N941DN
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.
43 reports on file, 2013-02-21 – 2019-02-21.
Part: WIRE — DAMAGED (CABIN LIGHTS) · airframe 44,899 hrs · 36,427 cycles
MISCELLANEOUS LIGHTS-CABIN & LAVATORY OCCUPIED LIGHTS AFT C/B POPPED. FOUND AFT FLT ATT PANEL SIDEWALL LT SWITCH AND SEVERAL WIRES DAMAGED RPLD SEVERAL WIRES FROM P1-2203 AND RPLCD AFT ATT SIDE WALL LIGHT RHEOSTAT. REPLACED WIRES PER MD 90 WDM:33-23-12. OPS CHECK GOOD.. A/C OK FOR SVC. (LP# 5280854)
Part: DEFLECTOR — MISSING (LT NLG) · airframe 44,776 hrs · 36,332 cycles
LT NOSE LANDING GEAR DEBRIS DEFLECTOR MISSING. REPLACED LEFT NOSE GEAR DEBRIS DEFLECTOR PER MD90 AMM 32-37. REM CDL/PLACARD. (LP# 3794464)
Part: WIRE — PULLED (CATWALK) · airframe 44,694 hrs · 36,279 cycles
EMERGENCY LIGHT IN AFT CATWALK INOP. FOUND WIRE PULLED OUT OF ASSY. REPINED WIRE REF SWP CHAP 20 OPS CKS OK. (LP# 3794445)
Earlier reports · 2013–2018 · 40 reports
2018
Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · airframe 44,308 hrs · 36,024 cycles
HIDDEN CORROSION: CORROSION LOWER JAMB AT AFT CARGO COMPARTMENT BELOW SCUFF PLATE AREA. SUMMARY OF NRC 00199 CORROSION LEVEL I, CORROSION ON LOWER JAMB WAS REMOVED PER MD-90 VOL.II SRM 51-10-03 PAR.26 (UT) WAS ACCOMPLISHED PER NDT 04-00-07 PAR.5 FIG.3 SHEET 1&2 ORIGINAL THICKNESS ON LOWER JAMB IS 0.160" AND MINIMUM REMAINING THICKNESS IS 0.145" . THEREFORE IT IS WITHIN LIMITS PER MD-90 VOL.I SRM 53-60-02 PAR.11 FIG.9 (SHEET 2). (LP# 0828103)
Part: BOTTLE — LOW PRESSURE (TAILCONE RELEASE) · airframe 44,308 hrs · 36,024 cycles
LOW PRESSURE ON TAILCONE JETTISON BOTTLE. SERVICING OF THE TAILCONE NITROGEN CYLINDER - (20011201) WAS PERFORMED PER MD-90 AMM 12-18-01-612-801 STAYING IN TEMPERATURE: 58F, PRESSURE: 2200 PSI. (LP# 0823822)
Part: SUPPORT BRACKET — BROKEN (BS 110 BULKHEAD) · airframe 44,308 hrs · 36,024 cycles
BROKEN ANGLE SUPPORT BRACKET (2EAS) IN FORWARD PRESSURE BULKHEAD, FWD FACE STA Y=110 AND X=-9. (FYT). ANGLE SUPPORT BRACKET (2EAS) IN FORWARD PRESSURE BULKHEAD, FWD FACE STA Y=110 AND X=-9 WERE REPLACED PER MD90 VOL II SRM 51-30-05 AND DWG 5912616 REV. CK. (LP# 0815193)
Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 43,286 hrs · 35,395 cycles
DURING INSP OF DOOR MOUNT WC 2561-2001 FOUND SLIDE PINS DISENGAGE. R&R L1 DOOR SLIDE PER WC 2561-4641. OPS CK GOOD. OK FOR SERVICE.
Part: SHEAR TIE — CRACKED (BS 522) · airframe 43,165 hrs · 35,320 cycles
FRAME STA 522 FORMER SKIN ATTACH ANGLE CRACKED BELOW STRINGER 19R (DUE GROUND INCIDENT). REMOVED DAMAGED FORMER P/N 9911525-42 FOR DOUBLER FABRICATION. FABRICATED, TREATED AND PAINTED REPAIR PARTS PER MD90 SRM 53-10-02. INSTALLED REPAIR PARTS. (LP#0569260)
Part: SHEAR TIE — DAMAGED (BS 503) · airframe 43,165 hrs · 35,320 cycles
BS 503 SKIN FRAME ATTACH ANGLE WAS DAMAGED BELOW STRINGER 19R. REMOVED FORMER 9957916-44 AND SENT TO PMSG FOR DOUBLER FABRICATION. COMPLIED WITH ALL OPEN FASTENER HOLES HFEC INSP IAW MDC93K0393- NDT SPM PART 06-10-01.003. FABRICATED A REPAIR IAW SRM 53-10-02. TREATED AND PAINTED REPAIR PARTS . INSTALLED THE REPAIR IAW SRM 53-10-02.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 42,794 hrs · 35,105 cycles
FOUND FLASHLIGHT UNDER F/A SEAT BY L1 DOOR OUT OF HOLSTER AND LIGHT NOT ILLUMINATED. FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED FLASHLIGHT AND CRADLE ASSY PER MD90 AMM 25-60. CHECKED GOOD. REPLACED EMERGENCY STRAP.
Part: INLET — CRACKED (RAM AIR) · airframe 42,424 hrs · 34,896 cycles
CRACK RT SIDE OF RAM AIR INLET. HFEC OF CRACK IAW NDT SPM 06-10-01.001. WELDED CRACK IAW ER/A 382101-MA NO FLAWS NOTED. ALODINED DAND PRIMED THE AREA IAW ER/A 382101-14MA.
Part: SLIDE — DAMAGED (TAILCONE) · airframe 42,424 hrs · 34,896 cycles
FOUND TAILCONE SLIDE EXPANDED. REMOVED AND REPLACED THETAILCONE SLIDE ASSY IAW AMI 2561-4643-02. OK FOR SERVICE.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 42,424 hrs · 34,896 cycles
RIGHT HORIZONTAL STABILIZER UPPER AFT SKIN SHOWS CRACK INDICATIONS DURING LFEC IAW AMDS 5510-01073-02, APPROXIMATELY .375 INCHES LONG. VERIFIED THE CRACK INDICATION. WORKED THE SKIN IAW AMDS 5510-01073-08. OK FOR SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,424 hrs · 34,896 cycles
AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-230 IAW MM. OPERATION CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,424 hrs · 34,896 cycles
CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACE BATTERY PACK B5-227 IAW MM. OPERATION CHECKS GOOD.
2017
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,806 hrs · 34,527 cycles
WHILE PERFORMING A SERVICE CHECK, FOUND THE SIDEWALL EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR INOPERATIVE. INSTALLED A NEW BATTERY POWER SUPPLY.
Part: SKIN — DENTED (BS 233) · airframe 41,753 hrs · 34,491 cycles
GATE AGENT REPORTED A DENT JUST AFT OF THE L1 DOOR. THE DENT AT BS 233 BETWEEN STRINGER 7 AND 8L. BLENDED THE DAMAGE AND PERFORMED HFEC INSPECTION, NO CRACKS NOTED. REPAIRED IAW ERA 562847-14.
Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 41,100 hrs · 34,090 cycles
L1 DOOR SLIDE PARACHUTE PINS NOT ENGAGED. REMOVED AND REPLACED SLIDE.
Part: LANYARD — DISCONNECTED (L1 DOOR) · airframe 39,750 hrs · 33,378 cycles
L1 LANYARD HAS BECOME DISCONNECTED. REATTACHED.
2016
Part: DOOR — DAMAGED (L1) · airframe 39,269 hrs · 33,117 cycles
FORWARD L1 CABIN DOOR BOTTOM FORWARD EDGE HAS DAMAGE. REWORKED DAMAGE IAW SRM 52-00-01.
Part: SLIDE — DAMAGED (L1 DOOR) · airframe 39,234 hrs · 33,098 cycles
L1 DOOR SLIDE PINS PULLED OUT. REMOVED AND REPLACED L1 SLIDE ASSEMBLY IAW MM.
Part: LANYARD — UNSECURE (L1 DOOR) · airframe 39,226 hrs · 33,095 cycles
L1 DOOR LANYARD LATCH CAME LOOSE. SECURED LANYARD IAW MM.
Part: CABLE — BROKEN (LANDING GEAR) · airframe 39,167 hrs · 33,051 cycles
PERFORMED AN AIR TURN BACK TO ATL DUE TO LANDING GEAR HANDLE WOULD NOT GO UP. CREW REPORTS GEAR HANDLE WOULD NOT GO PAST MID POSITION. PLACED LEVER BACK IN DOWN POSITION, HAD ALL 3 GEAR GREEN LIGHTS AND GEAR DOORS CLOSED. NORMAL LANDING. FOUND ANTI-RETRACTION CABLE SEGMENT 118A BROKEN. REPLACED WITH SERVICEABLE CABLE SEGMENT REF AMM 32-31-06. PERFORMED LANDING GEAR EXT/RETRACT TEST. NORMAL AND ALTERNATE TEST GOOD. ALL OPERATIONS NORMAL PER AMM 32-30-00.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 39,127 hrs · 33,025 cycles
VERTICAL ATTACH ANGLE LEFT HAND SIDE IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-02, 51-30-05 AND DWG 5912188, REV BD.
Part: ANGLE — CRACKED (BS 1520) · airframe 39,127 hrs · 33,025 cycles
AFT ACCESSORY COMPARTMENT ON FRAME BS 1520 STRINGER 18L ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-02 AND DWG 9915634.
Part: BRACKET — CRACKED (BS 1486) · airframe 39,127 hrs · 33,025 cycles
CRACKED BRACKET LONGERON 2R, BS 1486. REMOVED, FABRICATED AND INSTALLED BRACKET IAW SRM 51-30-02.
Part: SEAT TRACK — CORRODED (BS 200-257) · airframe 39,127 hrs · 33,025 cycles
SEAT TRACK LBL44 HAS CORROSION FROM BS 200 - 257. REMOVED, FABRICATED AND INSTALLED A NEW SECTION OF SEAT TRACK IAW SRM 53-40-01.
Part: FLOORBEAM — CORRODED (BS 1364) · airframe 39,127 hrs · 33,025 cycles
AFT CARGO, CORROSION ON AFT SIDE OF FLOORBEAM, BS 1364, BL 0 - RBL 20. REPAIRED.
Part: ANGLE — CRACKED (BS 1475) · airframe 39,127 hrs · 33,025 cycles
AFT ACCESSORY COMPARTMENT, BS 1475, LONGERON 15L ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED A NEW ANGLE IAW SRM 51-30-05 AND DWG 9964460, REV AA AND AB.
Part: SEAT TRACK — DAMAGED (BS 209) · airframe 39,127 hrs · 33,025 cycles
SEAT TRACK LBL 22 HAS ELONGATED HOLE AT BS 209. REMOVED AND REPLACED THE SECTION SECTION OF SEAT TRACK FROM BS 200 - 327 IAW SRM 53-20-01 AND 53-40-01.
Part: CUSP WEB — PUNCTURED (BS 882) · airframe 39,127 hrs · 33,025 cycles
CUSP WEB HAS A SMALL PUNCTURE BS 882. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-20-02.
Part: SUPPORT — CRACKED (LT MLG WW) · airframe 39,127 hrs · 33,025 cycles
LEFT MLG WHEEL WELL FORWARD DOOR CUT OUT INBOARD SUPPORT CRACKED. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-05.
Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 39,127 hrs · 33,025 cycles
RIGHT MLG WHEEL WELL FORWARD DOOR CUT OUT INBOARD SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-30-05. (LP# 2760997)
2015
Part: LANYARD — UNSECURE (L1 DOOR SLIDE) · airframe 35,437 hrs · 30,776 cycles
L1 DOOR SLIDE LANYARD FOUND LOOSE. R & R THE SLIDE IAW AMDS 2561-4641.
Part: SLIDE — UNSERVICEABLE · airframe 35,245 hrs · 30,669 cycles
VENTRAL DOOR AFT SLIDE UNSERVICABLE. R & R SLIDE IAW AMDS 5352-7116.
Part: PIN — MISSING (L1 DOOR SLIDE) · airframe 34,787 hrs · 30,381 cycles
L1 SLIDE PIN NOT INSTALLED. R & R L1 DOOR SLIDE IAW AMDS 2561-4641.
Part: FRAME — CRACKED (BS 962) · airframe 34,279 hrs · 30,087 cycles
ON HFEC INSPECTION OF OVERWING FRAME, BS 962, HAD A CRACK INDICATION. R & R THE FRAME, IAW AMDS 5310-01375-09 LT.
Part: FRAME — CRACKED · airframe 34,279 hrs · 30,087 cycles
HFEC INSPECTION OF OVERWING FRAME HAS A CRACK INDICATION. FRAME REPLACED IAW DWG SR90530027.
2014
Part: STRUCTURE — BENT (L1 DOOR) · airframe 32,400 hrs · 28,884 cycles
L1 DOOR BENT AT BOTTOM EDGE IN A 6 INCH SECTION. STRAIGHTENED L1 DOOR FLANGE IAW SRM 52-00-01.
2013
Part: GROUND WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 31,256 hrs · 28,188 cycles
PILOT REPORTED EMERGENCY LIGHTS ILLUMINATED WHEN ENTRY AND F/A LIGHTS ARE TURNED ON. THEY GO OUT WHEN ENTRY AND F/A LIGHTS ARE TURNED OFF. MAINTENANCE FOUND LOOSE GROUND WIRES ON OVERHEAD LIGHT ASSEMBLY. SECURED WIRE. OPS CHECKED NORMAL.
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 30,540 hrs · 27,726 cycles
L1 DOOR FOUND EMERGENCY SLIDE PACK NOT SECURED. MX R & R L1 SLIDE ON WC 2500-4332.
Part: LANYARD — DAMAGED (TAILCONE SLIDE) · airframe 29,309 hrs · 26,979 cycles
DURING SERVICE CHECK, FOUND TAILCONE LANYARD HARNESS DAMAGED. R & R TAILCONE LANYARD HARNESS IAW AMM.
Part: SKIN — CORRODED (TAIL SKID) · airframe 29,306 hrs · 26,977 cycles
TAIL SKID INNER SURFACE CORRODED AROUND BOLT HOLES. MRB 53-303-03. REMOVED CORROSION AND ALODINED AREA ON TAIL SKID INTERIOR IAW SRM 51-10-03. FOUND TO BE WITHIN LIMITS. TREATED, PRIMED AND TOP COATED ER/A 504825, REV O AND SRM 51-10-03.