J AT LEVEL STR26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE SUPPORT (3EA) LOC FWD FACE OF FRAME FROM BS 500I TO BS 500J AT LEVEL STR 26L AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 51-10-02 ITEM 9 AND DWG 143A7505.
Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 23,608 hrs · 16,894 cycles
(LOG 2457960) DURING INSPECTION FOUND CORROSION WEB - INTERCOSTAL FLOOR STRUCTURE LOC. BTW BS 947.5 TO BS 967 LBL 30 INCHES AT AFT GALLEY AREA. REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOC. BTW BS 947.5 TO BS 967 LBL 30 INCHES AT AFT GALLEY AREA AS PER B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A5650.
Part: CIRCUIT BREAKER — UNKNOWN (GALLEY) · airframe 23,608 hrs · 16,894 cycles
DUE TO A DISCREPANCY FOUND IN THE WIRING INSTALLATION OF THE FWD G1 GALLEY IN SAFRAN SB 501510-25-45 REV F, WHEN INSTALLING THE NEW BEVERAGE MAKER CIRCUIT BREAKER, ENGINEERING HAS DETERMINED THAT A REWORK IS NEEDED ON THE SAME INSTALLATION, AS THERE HAD BEEN NO FUNCTIONAL TEST PERFORMED TO DETERMINE IF THAT INSTALLATION WAS PERFORMED CORRECTLY. MAINTENANCE PERFORMED REWORK OF THE G1C GALLEY WIRING PER ERA 602966-14.
Part: NONE — NONE · airframe 23,608 hrs · 16,894 cycles
(LOG 2449348) DURING INSPECTION FOUND CRACK WEB TRAILING EDGE LOC BETWEEN DEFLECTION CONTROL RIBS AT LEVEL ORSS 261 AT LT WING. REPLACED WEB TRAILING EDGE LOC. BETWEEN DEFLECTION CONTROL RIBS AT LEVEL ORSS 261 AT LT WING AS PER B737-900ER SRM 51-10-02-0G, ITEM 9 AND DWG 115A2512.
Part: NONE — NONE · airframe 23,608 hrs · 16,894 cycles
(LOG 2439545) DURING INSPECTION FOUND CRACK WEB -INTERCOSTAL LOCATED FROM BS500C TO BS500D AND STR26L AT FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED FROM BS500C TO BS500D AND STR26L AT FWD CARGO COMPARTMENT AS PER B737-900 SRM 51-40-02, SRM51-10-02, AND DWG: 143A7505.
Part: SUPPORT FITTING — CRACKED · airframe 23,608 hrs · 16,894 cycles
(LOG 2434782) DURING INSPECTION FOUND CRACK ANGLE-SUPPORT LOCATED FWD AND AFT FACE BS500K AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE-SUPPORT LOCATED FWD AND AFT FACE BS500K AT LEVEL STR 26L AT FWD CARGO COMPARTMENT (2 EA) AS PER B737-900 SRM 51-40-02-0G ITEM 9, AND DWG 143A7505 SHEET 106
Part: NONE — NONE · airframe 23,608 hrs · 16,894 cycles
(LOG 2269788) DURING OPERATION BY LION AIR, PRIOR TO AIRCRAFT BEING OPERATED BY DELTA, A DENT WAS DISCOVERED IN THE FUSELAGE SKIN BETWEEN STA 500B AND STA 500C, STR 24R-25R. MAINTENANCE REPAIRED DAMAGE PER ERA 598771-14.