N941DN

No registry detail on file · not in current registry

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.

OTHER · 2019-02-21 Matched by certificate designator
ATA 3397

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)

Source: SDR DALA2019022201139
OTHER · 2019-01-29 Matched by certificate designator
ATA 3222

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)

Source: SDR DALA2019020100659
NO TEST · 2019-01-22 Matched by certificate designator
ATA 3397

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)

Source: SDR DALA2019012200399
Earlier reports · 2013–2018 · 40 reports

2018

OTHER · 2018-11-15 Matched by certificate designator
ATA 5310

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)

Source: SDR DALA2018111606645
OTHER · 2018-11-12 Matched by certificate designator
ATA 5350

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)

Source: SDR DALA2018111406630
OTHER · 2018-11-05 Matched by certificate designator
ATA 5312

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)

Source: SDR DALA2018110606475
OTHER · 2018-06-09 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA2018061203957
OTHER · 2018-05-24 Matched by certificate designator
ATA 5322

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)

Source: SDR DALA2018052503571
OTHER · 2018-05-24 Matched by certificate designator
ATA 5322

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.

Source: SDR DALA2018052503570
NO TEST · 2018-03-25 Matched by certificate designator
ATA 2560

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.

Source: SDR DALA2018032501878
OTHER · 2018-02-07 Matched by certificate designator
ATA 5532

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.

Source: SDR DALA2018020800760
OTHER · 2018-02-07 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA2018020800761
OTHER · 2018-02-07 Matched by certificate designator
ATA 5512

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.

Source: SDR DALA2018020700759
NO TEST · 2018-02-04 Matched by certificate designator
ATA 3350

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.

Source: SDR DALA2018020600715
NO TEST · 2018-02-04 Matched by certificate designator
ATA 3350

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.

Source: SDR DALA2018020600714

2017

NO TEST · 2017-11-06 Matched by certificate designator
ATA 3350

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.

Source: SDR DALA2017110607984
OTHER · 2017-10-21 Matched by certificate designator
ATA 5330

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.

Source: SDR DALA2017102707820
OTHER · 2017-07-27 Matched by certificate designator
ATA 2565

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 41,100 hrs · 34,090 cycles

L1 DOOR SLIDE PARACHUTE PINS NOT ENGAGED. REMOVED AND REPLACED SLIDE.

Source: SDR DALA2017080305942
OTHER · 2017-02-13 Matched by certificate designator
ATA 2560

Part: LANYARD — DISCONNECTED (L1 DOOR) · airframe 39,750 hrs · 33,378 cycles

L1 LANYARD HAS BECOME DISCONNECTED. REATTACHED.

Source: SDR DALA2017021701433

2016

OTHER · 2016-12-13 Matched by certificate designator
ATA 5210

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.

Source: SDR DALA2016121509953
OTHER · 2016-12-11 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA2016121309861
OTHER · 2016-12-09 Matched by certificate designator
ATA 2560

Part: LANYARD — UNSECURE (L1 DOOR) · airframe 39,226 hrs · 33,095 cycles

L1 DOOR LANYARD LATCH CAME LOOSE. SECURED LANYARD IAW MM.

Source: SDR DALA2016121309821
OTHER · 2016-11-28 Matched by certificate designator
ATA 3230

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.

Source: SDR DALA2016113009477
OTHER · 2016-11-12 Matched by certificate designator
ATA 5530

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.

Source: SDR DALA2016111308910
OTHER · 2016-11-10 Matched by certificate designator
ATA 5320

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.

Source: SDR DALA2016111108722
OTHER · 2016-11-10 Matched by certificate designator
ATA 5320

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.

Source: SDR DALA2016111108721
OTHER · 2016-11-10 Matched by certificate designator
ATA 5347

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.

Source: SDR DALA2016111108723
OTHER · 2016-11-10 Matched by certificate designator
ATA 5315

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.

Source: SDR DALA2016111108720
OTHER · 2016-11-08 Matched by certificate designator
ATA 5320

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.

Source: SDR DALA2016110908716
OTHER · 2016-11-08 Matched by certificate designator
ATA 5347

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.

Source: SDR DALA2016111108719
OTHER · 2016-11-08 Matched by certificate designator
ATA 5320

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.

Source: SDR DALA2016111108727
OTHER · 2016-11-08 Matched by certificate designator
ATA 5320

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.

Source: SDR DALA2016111108726
OTHER · 2016-11-08 Matched by certificate designator
ATA 5310

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)

Source: SDR DALA2016111108725

2015

OTHER · 2015-07-03 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA2015070904280
OTHER · 2015-06-11 Matched by certificate designator
ATA 2565

Part: SLIDE — UNSERVICEABLE · airframe 35,245 hrs · 30,669 cycles

VENTRAL DOOR AFT SLIDE UNSERVICABLE. R & R SLIDE IAW AMDS 5352-7116.

Source: SDR DALA2015061503808
OTHER · 2015-04-13 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA2015041502788
OTHER · 2015-02-10 Matched by certificate designator
ATA 5311

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.

Source: SDR DALA2015021101221
OTHER · 2015-02-10 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED · airframe 34,279 hrs · 30,087 cycles

HFEC INSPECTION OF OVERWING FRAME HAS A CRACK INDICATION. FRAME REPLACED IAW DWG SR90530027.

Source: SDR DALA2015021101219

2014

OTHER · 2014-05-06 Matched by certificate designator
ATA 5210

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.

Source: SDR DALA14029009241

2013

NO TEST · 2013-11-21 Matched by certificate designator
ATA 3350

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.

Source: SDR DALA13063599241
OTHER · 2013-08-16 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA13039939241
OTHER · 2013-03-05 Matched by certificate designator
ATA 2565

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.

Source: SDR DALA13010469241
OTHER · 2013-02-21 Matched by certificate designator
ATA 5330

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.

Source: SDR DALA13008729241