N942DN
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.
25 reports on file, 2012-12-22 – 2018-12-31.
Part: FASTENER — MISSING (RT WING) · airframe 45,432 hrs · 36,651 cycles
ON WALK AROUND FOUND RT WING APPROX 4 FEET FROM WING TIP FASTENER MISSING AND SEVERAL LOOSE. REMOVED RT WING O/B T/E FIXED WEDGE AND WING TIP PER AMM 57-20 FOR MTC ACCESS. COMPLIED WITH PRI 574177-14 REV 3. REINSTALLED RT WING O/B T/E FIXED WEDGE AND WING TIP PER AMM 57-20. REPAIRED ON LOG 0885769. (LP# 5282426)
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,954 hrs · 36,355 cycles
CORROSION ON LOWER DOOR JAMB BEAM , EXTERNAL AND INTERNNAL SURFACES , IN CTR CARGO COMPARTMENT. CORROSION LOWER DOOR JAMB BEAM, EXTERNAL AND INTERNNAL SURFACES, IN CTR CARGO COMPARTMENT (UT) WAS ACOMPLISHED PER SPM NDT 04-00-07 PAR. 5 FIG 3SHEET 1 AND 2 NOMINAL THICKNESS ON DAMAGE AREA IS 0.210" AND REMAINING THICKNESS IS 0.148" THEREFORE IT?S OUT OF LIMITS PER SRM 53-60-02 VOL I FIG. 9 EQUIPMENT : DIGITAL ULTRASONIC 38DLP S/N 151215011 DATE 09/NOV/18 TRANSDUCER S/N 1087463 DATE 22/FEB/19 LEVEL CORROSION 2. LOWER DOOR JAMB WAS REPAIRED PER SRM 53-60-02 VOL.1 FIG. 9. (LP 0791869)
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,954 hrs · 36,355 cycles
CORROSION ON LOWER DOOR JAMB BEAM , EXTERNAL AND INTERNNAL SURFACES , IN AFT CARGO COMPARTMENT. CORROSION LOWER DOOR JAMB BEAM, EXTERNAL AND INTERNNAL SURFACES, IN AFT CARGO COMPARTMENT (UT) WAS ACOMPLISHED PER SPM NDT 04-00-07 PAR. 5 FIG 3SHEET 1 AND 2 NOMINAL THICKNESS ON DAMAGE AREA IS 0.280" AND REMAINING THICKNESS IS 0.198" THEREFORE IT?S OUT OF LIMITS PER SRM 53-60-02 VOL I FIG. 9 EQUIPMENT : DIGITAL ULTRASONIC 38DLP S/N 151215011 DATE 09/NOV/18 TRANSDUCER S/N 1087463 DATE 22/FEB/19 LEVEL CORROSION 2. LOWER DOOR JAMB WAS REPAIRED PER SRM 53-60-02 VOL.1 FIG. 9 EXTENDED TASK CARD FIELDS. (LP 0791873)
Part: WINDOW — FAILED (16A) · airframe 44,716 hrs · 36,201 cycles
WINDOW AT 16A CRACKED IN FLIGHT, APPEARS TO BE OUTER PANE THAT DELAMINATED. OUTER PART OF WINDOW SEPARATED FROM AIRCRAFT IN FLIGHT. PERFORMED INSPECTION ON LT ENGINE WITH NO DEFECTS IAW AMM 05-51-19. REMOVED AND REPLACED PASSENGER COMPARTMENT WINDOW ASSY IAW AMM 56-20-00-020-801.
Part: CABLE — DAMAGED (TAILCONE RELEASE) · airframe 43,532 hrs · 35,520 cycles
TAILCONE EMERGENCY RELEASE LOCK CABLE FORWARD OF TEE PIN FAILED TO RELEASE FROM SUPPORT FITTING, WHEN THE TEE PIN CAME OUT. REPLACED THE CABLE IAW AMM 20-52.
Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 43,532 hrs · 35,520 cycles
TAILCONE EMERGENCY RELEASE LOCK CABLE FOR SUPPORT FITTING FRAYED AT CABLE BALL END. REPLACED THE CABLE IAW AMM 20-52.
Part: CABLE — DAMAGED (TAILCONE RELEASE) · airframe 43,532 hrs · 35,520 cycles
AFT ENTRY DOOR EMERGENCY TAILCONE RELEASE FAILED. DOOR ROD FAILED TO RELEASE CABLE QUADRANT AT DOOR UPPER FRAME. PULL TEST EXCEEDED LIMIT OF 15LBS. ACTUAL PULL TEST 40LBS TO BY PASS DOOR IN. LUBED CABLE ND REPLACED CABLE IAW AMM 20-52. OPS NORMAL WITHIN LIMITS.
Earlier reports · 2012–2017 · 18 reports
2017
Part: LINE — LEAKING (WATER SYSTEM) · airframe 42,554 hrs · 34,910 cycles
EXPERIENCED SMOKE AND FUMES IN THE AC CABIN AFTER PUSHBACK. FLIGHT CREW HAD TUG DRIVER RETURN AC TO JETWAY AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND A CRACKED WATER LINE ABOVE THE WATER HEATER LOCATED IN THE F/CLASS LAV. THE WATER LINE WAS DRIPPING ON TO A HOT WATER HEATER CAUSING STEAM. THE HOT WATER HEATER WAS REPLACED PRECAUTIONARY AND THE WATER LINE WAS REPLACED.
2016
Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 39,874 hrs · 33,358 cycles
DURING TAKEOFF AND LANDING, CREW REPORTED A STRONG ODOR OF BURNING RUBBER IN COCKPIT AND FORWARD CABIN. ODOR DISSIPATES RAPIDLY. TROUBLESHOT. NO TROUBLE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.
Part: FRAME — CRACKED · airframe 39,771 hrs · 33,292 cycles
NOSE LANDING GEAR CUTOUT LEFT FRAME CRACKED AT GUIDE FORWARD UPPER FASTENER ATTACH HOLE. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-90-01.
Part: WEB — CRACKED · airframe 39,771 hrs · 33,292 cycles
FORWARD WET AREA UNDER G7 GALLEY, WEB CRACKED BOTTOM SIDE AT FASTENER. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-20-02.
Part: VALVE — CRACKED (HYD SYSTEM) · airframe 38,821 hrs · 32,753 cycles
IN FLIGHT, HYDRAULIC QTY DROPPED TO 4. CREW RAN QRH PROCEDURE AND SHUT OWN RT HYDRAULIC SYSTEM. DURING DESCENT, IAW THE QRH, ATTEMPTED TO RE-PRESSURIZED THE RT SYSTEM. THE RT SYS INDICATED 3000 PSI BUT QTY DROPPED TO 0. MAINTENANCE FOUND THE LT WING OTBD ANTISKID VALVE HOUSING CRACKED. R & R VALVE. LEAK AND OPERATION CHECKS GOOD IAW MM. CLEANED AFT BELLY AND MAIN GEAR WELL, APU INLET WAS DRY AND NEITHER PACK HAD SMELL.
Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 38,549 hrs · 32,592 cycles
L1 DOOR DAMAGED. REPAIRED EDGE FLANGE IAW SRM 52-01-01.
2014
Part: STRUCTURE — CRACKED · airframe 34,544 hrs · 30,088 cycles
FOUND CRACK INDICATION ON FIRST FASTENER HOLE ABOVE ZFS=52.267-M. REAMED HOLE TO FINAL SIZE OF .231" IAW DWG SG09550005. INSTALLED BUSHING, FABRICATED STRAP AND INSTALLED REPAIR STRAP IAW DWG SG09550005-7003.
Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 34,544 hrs · 30,088 cycles
FORWARD RT INNER VERTICAL STABILIZER ATTACH ANGLE HAS A FOUR INCH CRACK. R & R INNER SKATE ANGLE IAW DWG 5912188.
Part: SKIN — CRACKED (BS 1475) · airframe 34,544 hrs · 30,088 cycles
SKIN CRACKED AT BS 1475, LONGERON 2R. UNDER INTERNAL SKATE ANGLE. REPAIRED SKIN CRACK IAW DWG SG 90530003.
2013
Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 32,348 hrs · 28,746 cycles
LIGHTNING STRIKE ON FASTENER AFT CORNER OF MID CARGO DOOR. REPAIRED IAW ERA 521840-14, SECTION I, REV O. REF LP 1243580, DTA.
Part: SKIN — CORRODED (BS 1172 S27-28R) · airframe 30,006 hrs · 27,299 cycles
CORROSION FOUND BS 1172 RT AFT FUSELAGE TWO INCHES ABOVE RBL 28, BETWEEN LONGERON 27-28. REMOVED CORROSION CUT-OUT DAMAGE AREA FABRICATED, LOCATED, TREATED, PRIMED AND INSTALLED REPAIRED PARTS IAW SRM 53-30-01, FIG 9 AND SRM 51-10-03, FIG 3 AT STA 1172 RT AFT FUSELAGE 2" ABOVE RBL 28.
Part: SKIN — CORRODED (BS 1145) · airframe 30,006 hrs · 27,299 cycles
DURING HMV, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1145.5 AND L29R. DAMAGE WAS REPAIRED IAW ER/A 504831-14, SECTION I. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER REPAIR AND TAPERED SHIM. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAQ ER/A 504831-04MA, REV O. SECT I. TIME CONTROLLED ITEM IAW SECTION II.
Part: SPAR CAP — CORRODED (RT WING) · airframe 30,006 hrs · 27,299 cycles
WHILE IN SERVICE, CORROSION WAS FOUND ON THE RT WING FRONT SPAR LOWER CAP HORIZONTAL FLANGE AT XRS=531.700. THE REPAIR WAS ACCOMPLISHED IAW ER/A 510556-14, SECTION I.
Part: LONGERON — CRACKED (BS 1458-1475) · airframe 30,006 hrs · 27,299 cycles
WHILE IN SERVICE, A CRACK WAS FOUND ON FUSELAGE LONGERON 2R BETWEEN BS 1458-1475. ACCOMPLISHED A SPLICE REPAIR AND INSTALLED A 0.160" THICK STRAP. INSTALLED REPAIR IAW PROCESS STANDARD 900-5-1 NR 04. COMPLIED WITH ER/A 510485-14, REV "O".
Part: SKIN — CORRODED (LT WING) · airframe 30,006 hrs · 27,299 cycles
WHILE IN SERVICE, CORROSION WAS FOUND ON THE EXTERNAL SURFACE OF THE LT LOWER WING SKIN PANEL OTBD OF XRS=545.380 AT THE T/E. REPAIR WAS ACCOMPLISHED IAW ER/A 510483-14 SECTION I.
Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · airframe 30,006 hrs · 27,299 cycles
CORROSION REPAIR ON RT HORIZONTAL STABILIZER UPPER FRONT SPAR CAP AND LT HORIZONTAL STABILIZER LOWER FRONT SPAR CAP BARREL NUT FORWARD AND AFT HOLES IAW ER/A 510432-14, ACCOMPLISH SECTION I AT THE PRIOR TO SERVICE VISIT. ASSOCIATED ER/A 14-510432 ADDED FOR ACFT.
2012
Part: SEAT TRACK — GOUGED (BS 436) · airframe 30,006 hrs · 27,299 cycles
SEAT TRACK, RBL 22, BS 436 GOUGED. CUT OUT DAMAGED AREA. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-40-01, FIG 6, VOL I. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-40-01, FIG 6, VOL I.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 30,006 hrs · 27,299 cycles
DURING SERVICE CHECK, MX FOUND L1 DOOR AFT INTERNAL UPPER DOOR FRAME CRACKED. REMOVED OLD BEAM. FABRICATED AND INSTALLED NEW BEAM IAQ SRM 51-30-01.