N16647
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.
34 reports on file, 2002-06-09 – 2010-04-05.
Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 32,866 hrs · 17,262 cycles
DOUBLER FOUND ON RADIO ALTIMETER ANTENNA CUTOUT AT STA 410 WHILE ACCOMPLISHING EA- CONTACT ENGINEERING TO OBTAIN AMOC DISPOSITION FOR DOUBLER. PERFORMED ALL STEPS OF PART 1, STEPS 1-18 OF ECRA 5330-04011 REV A. ISSUED DIP TO ACCOMPLISH INSPECTIONS PER PART 2 AT A THRESHOLD OF 77,000 TOTAL FLIGHT CYCLES AND CONTACT ESC AFTER 72,500 TOTAL FLIGHT CYCLES BUT BEFORE 73,000 TOTAL FLIGHT CYCLES. //QC// ACCOMPLISH INSPECTIONS PER PART 2 AT A THRESHOLD OF 77,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ESC AFTER 72,500 TOTAL FLIGHT CYCLES BUT BEFORE 73,000 TOTAL FLIGHT CYCLES STA 400-420 S-27L TO S-28RT PER ECRA 5330-04011. DIP CTL NUMBER 04455.
Part: SKIN — CRACKED (FUSELAGE) · airframe 32,866 hrs · 17,262 cycles
SUPPORT TASK STA 303 L-1 DOOR LOWER HINGE CUTOUT FASTENER HOLE HAS CRACK INDICATION. BOTTOM FASTENER REMOVED PER EA 5330-03736. REPAIRED FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT PER EC/RA 5330-03999. GENERATED A DIP: 53-DIP CONTROL#04376 TO PERFORM AN INSPECTION PER PART 2 OF ECRA 5330-039999 PRIOR TO 72,262 TOTAL FLT CYCLES BEFORE THE ACCUMULATION OF 72,262 TOTAL A/C FLT CYC, PERFORM AN QC BEFORE THE ACCUMULATION OF 72,262 TOTAL AIRFRAME FLT INSPECTION PER PART 2 OF ECRA. PLANNING TO CONTACT ENGR AFTER CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5330-03999. ACCUMULATION OF 66,000 TOTAL FLT CYC BUT BEFORE 67,000 TOTAL PLANNING TO CONTACT ENGINEERING AFTER ACCUMULATION OF 66,000 FLT CYC FOR INSP DETAILS. TOTAL FLIGHT CYCLES BUT BEFORE 67,000 TOTAL FLIGHT CYCLES FOR INSPECTION DETAILS. NOTE BEING EVALU PER DTA 14CFR25.571 1) INIT: AFTER 66000 BUT BEFORE 67000 TOTAL A/C F/C & 2) T/A: W/I 72262 TOTAL A/C F/C.
Part: SKIN — DENTED (FUSELAGE) · airframe 32,866 hrs · 17,262 cycles
SUPPORT TASK DENT AT RT FUSELAGE AT 822.5 15 INCHES BELOW LOWER EDGE OF CARGO DOOR CUTOUT. PREVIOUSLY BLENDED OUT OF LIMITS. NDT SHOWS .050 MATERIAL REMAINS AT DENT/BLEND DMG L/P 5664181 INSTALLED INTERIM REPAIR DOUBLER & TRIPLER AND INITIATED DIP FLIGHT CYCLES FOR INSP DETAILS REF ECRA 5330-04012 004401 FOR SKIN REPAIR AT STA 822 S-26R ACCOMPLISH AN INSP OF REPAIR BEFORE THE ACCUM OF 77,262 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2 OF ECRA 5330-04012 CONTACT PLANNING ENGINEERING AFTER ACCUM OF 70,000 TOTAL FLIGHT CYCLES BUT BEFORE 72,000 TOTAL. QC FOR THE FUSELAGE SKIN REPAIR AT STA 822 S-26R ACCOMPLISH AN INSPECTION OF REPAIR BEFORE THE ACCUMULATION OF 77,262 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2 OF ECRA 5330-04012. PLANNING TO CONTACT ENGINEERING AFTER ACCUMULATION OF 70,000 TOTAL FLIGHT CYCLES BUT BEFORE 72,000 TOTAL FLIGHT CYCLES FOR INSP DETAILS.
Earlier reports · 2002–2008 · 31 reports
2008
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 28,850 hrs · 15,168 cycles
LEFT OUTBOARD AFT FLAP HAS A DELAMINATED AREA ON LOWER INBOARD SURFACE. REMOVED LEFT OUTBOARD AFT FLAP PER MM 27-51-39, REPAIRED PER SRM 51-70-10, REINSTALLED LEFT OUTBOARD AFT FLAP PER MM 27-51-39.
Part: SILL — CORRODED (FWD CARGO) · airframe 28,850 hrs · 15,168 cycles
FWD CARGO LOWER SILL PLATE HAS CORROSION ON TOP AND BOTTOM SIDES. INSTALLED NEW SILL PLATE IN FWD CARGO IAW B737 SRM51-40-02.
Part: FRAME — CORRODED (L2 DOOR) · airframe 28,850 hrs · 15,168 cycles
CORROSION ON L2 DOOR SUPPORT STRUCTURE JUST AFT OF LOWER AFT CORNER. FOUND CORROSION TO BE BEYOND LIMITS PER SRM 51-10-02. FABRICATED AND REPLACED FRAME SECTION AND REPAIRED SPLICE PER SRM 51-70-11 AT L2 DOOR SUPPORT STRUCTURE JUST AFT OF LOWER AFT CORNER.
Part: STIFFENER — DEFORMED (BS 1138) · airframe 28,850 hrs · 15,168 cycles
STIFFENER STATION 1138 DEFORMED. REMOVED OUT OF LIMITS STIFFENER AT STATION 1138, FABRICATED AND INSTALLED NEW STIFFENER AND SPLICE AT STATION 1138 PER DWG 65-54832 AND B-737-500 SRM 51-70-11.
Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 28,850 hrs · 15,168 cycles
NR 5 SLAT TRAILING EDGE WARPED AT OUTBOARD END AT PREVIOUS REPAIR. REPAIRED AT OUTBOARD END AT PREVIOUS REPAIR AND UPPER SURFACE REFINISHED PER SRM 51-70-10 AND CAL 5100500128 REV Q.
Part: FRAME — CRACKED (BS 360 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 360 FRAME CRACKED BETWEEN S-8 AND S-9 LT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED CRACKED FRAME AT BODY STATION 360 BETWEEN S-8 AND S-9 LEFT PER PACE EA647-53-001CAL AND EC/RA 5310-04812.
Part: ANGLE — CORRODED (BS 727B-787) · airframe 28,850 hrs · 15,168 cycles
AFT CARGO BAY RIGHT SIDE TRANSLATION ANGLE HAS CORROSION FROM STATION 727B TO 787. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF TRANSITION ANGLE FROM STATION 733-766 RIGHT SIDE PER SRM 53-60-53.
Part: ANGLE — CORRODED (L2 DOOR) · airframe 28,850 hrs · 15,168 cycles
AFT CABIN L2 DOOR Z-ANGLE HAS CORROSION. CORROSION ON L2 DOOR Z-ANGLE FOUND TO BE BEYOND LIMITATIONS PER SRM 53-60-15 FIGURE 1, REMOVED AND REPLACED Z-ANGLE PRE SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (BS 947-967) · airframe 28,850 hrs · 15,168 cycles
CORROSION FOUND ON STRAP BETWEEN STATION 967 AND 947 LBL 47. REMOVED CORROSION FOUND TO BE BEYOND LIMITS OF SRM 53-60-15. REMOVED AND REPLACED INTERCOSTAL LBL 47 BETWEEN STATION 967 AND 947 PER SRM 51-40-02.
Part: FRAME — CRACKED (BS 867 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 867 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STATION 867 LEFT BETWEEN S-8 AND S-9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 827 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 827 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BRACKET, CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STATION 827 LEFT BETWEEN S-8 AND S-9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 907 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 907 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) A/C BRACKET INBOARD HOLE. REMOVED A/C BRACKET, CUT OUT DAMAGED AREA & REPAIRED FRAME AT STATION 907 LEFT BETWEEN S-8 AND S-9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 787 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STA 787 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BRACKET CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STA 787 LT BETWEEN S-8 AND S-9 PER EA 5310-04498.
Part: SILL — CORRODED (R2 DOORWAY) · airframe 28,850 hrs · 15,168 cycles
R2 DOOR SILL WEB HAS CORROSION ON UPPER AND LOWER SURFACES. REMOVED R-2 DOOR SILL WEB IAW B737 SRM 51-40-02 MATL ID FOR NEW SIL WEB 7075 T6 .063 IAW B737 SRM 53-60-15. FABBED NEW WEB IAW BAC DWG 65-45855. ALODINED AND PRIMED IAW B737 SRM 51-20-01 INSTALLED WEB IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (BS 747 S8-9R) · airframe 28,850 hrs · 15,168 cycles
RIGHT SIDE STATION 747 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW EA5310-04498.
Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 28,850 hrs · 15,168 cycles
INTERCOSTAL CRACKED AT STA 344 TO 360 BL 11L. REMOVED CRACKED INTERCOSTAL AT STA 344 TO 360 BL 11L AND INSTALLED NEW INTERCOSTAL IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 440 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES AT LEFT SIDE FRAME STATION 440 BETWEEN S-8 AND S-9 PER EA5310-04498.
Part: STRINGER CLIP — CRACKED (BS 380 S8R) · airframe 28,850 hrs · 15,168 cycles
RIGHT SIDE STA 380 STRINGER 8 CLIP CRACKED. REMOVED DAMAGED STRINGER CLIP AT STA 380 RT S-8 RECEIVED NEW FROM STOCK LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-02.
Part: FRAME — CRACKED (BS 380 S8-9R) · airframe 28,850 hrs · 15,168 cycles
RIGHT SIDE STA 380 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BRACKET CUTOUT DAMAGED AREA AND REPAIRED FRAME AT STA 380 RT BETWEEN S-9 AND S-9 PER EA 5310-04498.
Part: FRAME — CRACKED (BS 747 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STA 747 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET. REMOVED A/C RAIL BRACKET CUTOUT DAMAGED AREA AND REPAIRED FRAME AT STA 747 LT BETWEEN S-8 AND S-9 PER EA 5310-04498.
Part: ANGLE — CORRODED (R2 DOOR) · airframe 28,850 hrs · 15,168 cycles
AFT CABIN R2 DOOR Z-ANGLE HAS CORROSION. REMOVED R2 DOOR Z-ANGLE IAW B737 SRM 51-40-02, INSTALLED NEW R2 DOOR Z-ANGLE IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 400 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES AT STATION 400 LEFT FRAME BETWEEN S-8 AND S-9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 787 S8-9R) · airframe 28,850 hrs · 15,168 cycles
RIGHT SIDE STATION 787 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED AIR CONDITIONING (A/C) RAIL BRACKET IAW EA5310-04498. CUT OUT DAMAGED AREA OF FRAME IAW EA 5310-04498. INSTALLED REPAIR ANGLES IAW EA 5310-04498.
Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 28,850 hrs · 15,168 cycles
INTERCOSTAL CRACKED AT STATION 312 TO 328 BL 45L. REMOVED AND REPLACED INTERCOSTAL IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (BS 482 S8-9L) · airframe 28,850 hrs · 15,168 cycles
LEFT SIDE STATION 482 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES AT STATION 482 LEFT FRAME BETWEEN S-8 AND S-9 PER EA5310-04498.
Part: FRAME — CRACKED (BS 400 S8-9R) · airframe 28,850 hrs · 15,168 cycles
RIGHT SIDE STA 400 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED FRAME AT STA 400 S-8 AND S-9 PER EA 5310-04498.
Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 28,850 hrs · 15,168 cycles
INTERCOSTAL CRACKED AT STA 328 TO 344 BL 45L. REMOVED CRACKED INTERCOSTAL AT STA 328 TO 344 BL 45L AND INSTALLED NEW INTERCOSTAL IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (BS 440 S8-9R) · airframe 28,850 hrs · 15,168 cycles
RIGHT SIDE STA 440 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED CRACKED FRAME AT STA 440 BETWEEN S-8 AND S-9 PER EA 5310-04498.
2003
Part: ANGLE — CORRODED (R-2 DOOR) · airframe 16,627 hrs · 8,799 cycles
INSPECTION FOUND UPPER SURFACE OF R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 16,627 hrs · 8,799 cycles
INSPECTION FOUND LOWER SURFACE OF LT HORIZONTAL STABILIZER SKIN DENTED APPROXIMATELY 8 INCHES FORWARD OF AFT SPAR AND 102 INCHES O/B OF FUSELAGE. A REPAIR WAS INSTALLED IAW SRM 55-10-01.
2002
Part: SKIN — DENTED (STA 907) · airframe 13,684 hrs · 7,166 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 907 BETWEEN S22R AND S23R. REPAIRED IAW SRM 53-00-01, FIGURE 224.