N16650
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.
23 reports on file, 1999-12-09 – 2008-10-27.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 28,610 hrs · 15,160 cycles
LEFT WING NUMBER 2 SLAT INBOARD AND OUTBOARD WEDGE SEALANT DAMAGED, NEED TO CHECK FOR DELAMINATION. REMOVED AND REPLACED DELAMINTED SKIN AND CORE ON LEFT WING NUMBER 2 SLAT PER SRM 51-70-10 AND APPLIED PROTECTIVE FINISH PER CAL ECRA 5100 500128 REV Q.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 787L FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT BODY STATION 787L BETWEEN S-8 AND S-9. FABRICATED REPAIR PARTS AND INSTALLED PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 907R FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 907 RIGHT FRAME AT S8R AND S9R PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 827L FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT BODY STATION 827L BETWEEN S-8 AND S9. FABRICATED REPAIR PARTS AND INSTALLED PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 482 RT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT STATION 482 BETWEEN S8R AND S9R, REPAIRED SAME IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 440 RT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S8 AND S9. CUT OUT DAMAGE ON FRAME AT STATION 440 BETWEEN S8R AND S9R REPAIRED SAME IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 787R FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 787 RIGHT FRAME AT S8R AND S9R PER EA 5310-04498.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
INTERCOSTAL CRACKED AT ATTACH POINT TO CABIN FLOORBEAM STATION 540, LBL 3. REMOVED AND REPLACED INTERCOSTAL IAW B737 SRM 51-40-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 360 LT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED FRAME AT BODY STATION 360L BETWEEN S-8 AND S-9 IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 867 RIGHT FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 867 RIGHT FRAME AT S8 AND S9 PER EA 5310-04498.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
INTERCOSTAL BETWEEN STATIONS 344 TO 360 BL 0 CRACKED AROUND FASTENER HOLES. REPAIRED DAMAGE TO INTERCOSTAL BETWEEN STATION 344 TO 360, BL 0 PER B-737-500 SRM 51-70-11 AND 51-10-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 400L FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S8 AND S9. REPAIRED FRAME AT BODY STATION 400L BETWEEN S-8 AND S-9 IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 747 RT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 747 RIGHT FRAME AT S8 AND S9 PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 867 LT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT BODY STATION 867L BETWEEN S8 AND S9. FABRICATED REPAIR PARTS AND INSTALLED PER EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 827R FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION FRAME 827 RIGHT AT S8R AND S9R PER EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 440 LT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRD FRAME AT BODY STATION 440 LT SIDE AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 IAW EA 5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
BODY STATION 400R FRAME CRACKED AT AIR CONDITION (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT STATION 400 BETWEEN STR 8R AND 9R, REPAIRED SAME IAW EA 5310-04498.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,610 hrs · 15,160 cycles
INTERCOSTAL BETWEEN STATION 344 TO STATION 360 LBL 10 CRACKED AROUND FASTENER HOLES. REMOVED AND REPLACED ANGLE AT STA 344 TO STA 360 LBL 10 PER B737 SRM 51-40-02 AND 53-10-51.
Part: CABIN PRESSURE — MALFUNCTIONED · airframe 27,721 hrs · 14,692 cycles
AT FL70 CABIN ALT WARNING HORN SOUNDED, CHECKED CABIN ALT GOING ABOVE 10,000. DID AN EMERGENCY DESCENT AND RAN CHECKLIST WAS NOT ABLE TO CONTROL CABIN IN MANUAL UNTIL BELOW 10,000 T/S PER AMM 21-31-25 FAULT CODE 030. PERFORMED HEALTH CHECK REF AMM 21-30-00/601, TEST PASSED. REMOVED AND REPLACED O/H CONTROL MODULE PRECAUTIONARY PER AMM 21-31-25, CHECK OK. BITE & PRESS CHECKED AGAIN PRECAUTIONARY CHECK OK. PANEL, PRESS, C OFF 24-2131-9-0001 2845 ON 24-2131-9-0001 2019.
Earlier reports · 1999–2004 · 4 reports
2004
Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 16,645 hrs · 8,932 cycles
THE A-HYDRAULIC SYSTEM QUANTITY AND PRESSURE BEGAN TO DROP WHILE CLIMBING THROUGH 24,000 FEET EN ROUTE FROM MDW TO EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-HYDRAULIC SYSTEM WARNING LIGHT. A MANUAL GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED PER OP NR 1 OF EA 2910-01325, REV D. OPERATIONAL AND LEAK CHECKS WERE GOOD.
2003
Part: BELTFRAME — PUNCTURED (FUSELAGE) · airframe 16,498 hrs · 8,847 cycles
INSPECTION FOUND LT BELT FRAME PUNCTURED IN TWO PLACES AT STA 847. THE DAMAGE WAS ROUTED OUT AND A BELT FRAME REPAIR WAS INSTALLED IAW SRM 51-70-11.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,498 hrs · 8,847 cycles
INSPECTION FOUND L-2 DOORWAY Z-ANGLE CORRODED AT STA 967. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
1999
Part: SKIN — PUNCTURED (HORIZONTAL STAB)
INSPECTION FOUND A PUNCTURE IN LT I/B HORIZONTAL STABILIZER LEADING EDGE AT STA 70. A FLUSH DOUBLER REPAIR WAS INSTALLED IAW SRM 55-10-01.