N957DN

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.

49 reports on file, 2012-03-22 – 2016-10-26.

OTHER · 2016-10-26 Matched by certificate designator
ATA 3350

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 50,440 hrs · 28,826 cycles

EMERGENCY LIGHT LENS DAMAGED. REPAIRED.

Source: SDR DALA2016102707789
OTHER · 2016-06-26 Matched by certificate designator
ATA 2565

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 49,682 hrs · 28,359 cycles

L1 DOOR SLIDE UNLACED. REMOVED AND REPLACED L1 DOOR SLIDE.

Source: SDR DALA2016062905131
WARNING INDICATION · 2016-06-03 Matched by certificate designator
ATA 2133

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 49,484 hrs · 28,220 cycles

AUTO 1 AND 2 PRESSURIZATION FAILED IN FLIGHT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND AUTO 1 AND 2 INOPERATIVE. R & R OUTFLOW ACTUATOR IAW MM. OPERATION CHECKS GOOD.

Source: SDR DALA2016060604495
OTHER · 2016-04-16 Matched by certificate designator
ATA 7200

Part: TURBINE CASE — CRACKED (LT ENGINE) · airframe 49,140 hrs · 28,017 cycles

LEFT ENGINE AFT VIBRATOR ISOLATOR THERMAL OVERHEATING FROM CRACK IN TURBINE CASE. R & R AFT VIBRATIONS ISOLATOR IAW MM.

Source: SDR DALA2016041803161
OTHER · 2016-04-13 Matched by certificate designator
ATA 5311

Part: FRAME — WORN (BS 883) · airframe 49,140 hrs · 28,017 cycles

OVERWING FRAME, BS 883 RT HAS WEAR ON UPPER RADIUS OF THE FRAME TAB FROM THE CUSP WEB. REPAIRED IAW ERA 545329-14AD, REV O.

Source: SDR DALA2016041402922
OTHER · 2016-04-13 Matched by certificate designator
ATA 5311

Part: FRAME — WORN (BS 883) · airframe 49,140 hrs · 28,017 cycles

OVERWING FRAME, BS 883 LT HAS WEAR ON UPPER RADIUS OF THE FRAME TAB FROM THE CUSP WEB. REPAIRED IAW ERA 545329-14AD.

Source: SDR DALA2016041402921
OTHER · 2016-04-09 Matched by certificate designator
ATA 5340

Part: MOUNT — CRACKED (LAVATORY) · airframe 49,140 hrs · 28,017 cycles

FORWARD LAV AFT MOUNT FLOOR FITTING CORRODED AND CRACKED. FABRICATED AND INSTALLED FITTING IAW DWG.

Source: SDR DALA2016041002846
OTHER · 2016-04-08 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 1494) · airframe 49,140 hrs · 28,017 cycles

TAIL INTERIOR LONGERON L3R CRACKED, BS 1494. REPAIRED IAW SRM 53-10-01.

Source: SDR DALA2016041102847
OTHER · 2016-04-08 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 1475) · airframe 49,140 hrs · 28,017 cycles

LONGERON 2L CRACKED AT BS 1475. REPAIRED IAW PRI/ERA 545446-14, REV O.

Source: SDR DALA2016040902845
OTHER · 2016-04-08 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 1481-1483) · airframe 49,140 hrs · 28,017 cycles

FUSELAGE EXTERIOR SKIN CRACKED AT 3 LOCATIONS, BS 1483 AND BS 1481 BETWEEN L2R AND L4R RT SIDE. COMPLIED WITH ERA 545389-14, REV O.

Source: SDR DALA2016040802844
OTHER · 2016-04-07 Matched by certificate designator
ATA 5340

Part: FITTING — CORRODED (GALLEY) · airframe 49,140 hrs · 28,017 cycles

G2 AFT INBD FITTING CORRODED. REPAIRED IAW DWG C712071.

Source: SDR DALA2016040802843
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 200-128) · airframe 49,140 hrs · 28,017 cycles

CORROSION UNDER G7 GALLEY AND FORWARD LAVATORY FLOOR SUPPORTS, BS 200-BS 218, LBL 18. REPAIRED IAW SRM 53-00-01 AND DWG 9936534 AND 9936535.

Source: SDR DALA2016040602719
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR SUPPORT, BS 200. OUT OF LIMITS. REPLACED IAW DWG 9936534.

Source: SDR DALA2016040602835
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 177-181) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR SUPPORT, BS 177 TO 181. REPLACED IAW DWG 9936534.

Source: SDR DALA2016040602841
OTHER · 2016-04-06 Matched by certificate designator
ATA 5321

Part: FLOORBOARD — CORRODED (BS 195) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOORBOARD WEB AT BS 195. REPAIRED IAW SRM 51-11-01.

Source: SDR DALA2016040602834
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (BS 196-200) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR WEB, BS 196-200. REPAIRED IAW SRM 51-11-01.

Source: SDR DALA2016040602723
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (BS 192) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR WEB, BS 192. REPAIRED IAW SRM 53-20-02 AND 51-11-01.

Source: SDR DALA2016040602722
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR SUPPORT, BS 200. REPLACED IAW DWG 9936534.

Source: SDR DALA2016040602836
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (BS 200) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR WEB, BS 200.5. REPAIRED IAW SRM 51-11-01.

Source: SDR DALA2016040602721
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR SUPPORT, BS 200. REPLACED IAW DWG 9936534.

Source: SDR DALA2016040602838
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: CUSP WEB — CORRODED (BS 180-190) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON CUSP WEB, BS 180-190, RBL 46. REMOVED CORROSION. REPAIRED IAW SRM 53-00-01.

Source: SDR DALA2016040602837
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 160) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR SUPPORT, BS 160. REPLACED IAW DWG 9936534.

Source: SDR DALA2016040602840
OTHER · 2016-04-06 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 160) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON CABIL FLOORBEAM , BS 160, BETWEEN RBL 10-20. REPLACED SUPPORT IN NRC 367.

Source: SDR DALA2016040602842
OTHER · 2016-04-06 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON FLOOR SUPPORT, BS 180. REPLACED IAW DWG 9936534.

Source: SDR DALA2016040602839
OTHER · 2016-04-06 Matched by certificate designator
ATA 5340

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,140 hrs · 28,017 cycles

CORROSION ON R1 DOOR AFT GIRT BAR FITTING. R & R FITTING IAW SRM 51-00-01.

Source: SDR DALA2016040602720
OTHER · 2016-04-05 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 902) · airframe 49,140 hrs · 28,017 cycles

CRACK FOUND ON FORWARD SIDE OF FRAME TAB, VERIFIED WITH HFEC. REPAIRED FRAME, STA 902.

Source: SDR DALA2016040602718
OTHER · 2016-03-29 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CRACKED (TAIL CONE) · airframe 49,140 hrs · 28,017 cycles

TAIL INTERIOR CANTED BULKHEAD STA 1520, FORWARD AND AFT WEB IS CRACKED RT SIDE. REPAIRED IAW SRM 53-10-03, PARA 10A.

Source: SDR DALA2016033002635
OTHER · 2016-03-29 Matched by certificate designator
ATA 5710

Part: STRUCTURE — CRACKED (RT WING) · airframe 49,140 hrs · 28,017 cycles

RIGHT WING LOWER L/E CRACKED AT OTBD FWD CORNER OF FUELING BAY. REPAIRED IAW SRM 57-20-01.

Source: SDR DALA2016033002636
OTHER · 2016-03-25 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CRACKED (BS 1520) · airframe 49,140 hrs · 28,017 cycles

CANTED BULKHEAD, BS 1520, AFT WEB IS CRACKED LT SIDE. ACCESS INSIDE LT VENT BOX. REPAIRED BULKHEAD IAW SRM 51-10-03, FIG 9C.

Source: SDR DALA2016032602419
Earlier reports · 2012–2014 · 20 reports

2014

OTHER · 2014-10-28 Matched by certificate designator
ATA 5350

Part: LATCH — WORN (TAILCONE) · airframe 45,485 hrs · 25,753 cycles

LEFT UPPER TAILCONE LATCH WORN. R & R LATCH ASSEMBLY.

Source: SDR DALA2014102905827
OTHER · 2014-05-22 Matched by certificate designator
ATA 5311

Part: FRAME — CHAFED (BS 1437) · airframe 44,348 hrs · 25,031 cycles

FOUND CHAFING DAMAGE ON FRAME WEB AT BS 1437, L4L. COMPLIED WITH ERA 526153-14, REV O.

Source: SDR DALA14032699257
OTHER · 2014-05-21 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 1531) · airframe 44,348 hrs · 25,031 cycles

LEFT LOWER AFT FUSELAGE, BS 1531, SKIN CRACKED, AT RIVET ABOVE VENTRAL STAIR CUTOUT. REMOVED DAMAGE. COMPLETED REPAIR IAW SRM 53-00-01, FIG 6.

Source: SDR DALA14032689257
OTHER · 2014-05-21 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 1475) · airframe 44,348 hrs · 25,031 cycles

SKIN HAS A CRACK THROUGH 2 SIDE OF FASTENER HOLE, BS 1475, L2R. REPAIRED FUSELAGE AND INSTALLED DOUBLER IAW ERA 526106-14, REV O.

Source: SDR DALA14032679257

2012

F.O.D.; SMOKE/FUMES/ODORS/SPARKS · 2012-11-18 Matched by certificate designator
ATA 2530

Part: COFFEEMAKER — CONTAMINATED (GALLEY) · airframe 40,541 hrs · 22,754 cycles

FLIGHT CREW REPORTED A BURNING ODOR FROM COFFEEMAKERS BY THE L1 DOOR. COFFEEMAKERS TURNED OFF. ODOR DISSIPATED. MX FOUND PLASTIC CUP RESIDUE ON LOWER COFFEE DISPENSER HOT PLATE. CLEANED DEBRIS AND ALL RESIDUE. OPS CHECKS GOOD. ALL NORMAL.

Source: SDR DALA12014079257
OTHER · 2012-09-21 Matched by certificate designator
ATA 5260

Part: CABLE — WORN (AIR STAIR) · airframe 42,323 hrs · 23,778 cycles

VENTRAL STAIRWAY MOVEABLE CEILING CABLE AND SPRINGS WORN. R & R LEFT LIFT CABLE AND SPRING IAW MM. OPS CHECKED GOOD.

Source: SDR DALA13037239257
OTHER · 2012-04-23 Matched by certificate designator
ATA 5313

Part: LONGERON — CORRODED (BS 1259) · airframe 39,368 hrs · 22,042 cycles

AFT CARGO COMPARTMENT AREA, LONGERON 30 HAS EXFOLIATED CORROSION AT STA 1259 LT AND RT. REPAIRED PER ERA 502682-14 REV O.

Source: SDR DALA1235989257
OTHER · 2012-04-12 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 693) · airframe 39,368 hrs · 22,042 cycles

MID CARGO FLOORBEAM HAS CORROSION STA 693 L28R TO L28L. REPLACED PER SRM 51-30-05.

Source: SDR DALA1222869257
OTHER · 2012-04-12 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,368 hrs · 22,042 cycles

R1 DOOR CUT OUT LOWER CORNER EXTERNAL SKIN HAS EDGE CRACKED. REPAIRED PER ERA 501348-14 REV O.

Source: SDR DALA1235959257
OTHER · 2012-04-09 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 1307) · airframe 39,368 hrs · 22,042 cycles

CORROSION ON TOP OF FLOORBEAM STA 1307 LBL 4.5 AND LBL 9.5. FABRICATED FLOORBEAM PER DWG S2929169 AND INSTALLED PER SRM 51-30-05.

Source: SDR DALA1222849257
OTHER · 2012-04-08 Matched by certificate designator
ATA 5312

Part: DOUBLER — CORRODED (BULKHEAD) · airframe 39,368 hrs · 22,042 cycles

AFT PRESSURE DOME LOWER BL 0 TRIANGLE SHAPED DOUBLER CORRODED. REMOVED TEE ANGLE AND DOUBLER. DOUBLER CORRODED OUT OF LIMITS. INSTALLED NEW DOUBLER AND INSTALLED TEE ANGLE PER SRM 53-10-03 VOL I.

Source: SDR DALA1222019257
OTHER · 2012-04-07 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (BS 1156 LBL 22) · airframe 39,368 hrs · 22,042 cycles

SEAT TRACK GOUGED AND CORRODED STA 1156 LBL 22. REPLACE SEAT TRACK AND INSTALLED SPLICE REPAIR PER SRM 53-40-01.

Source: SDR DALA1222839257
OTHER · 2012-03-28 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — DAMAGED (BS 1231-1146) · airframe 39,368 hrs · 22,042 cycles

FOUND CABIN SEAT TRACK SCRATCHED LBL44.5 STA 1231 TO 1146. REPLACED TRACK PER SRM 53-40-01.

Source: SDR DALA1233709257
OTHER · 2012-03-28 Matched by certificate designator
ATA 5320

Part: CUSP WEB — CORRODED (BS 674-750) · airframe 39,368 hrs · 22,042 cycles

RT CUSP WEB FROM BS 674 TO 750 SEVERAL AREAS WITH SURFACE CORROSION. REMOVED CORROSION, OIL CANNING AND OUT OF LIMITS. REPAIRED AREAS PER SRM 53-20-02 VOL I AND 53-30-02 VOL II.

Source: SDR DALA1220319257
OTHER · 2012-03-28 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (BS 234) · airframe 39,368 hrs · 22,042 cycles

FOUND CORROSION ON SEAT TRACK RBL 44.5 BS 234. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-01 FIG 4 AND FIG 6.

Source: SDR DALA1235979257
OTHER · 2012-03-25 Matched by certificate designator
ATA 5320

Part: ANGLE — CRACKED (BS 1520.225) · airframe 39,368 hrs · 22,042 cycles

EMPENNAGE RT SIDE AT STRINGER 16 ON CANTED 1520.225 THERE IS A CRACK IN THE RADIUS. REMOVED ANGLE AND REPLACED PER MD90 SRM 51-30-05 VOL II, 51-30-02 VOL II, AND 51-20-00 VOL II.

Source: SDR DALA1235949257
OTHER · 2012-03-25 Matched by certificate designator
ATA 5743

Part: SUPPORT FITTING — UNKNOWN (RT MLG) · airframe 39,368 hrs · 22,042 cycles

INSPECTED RT MLG RETRACT ACTUATOR SUPPORT FITTING. REPLACED FITTING, BUSHING, AND BEARING.

Source: SDR DALA1233699257
OTHER · 2012-03-24 Matched by certificate designator
ATA 5313

Part: LONGERON — CORRODED (BS 758-769 L28R) · airframe 39,368 hrs · 22,042 cycles

MID CARGO HAS CORROSION SPOT ON 4EA. STRAPS LONGERON 28R AND 30 STA 758-769. FABRICATED STRAPS PER DWG 9936578 AND 5936071. INSTALLED PER MD 90 SRM 51-10-05 AND 51-30-05.

Source: SDR DALA1222829257
OTHER · 2012-03-23 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,368 hrs · 22,042 cycles

AFT CARGO COMPT BETWEEN STA 1212 AND 1269 FLOOR SUPPORT WITH CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER MD90 SRM 51-10-05 VOL. II.

Source: SDR DALA1235939257
OTHER · 2012-03-22 Matched by certificate designator
ATA 5313

Part: LONGERON — CORRODED (FUSELAGE) · airframe 39,368 hrs · 22,042 cycles

MIS CARGO COMPARTMENT DOOR JAMB BETWEEN STA 693-750 WITH HEAVY CORROSION. REMOVED AND REPLACED LONGERON 28R FROM STA 655 - 788 PER SRM 51-30-05 AND DRAWING 5930481.

Source: SDR DALA1235929257