N11612

No registry detail on file · not in current registry

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.

33 reports on file, 2007-10-22 – 2012-04-13.

FALSE WARNING · 2012-04-13 Matched by certificate designator
ATA 3260

Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 45,561 hrs · 24,244 cycles

AFTER TAKEOFF LEFT MAIN GEAR RED LIGHT REMAINED ON. AFTER GEAR RETRACTION RED UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN BOTH UP AND OFF. FOUND LT MLG UPLOCK SENSOR AT FAULT. REF MM 32-61-00-101 R/R LT MLG UPLOCK SENSOR REF MM 32-61-21. CYCLED GEAR. ALL INDICATIONS NORMAL.

Source: SDR CALA2012041600264
FLUID LOSS; WARNING INDICATION · 2012-03-28 Matched by certificate designator
ATA 2910

Part: FLEX LINE — TORN (RT MLG WW) · airframe 45,448 hrs · 24,192 cycles

AFTER T/O B-SYS HYD WENT TO ZERO AND BOTH PRESSURE LOW LIGHT CAME ON. RAN QRH, RETURN TO EWR. FOUND FLEX LINE TORN. REMOVED AND REPLACED FLEX LINE REF L/P 4556125 LINE, OPS CK NORMAL. OK TO CONTINUE.

Source: SDR CALA2012032900216
Earlier reports · 2007–2011 · 31 reports

2011

NO TEST · 2011-04-30 Matched by certificate designator
ATA 3350

Part: FUSE — BLOWN (BATTERY PACK) · airframe 43,163 hrs · 22,984 cycles

FLT DECK EMERGENCY DOME LIGHT FAILED DURING TEST, L273. FOUND EMERGENCY BATT PWR PACK M1675 AT STA 318, F4 PICO FUSE BAD. REPLACED FUSE REF AMM 33-5151-910-817C1, OPS CHECK GOOD.

Source: SDR CALA2011050200328
OTHER · 2011-03-06 Matched by certificate designator
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

LT UPPER FUSELAGE SKIN DAMAGED AT APPROX STA 1121 BENEATH VERTICAL STAB ATTACH ANGLE. INSTALLED REPAIR DOUBLER REF EC/RA 5331-01553.

Source: SDR CALA2011030700126
OTHER · 2011-03-04 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

LARGE SHALLOW DENT RT SIDE OF FUSELAGE STARTING AT STA 362.5 AND EXTENDING TO STA 372.75 AND LOCATED BETWEEN S-18R AND S-19R. REPAIRED FUSELAGE PER ECRA 5331-01552 AND INITIATED DIP 09510 TO RE-INSPECT PER PART 2 OF ECRA 5331-01552 ON OR BEFORE THE ACCUMULATION OF 66000 TOTAL A/C FLT CYCLES. INTERIM REPAIR ACCOMPLISHED PER ECRA 5331-01552, PART 1. ON OR BEFORE THE ACCUMULATION OF 66,000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM A PERMANENT REPAIR PER PART 2 OF ECRA 5331-01552.

Source: SDR CALA2011030400117
OTHER · 2011-03-02 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

SUPPORT TASK: PER STEP 20.0 OF EA 5330-03736 REV B CRACK INDICATION VERIFIED IN HOLE MARKED NR 1 ON FIG 5 SHEET 2 OF WORKCARD. REPAIR ACCOMPLISHED PER ECRA 5330-04106. SEQ N959 FOR DIP INITIATED.

Source: SDR CALA2011030700122
OTHER · 2011-02-28 Matched by certificate designator
ATA 5230

Part: SKIN — DENTED (CARGO DOOR) · airframe 42,710 hrs · 22,751 cycles

SUPPORT TASK - DENT ON AFT CARGO DOOR EXTERNAL SKIN LOCATED 12 INCHES FROM FWD EDGE A/Y IS LESS THAN 30. INSTALLED REPAIR DOUBLER ON AFT CARGO EXTERNAL SKIN REF SRM 52-00-01 REPAIR 3.

Source: SDR CALA2011022800111
OTHER · 2011-02-24 Matched by certificate designator
ATA 5242

Part: SKIN — WORN (E&E DOOR) · airframe 42,710 hrs · 22,751 cycles

SUPPORT TASK E&E DOOR HAS LARGE BLEND OUT ON SKIN EDGE. REPAIRED E&E DOOR OUT SKIN REF SRM 52-00-01 PAGE 201 TO 204 (REPAIR NR 2).

Source: SDR CALA2011022400108
OTHER · 2011-02-18 Matched by certificate designator
ATA 5240

Part: PLATE — CRACKED (R1 DOOR) · airframe 42,710 hrs · 22,751 cycles

R1 DOOR-AFT LOWER CORNER STOP FITTING IS CRACKED THROUGH HI-LOK HOLE (MARKED) SEEN FROM INTERIOR P/N 65-51674-501. INSPECT STOP FITTING AND NO CRACK WAS FOUND. HOWEVER, REINFORCING PLATE ON BACK SIDE OF FITTING WAS CRACKED. REMOVED AND REPLACED REINFORCING PLATE REF SRM 51-40-02.

Source: SDR CALA2011021800099
OTHER · 2011-02-18 Matched by certificate designator
ATA 5344

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

SUPPORT TASK-L-1 DOOR FWD JAMB UPPER HINGE FITTING IS CRACKED. REMOVED & REPLACED L-1 FWD JAMB UPPER HINGE FITTING REF SRM 51-40-02.

Source: SDR CALA2011021800098
OTHER · 2011-02-17 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

SUPPORT TASK - LT SIDE MAIN FRAME CRACK STA 616 AT JUST BELOW MAIN DECK FLOOR ACCOMPLISHED FRAME REPAIR ON (SEE) EA 5310-05331 OP1 STEP 24.1 THRU STEP 24.14.

Source: SDR CALA2011021700096
OTHER · 2011-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

FRAME CRACKED STA 867 AT S-9R. INSTALLED REPAIR ANGLES A&B REF EA 5310-04498 REV A OP2.

Source: SDR CALA2011032400176
OTHER · 2011-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

FRAME CRACKED STA 907 AT S-9R CTN53-304-108 INSTALLED REPAIR ANGLES A&B PER EA.5310-04498, REV-A.

Source: SDR CALA2011032400177
OTHER · 2011-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

FRAME CRACKED STA 907 AT S-9L. CTN53-304-108 INSTALLED REPAIR ANGLES A&B REF EA 5310-04498 REV A.

Source: SDR CALA2011032400175
OTHER · 2011-02-09 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

SMALL AREAS OF LIGHT CORROSION (MARKED) ON FLOOR STRUCT. "Z" ANGLE AT R2 DOOR OPENING. REMOVED DAMAGE, FOUND OUT OF LIMITS SRM 53-60-15 FIG 101. REMOVED AND REPLACED "Z" ANGLE AT R2 DOOR SRM 51-40-02.

Source: SDR CALA2011020900077
OTHER · 2011-02-08 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

FRAME IS CRACKED AT O/H BIN RAIL STA 360 S-8L. INSTALLED REPAIR DOUBLERS IN REF ECRA 5310-05351.

Source: SDR CALA2011020800072
OTHER · 2011-02-08 Matched by certificate designator
ATA 5320

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

SUPPORT TASK - STA 482 AIR CONDITIONING SUPPORT BRACKET BTWN S-8 LT & S-9 LT I/B RIVET HOLE CRACKED. INSTALLED REPAIR ANGLES REF EA 5310-04498 REV A OP 02.

Source: SDR CALA2011020800071
OTHER · 2011-02-06 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,710 hrs · 22,751 cycles

FRAME IS CRACKED AT O/H BIN RAIL STA 400 S-8L. INSTALLED REPAIR DOUBLERS AT O/H BIN RAIL STA 400 STR 8L REF EA 5310-04498 REV A.

Source: SDR CALA2011020700066

2007

OTHER · 2007-10-31 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME BETWEEN STRINGER 8R AND 9R, STA 727-827. A DOUBLER AND STRAP WERE INSTALLED IAW ECRA 5310-04668, REV B.

Source: SDR CALA0700630
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 867 S8-9L) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A 5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 867 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700617
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 747 S8-9L) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 747 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700614
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 787 S8-9L) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700618
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 400 S8L) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700613
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 787 S8-9R) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK AT FORWARD FASTENER HOLE OF FRAME AT STA 787 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700615
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 827 S8-9L) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 827 BETWEEN STRINGERS 8L AND 9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700616
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 440 S8R) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A . 5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 440 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700620
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 400 S8R) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 400 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700612
OTHER · 2007-10-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 380 S8R) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT SIDE OF FUSELAGE FRAME AT STA 380 AROUND RIVET BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04668.

Source: SDR CALA0700619
OTHER · 2007-10-24 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CRACKED (BS 616) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE IN RT FUSELAGE INNER CHORD ABOVE WING CENTER SECTION STA 616, S17R. A STIFFENING ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.

Source: SDR CALA0700606
OTHER · 2007-10-24 Matched by certificate designator
ATA 5320

Part: FITTING — CRACKED (BS 349) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND A 1.5 INCH CRACK AT DOOR FITTING FASTENER IN L-1 DOOR OPENING AFT SIDE STRUCTURAL STRAP, STA 349, S16L. A REPAIR WAS INSTALLED IAW SRM 53-10-04.

Source: SDR CALA0700607
OTHER · 2007-10-22 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (BS 907-1006) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND AN L-2 DOOR Z-ANGLE CORRODED AT STA 907-1006, LBL 43 TO LBL 60. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-52878.

Source: SDR CALA0700601
OTHER · 2007-10-22 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 986) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 4. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51.

Source: SDR CALA0700599
OTHER · 2007-10-22 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 986) · airframe 37,035 hrs · 19,836 cycles

INSPECTION FOUND SURFACE CORROSION ON FLOORBEAM AT STA 986, RBL 40. A REPAIR STRAP WAS INSTALLED IAW SRM 53-60-51.

Source: SDR CALA0700598