N14653
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.
35 reports on file, 2003-08-13 – 2011-07-18.
Part: SKIN — CORRODED (BS 727C-747) · corrosion level 2
FOUND CORROSION IN AFT CARGO COMPT BILGE AREA INNER SKIN SURFACE APPROX BETWEEN BS 747 TO STA. 727C.
Part: SKIN — DAMAGED (BS 891 S23L)
LIGHTNING STRIKE ON LT FUSELAGE SKIN AT BS 891 AND .75" BELOW STR 23L.
Part: SKIN — DAMAGED (BS 773-927)
REPAIRED LIGHTNING STRIKES AT BS 773.5 TO BS 786.5 FROM S-28L TO S-28R, BS 798 TO BS 807 FROM 2.0" TO 2.75" ABOVE S-22L, BS 859.5 TO BS 937 1.5" BELOW S-21R TO 4.5" ABOVE S-21R, BS 861 4.0" ABOVE S-23L, BS 927 3.0" ABOVE S-24L AND BS 1016 BETWEEN S-23 AND S-24R BY INSTALLING SOLID RIVET PERMANENT REPAIRS IAW SRM 53-00-01 REPAIR 19, SECTION II.
Part: SKIN — DAMAGED (BS 203-482)
REPAIRED SKIN FROM BS 203 TO BS 243, FROM 8.0" TO 13.0" ABOVE STR. 24L, BS 311.75 TO BS 343.5 FROM 1.5" TO 3.0" ABOVE STR. 23L, BS 400 4.5" ABOVE STR. 22L, BS 416.5 TO BS 440 FROM ON STR. 21L TO 3.0" ABOVE STR. 21L AND BS 456 TO BS 482 FROM ON STR. 20L TO 2.24" ABOVE STR. 20L BY INSTALLING SOLID PERMANENT REPAIR FASTENER IAW SRM 53-00-01. REPAIR 19, SECTION II.
Earlier reports · 2003–2010 · 31 reports
2010
Part: SKIN — CRACKED (FUSELAGE) · airframe 32,522 hrs · 17,365 cycles
SUPPORT TASK - L-1 DOOR LOWER HINGE CUTOUT BOTTOM HOLE HAS CRACK INDICATION VERIFIED BY HFEC. TRIMMED OUT SKIN, INSTALLED A REPAIR DOUBLER REF ECRA5330-04033 & INITIATED A DIP (53-DIP CONTROL #05684) BEFORE THE ACCUMULATION OF 72,365 TOTAL FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA5330-04033. PLANNING CONTACT ENGINEERING AFTER 66,000 TOTAL FLIGHT CYCLES BUT BEFORE 67,000 FOR INSPECTION DETAILS. QC BEFORE THE ACCUMULATION OF 72,365 TOTAL A/C FLIGHT CYCLES, PERFORM INSPECTION PER PART 2 OF ECRA5330-04033. PLANNING CONTACT ENGINEERING AFTER ACCUMULATION OF 66,000 TOTAL FLIGHT CYCLES BUT BEFORE 67,000TOTAL FLIGHT CYCLES FOR INSPECTION DETAILS DIP#5684.
Part: STRUCTURE — UNKNOWN (FUSELAGE) · airframe 32,522 hrs · 17,365 cycles
SUPPORT TASK - REMOVE STA 178 LT SIDE CHORD AT LBL 28 FROM APPROX WL 230 TO WL 185 (REF EA 5310-04111 OP 1) SIDE CHORD. REMOVED AND REPLACED STA 178 LT SIDE CHORD AT LBL 28, FROM APPROX WL 230 TO WL185 REF PER EC/RA 5310-05224.
2009
Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 31,048 hrs · 16,613 cycles
LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. RETURNED TO EWR WITH AN UNDERWEIGHT LANDING. FOUND THE LATCH AND PRESS WARNING CIRCUIT BREAKER TO BE TRIPPED. RESET C/B. JACKED A/C SWUNG GEAR IAW AMM 32-32-00 SEVERAL TIMES COULD NOT DUPLICATE PROBLEM. A/C OK TO CONTINUE.
2008
Part: FRAME — CRACKED (BS 360) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 360 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED FRAME AT BODY STATION 360 BETWEEN S8L AND 9L AND REPLACED INTERCOSTAL CLIP AT BS 360 AND S8L PER EA5310-04498 AND EC/RA 5310-04830.
Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 28,313 hrs · 15,127 cycles
R2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE OUTSIDE AND LOWER INSIDE. FOUND FUSE'S BAD AT POWER SUPPLY, REPLACED FUSES IAW AMM33-51-51, OPS CHECK GOOD.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 28,313 hrs · 15,127 cycles
R-2 DOOR AFT FRAME WEB CORRODED OUT OF LIMITS PER SRM 51-10-02. FABRICATED PARTS PER BAC DRWG65C33583, REMOVED AND REPLACED FRAME SECTION IAW 51-10-02.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 28,313 hrs · 15,127 cycles
R2 DOOR AFT FRAME CORRODED AT STR 17R BETWEEN ATTACH CLIP AND FRAME. REPAIRED R2 DOOR AFT FRAME AT STR 17R BETWEEN ATTACH CLIP AND FRAME PER BOEING DWG 65-46566, B737 SRM 51-70-11 AND B737 SRM 51-40-02.
Part: FRAME — CRACKED (BS 400 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 400 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 400 RIGHT SIDE AT (AC) BRACKET BETWEEN STR 8 AND 9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 440 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 440 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT BODY STATION 440 RIGHT SIDE BETWEEN S-8R AND S-9R AT AC RAIL BRACKET PER EA5310-04498.
Part: FRAME — CRACKED (BS 380 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 380 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 380 RIGHT SIDE AT AC BRACKET BETWEEN STR 8 AND 9 PER EA 5310-04498.
Part: FRAME — CRACKED (BS 827 S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 827 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 827 LEFT AT AC BRACKET BETWEEN STR 8 AND 9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 400 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES PER EA 5310-04498 ON FRAME STATION 400 LEFT SIDE BETWEEN STR 8 LT AND STR 9 LT.
Part: FRAME — CRACKED (BS 747 S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 747 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME AT STATION 747 LEFT SIDE AT AC BRACKET BETWEEN STR 8 AND STR 9 PER EA 5310-04498.
Part: FRAME — CRACKED (BS 827 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 827 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 827 RIGHT AT AC BRACKET BETWEEN STR 8 AND 9 PER EA 5310-04498.
Part: FRAME — CRACKED (BS 867 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 867 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND STR 9. REPAIRED CRACKED FRAME AT STATION 867 RIGHT AT AC BRACKET BETWEEN STA 8 AND 9 PER EA 5310-04498 OP2.
Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 440 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES PER EA5310-04498 ON FRAME STA 440 LEFT SIDE BETWEEN STR 8 LT AND STR 9 LT.
Part: FRAME — CRACKED (BS 787 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 787 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REMOVED CRACK AND INSTALLED REPAIR ANGLES PER EA 5310-04498.
Part: FRAME — CRACKED (BS 727B S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 727B LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME AT STATION 727B AT A/C BRACKET BETWEEN STR 8 AND S9 LEFT PER EA 5310-04498.
Part: FRAME — CRACKED (BS 907 S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 907 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME AT STATION 907 LEFT AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN S8 AND S9 PER EA 5310-04498.
Part: FRAME — CRACKED (BS 787 S8-9L) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 787 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME AT STATION 787 LEFT SIDE AT AC BRACKET BETWEEN STR 8 AND 9 PER EA 5310-04498.
Part: FRAME — CRACKED (BS 907 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 907 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 907 RIGHT AT AC RAIL BRACKET BETWEEN STR 8 AND 9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 747 S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 747 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REMOVED CRACK AND INSTALLED REPAIR ANGLES PER EA5310-04498.
Part: FRAME — CRACKED (BS 727B S8-9R) · airframe 28,313 hrs · 15,127 cycles
BODY STATION 727B RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8R AND S9R. REPAIRED CRACKED FRAME AT RIGHT SIDE BODY STATION 727B BETWEEN S8R AND S9R PER EA 5310-04498.
Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 28,313 hrs · 15,127 cycles
HORIZONTAL STABILIZER CENTER SECTION TRUSS STRUCTURE HAS A CRACKED BRACKET AT APROXIMATELY STATION 1121 LT SIDE CENTER P/N 65C25156-8. REMOVED AND REPLACED CRACKED FITTING ON HORIZONTAL STABILIZER CENTER SECTION TRUSS AT APPROXIMATELY STATION 1121 LT SIDE CENTER IAW B737 SRM 51-40-02.
Part: STRINGER CLIP — CRACKED (BS 400 S16R) · airframe 28,313 hrs · 15,127 cycles
STATION 400 S16R TIE CLIP CRACKED. REMOVED AND REPLACED TIE CLIP AT STA 400 S16R REF SRM 51-40-02.
Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 28,313 hrs · 15,127 cycles
STATION 482 S16R TIE-CLIP CRACKED. REMOVED AND REPLACED TIE CLIP AT STATION 482 S16R REF SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (BS 380) · airframe 28,313 hrs · 15,127 cycles
STATION 380 + 7 INCHES LBL 25 INTERCOSTAL DENTED AT FASTENER ON VERTICAL LEG. REMOVED CRACKED PORTION ON WEB, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 51-70-13.
Part: INTERCOSTAL — CRACKED (BS 947-927) · airframe 28,313 hrs · 15,127 cycles
INTERCOSTAL BETWEEN FS 947-927 AT RBL 24 HAS POSSIBLE CRACK. REMOVED DAMAGED INTERCOSTAL CAP ANGLE IAW SRM 51-40-02. PER SRM 51-20-01 AND EC/RA 5310-03585 MATERIAL ID EXTRUSION BAC1505-101353 FOR CAP ANGLE, PAC 40859, .190 INCH, 7075-76, IC 0654053 FOR FILLER, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED REPAIR PARTS.
2006
Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 22,020 hrs · 11,740 cycles
A/C UNABLE TO MAINTAIN CABIN PRESSURE AT FL 250, EMERGENCY DESCENT. PERFORMED PRESSURIZATION TESTS, OPS CHECK NORMAL.
2003
Part: CHANNEL — CRACKED (LT PYLON) · airframe 16,056 hrs · 8,661 cycles
INSPECTION FOUND A 1INCH CRACK IN LT PYLON RT SIDE VERTICAL CHANNEL THAT FORWARD END PANEL NR 5843R AND AFT END OF PANEL NR 5842R ATTACHES TO. A NEW SPLICE PLATE WAS INSTALLED IAW SRM 51-40-02.
Part: IMPELLER — BROKEN (APU)
BROKEN BLADE FROM SECOND STAGE IMPELLER THAT POSSIBLY EXITED TURBINE PLENUM.