N242DL
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.
12 reports on file, 2001-01-29 – 2006-08-26.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 44,769 hrs · 25,654 cycles
STRINGER 19 LT AT BS 967 HAS TWO REPAIRS NOT PER THE SRM. REPLACED SECTION OF STRINGER PER SRM 53-00-03 FIG 201, REPAIR 1 AND 51-40-2.
Part: SKIN — DENTED (FUSELAGE) · airframe 44,769 hrs · 25,654 cycles
FUSELAGE SKIN DENTED FROM BS 867 TO BS 947 BETWEEN STR 21 RT AND 22 RT. REPAIRED PER EA 53-220.
Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 44,769 hrs · 25,654 cycles
DOUBLER UNDER THE L-2 DOOR AT BS 975 HAS NO DOCUMENTATION. REPLACED EXISTING DOUBLER PER EA 53-221.
Part: SKIN — CRACKED (L/E SLAT) · airframe 44,769 hrs · 25,654 cycles
NUMBER THREE SLAT LOWER SKIN IS CRACKED AT THE ACTUATOR. REPAIRED PER SRM 57-43-01.
Part: FITTING — ELONGATED (MLG) · airframe 44,769 hrs · 25,654 cycles
DURING REPLACEMENT OF THE AFT OB SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IAW SB 737-1216R2, PART III, NOTED SEVERAL ATTACHMENT HOLES IN THE REPLACEMENT FITTING OUT OF ROUND. REPAIRED DAMAGE AREA IN FITTING IAW MESSAGE NUMBER 1-213752921-12 DATED 26 JUL 2006 AND FAA FORM 8100-9 DATED 7 AUG 2006 WHICH IS AN AMOC TO AD 2005-18-08.
Part: SPAR — DAMAGED (WING) · airframe 44,769 hrs · 25,654 cycles
DURING REPLACEMENT OF THE AFT OB SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IAW SB 737-1216R2 PART III, NOTED SEVERAL ATTACHMENT HOLES IN SPAR CHORD AND WEB TO BE OUT OF ROUND. REPAIRED DAMAGE IAW MFG MESSAGE NR 1-21375291-12 DATED 26 JULY 2006 AND FAA FORM 8100-9 DATED 7 AUG 2006 AS AN AMOC TO AD 2005-18-08.
Part: SKIN — CRACKED (FUSELAGE) · airframe 43,743 hrs · 24,223 cycles
MAJOR REPAIR INSTALLED. INSTALLED DOUBLER BETWEEN STR 28L & 28R STA 380 IAW SRM 53-30-01D.
Part: RELAY — FAILED (COCKPIT) · airframe 41,059 hrs · 20,422 cycles
ABORTED TAKEOFF AT 90 KTS. WHEN APPROX. 40 LIGHTS ANUNNICATED ON OVERHEAD PANEL AND CONSOLE. FOUND ALL LIGHTS ILLUMINATED COMMON TO MASTER CAUTION SECT. A. RECYCLED MASTER TEST SW. LIGHTS EXTINGUISH.REPLACED MASTER TEST RELAY R33. ALL MASTER DIM AND TEST FUNCTIONS CHK GOOD PER AMM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 38,879 hrs · 18,126 cycles
A CRACK INDICATION WAS NOTED AT AN EXISTING GOUGE TRIMOUT LOCATION AT THE FWD EDGE OF THE C1 DOOR CUTOUT ABOVE THE LOWER CORNER.
Part: PROXIMITY SENSOR — LOOSE (NLG) · airframe 38,621 hrs · 17,872 cycles
ON APPROACH WHEN LDG GEAR SELECTED DOWN. NOSE GEAR RED UNSAFE INDICATION ON FWD PNL. EXTENDED NOSE GEAR MANUALLY PER POM WITH NO CHANGE ON FWD PNL. THEN NOTICED GEAR GREEN INDICATION ON OVERHEAD PNL. NOSE GEAR VISUALLY INSPECTED DOWN AFTER TOUCH DOWN NOSE GEAR INDICATED GREEN. FOUND PROX SW S 846 PRIMARY NOSE DOWNLOCK SENSOR LOOSE AND GAP OUT OF LIMITS. ADJ AND SECURED NOSE DOWNLOCK SENSOR PER M/M.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 38,092 hrs · 17,318 cycles
THE BEAR STRAP AT THE LOWER AFT CORNER OF THE R1 DOOR WAS FOUND WITH A 1 INCH CRACK. THE DAMAGE WAS TRIMMED OUT AND A REPAIR WAS INSTALLED PER SRM 53-10-01, FIGURE 202. THE REPAIR WAS ACCOMPLISHED AT MV.
Part: UNKNOWN — ODOR (CABIN) · airframe 38,028 hrs · 17,256 cycles
AFTER PUSHBACK BOTH ENGINES RUNNING, TWO F/A NOTICED ELECTRICAL ODOR AFT OF EMERGENCY EXITS, FWD OF AFT GALLEY. F/O CONFIRMS ELECTRICAL ODOR AROUND ROW 24 THE STRONGEST ODOR SEEMS TO DISSIPATE AFTER 3 - 4 MINUTES. RAN BOTH ENGINES, NTF.