N763CA

CIRRUS DESIGN CORP SR20 · 2014 · Fixed-wing single-engine · 1 engine · 4 seats · Valid Registration

Registered owner: HA AVIATION LLC, SC (owner ≠ operator)

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.

98 reports on file, 2002-01-17 – 2012-09-18.

OTHER · 2012-09-18 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE EXTERIOR BS 1620 - 1640, BETWEEN S23-24R, TWO EACH DENTS FOUND IN SKIN.

Source: SDR U2RA2012092148603
OTHER · 2012-09-18 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE EXTERIOR SKIN BETWEEN BS 1580 AND 1600 AND BETWEEN S25-26R DENTED.

Source: SDR U2RA2012092148602
OTHER · 2012-09-18 Matched by certificate designator
ATA 5313

Part: STRINGER SPLICE — CRACKED (BS 1620 S23R) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT AT BS 1620 STRINGER SPLICE 23R WAS FOUND CRACKED.

Source: SDR U2RA2012092148601
OTHER · 2012-07-23 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE SKIN AT BS 450, BETWEEN S25-26R HAS DENT FOUND TO BE OUT OF SRM LIMITS.

Source: SDR U2RA2012072348602
INADEQUATE Q C · 2012-07-23 Matched by certificate designator
ATA 5330

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

SKIN MISREPAIRED AT BS 490, BETWEEN S22-23R.

Source: SDR U2RA2012072348603
OTHER · 2012-07-23 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

CORROSION FOUND AROUND FASTENER HOLES ABOVE AND BELOW ANGLE ON THE LT EMERGENCY EXIT SILL PLATE AT BS 1320 - 1360.

Source: SDR U2RA2012072348601
OTHER · 2012-06-28 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS1600, BETWEEN LBL24 AND RBL24. REPAIRED IAW EA PD57-53-170.

Source: SDR U2RA2012072448601
OTHER · 2012-06-14 Matched by certificate designator
ATA 7120

Part: FITTING — GALLED (ZONE 400) · airframe 53,893 hrs · 23,065 cycles

NR 1 ENGINE 1/B SIDE LOAD FITTING TWO FASTENER HOLES GALLING AND ELONGATED.

Source: SDR U2RA201206148602
OTHER · 2012-06-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FORWARD CARGO FLOOR SUPPORT WEB CRACKED UPPER AFT SECTIONS BS 657 AT LBL 7.55

Source: SDR U2RA201206148601
OTHER · 2012-04-13 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 625) · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN AREA, 3 EA CRACKS FOUND IN STRINGER S7L AT BS 625, EACH CRACK IS 0.125" LONG.

Source: SDR U2RA2012041648601
OTHER · 2012-04-13 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN AREA, CRACK FOUND IN STRINGER S10L AT BS 625 EXTENDING FROM RIVET HOLE. CRACK LENGTH IS 0.125" LONG.

Source: SDR U2RA2012041648602
OTHER · 2012-04-05 Matched by certificate designator
ATA 5313

Part: STRINGER — CRACKED (BS 1701) · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN AT BS 1701, STRINGER 11R WAS FOUND TO BE CRACKED. CRACK LENGTH 1".

Source: SDR U2RA2012040548601
OTHER · 2012-03-23 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

INTERCOSTAL IN MAIN PASSENGER CABIN WAS FOUND TO BE CRACKED AT AFT LOWER END AT BS 1600 RBL 24. CRACK LENGTH IS 1.5" LONG.

Source: SDR U2RA2012032348601
OTHER · 2012-03-23 Matched by certificate designator
ATA 5313

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN AT BS 1701, STRINGER 16R FOUND TO BE CRACKED. CRACK LENGTH IS APPROX 1.5" LONG.

Source: SDR U2RA2012032348602
OTHER · 2012-03-13 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 1325) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOORBEAM ZEE CHANNELS ARE CORRODED UNDER NUTPLATES AT BS 1325, BTW RBL 10 & LBL 15.

Source: SDR U2RA2012032148601
OTHER · 2012-02-15 Matched by certificate designator
ATA 5320

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN, CORROSION FOUND ON THE CUSP WEB BETWEEN BS 1620 TO 1640 AT RBL 54.

Source: SDR U2RA2012021648601
OTHER · 2012-02-15 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

E & E COMPARTMENT INTERCOSTAL CRACKED AT AFT END, BS 440 - 410 AT S23L.

Source: SDR U2RA2012021648602
OTHER · 2012-01-05 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT CHANNEL LOCATED AT BS 1510 AND LBL 15 FOUND TO BE CORRODED UNDER NUTPLATES.

Source: SDR U2RA20110105079
OTHER · 2012-01-05 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FORWARD CARGO COMPARTMENT AT BS 845 AND RBL 19, STIFFENER FOUND CRACKED.

Source: SDR U2RA20120105080
Earlier reports · 2002–2011 · 79 reports

2011

OTHER · 2011-12-13 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

DENT FOUND ON TOP OF FRAME AT BS 690 S24L.

Source: SDR U2RA20111213077
OTHER · 2011-12-13 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT AT BS 1350 LBL 7.5, FLOOR SUPPORT WAS FOUND TO BE CORRODED.

Source: SDR U2RA486DHN078
OTHER · 2011-12-03 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

BS 1681 S17R, AFT LOWER WEB INTERCOSTAL FOUND TO BE CORRODED.

Source: SDR U2RA2011120300076
OTHER · 2011-11-29 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT - SPLICE ANGLES HAS SEVERAL AREAS OF CORROSION, BS1340 - 1345 RBL 2.7, LBL 2.90, LBL 7.55 AND LBL 10.95.

Source: SDR U2RA2011112948675
OTHER · 2011-11-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 1335) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT, FLOOR SUPPORT "Z" CHANNEL FOUND TO BE CORRODED UNDER NUT-PLATES AT BS 1335 LBL 10.

Source: SDR U2RA2011112948674
OTHER · 2011-10-25 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE SKIN BS 460, BETWEEN S23R AND S24R, DENTED. REPAIRED IAW SRM 53-00-01/REPAIR 2.

Source: SDR U2RA486DHN071
OTHER · 2011-10-17 Matched by certificate designator
ATA 5340

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

R4 DOOR WEB & ATTACHING SUPPORT FOR FLOORBEAM AT BS1640 - 1681 REPLACED DUE TO CORROSION.

Source: SDR U2RA20111017070
OTHER · 2011-10-14 Matched by certificate designator
ATA 5310

Part: BEAM — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN PRESSURE RESISTANT BEAM CRACKED AT FASTENER HOLE AT STA BS 1681 BL 0.

Source: SDR U2RA20111014068
OTHER · 2011-10-14 Matched by certificate designator
ATA 5320

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO ZEE CHANNEL FRAME SUPPORT, CORRODED AT BS 1320 RBL 10.

Source: SDR U2RA20111014066
OTHER · 2011-10-14 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

BS377 LBL45 - 62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM, AREA DAMAGE CUT-OUT 85 INCHES.

Source: SDR U2RA20111014067
OTHER · 2011-10-14 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

BS377 LBL 45-62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM. AREA DAMAGE CUT-OUT 85 INCHES.

Source: SDR U2RA201110140066
OTHER · 2011-10-14 Matched by certificate designator
ATA 5340

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

BS 1720 RBL 53, HEAVY CORROSION ON CORNER FITTING BELOW AFT PRESSURE BULKHEAD.

Source: SDR U2RA20111014069
OTHER · 2011-10-04 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN, L1 DOOR LOWER SILL HAS CORROSION, APPROX 10 INCHES FROM FORWARD FRAME.

Source: SDR U2RA
OTHER · 2011-10-04 Matched by certificate designator
ATA 5330

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT, PUNCTURE IN BELLY FUSELAGE SKIN BTW BS 1661 - 1681.5 AT LBL 11, APPROX NR 10 SIZE HOLE.

Source: SDR U2RA486DHN061
OTHER · 2011-10-04 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

INTERCOSTAL AFT SIDE OF FLOORBEAM AT BS 1320 LBL45 BELOW SEAT TRACK IS CRACKED.

Source: SDR U2RA20111004003
OTHER · 2011-10-04 Matched by certificate designator
ATA 5320

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 53,893 hrs · 23,065 cycles

BS 376 AT RBL 66, CUSP HAS CORROSION ON BOTTOM SIDE.

Source: SDR U2RA486DHN062
OTHER · 2011-10-04 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

BS 336, LBL 53 FWD OF L1 DOOR HAS CORROSION, AROUND NUTPLATES AND HOLE DRILLED IN RADIUS WITH GOUGE INSIDE.

Source: SDR U2RA20111004001
OTHER · 2011-08-23 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FORWARD CARGO LT BS 508 - 660, TRANSITION ANGLE CORRODED TOP AND BOTTOM.

Source: SDR U2RA20110823001
OTHER · 2011-08-16 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT, FLOOR SUPPORT, LT SIDE WEB AT FUSELAGE STATION 1530 - 1640, HAS CORROSION ON NUTPLATE UNDER WEB.

Source: SDR U2RA20110816001
OTHER · 2011-08-11 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT "Z" CHANNEL AT STATION BS 1510, RBL 10 HAS CORROSION UNDER NUTPLATES.

Source: SDR U2RA486DHN054
OTHER · 2011-08-11 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — DAMAGED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FORWARD CARGO COMPARTMENT, INTERCOSTAL BETWEEN FR620 AND FR640 AND BETWEEN S26L AND S27L IS DAMAGED AT FASTENER HOLE. DAMAGE MEASURES 2.75" X 0.75".

Source: SDR U2RA486DHN052
OTHER · 2011-08-11 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 1200-1240) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, RT SIDE FLOOR SUPPORT TO SLANT PANEL AT STATION BS 1200 - BS 1240 HAS CORROSION AROUND FASTENER HOLES.

Source: SDR U2RA486DHN055
OTHER · 2011-08-11 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT "Z" CHANNEL AT STATION BS1490 - 1500 AND LBL 7.55 CORRODED.

Source: SDR U2RA486DHN056
OTHER · 2011-08-11 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT "Z" CHANNEL AT STATION 1510 AND LBL10 HAS CORROSION UNDER NUTPLATES.

Source: SDR U2RA486DHN057
OTHER · 2011-08-11 Matched by certificate designator
ATA 5320

Part: SUPPORT ANGLE — CORRODED (BS 1701-1702) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN, R & R ANGLE BETWEEN STATION BS 1701 - 1702, RT SIDE OF BL 0 DUE TO CORROSION AT FASTENER HOLE.

Source: SDR U2RA486DHN053
OTHER · 2011-07-29 Matched by certificate designator
ATA 5230

Part: DOOR — GOUGED (CARGO BAY) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT DOOR HAS NICK (GOUGE) BETWEEEN FUSELAGE STATION BS1400 AND BS 1420 AND BTW S24R AND S25R.

Source: SDR U2RA486DHN051
OTHER · 2011-07-28 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO CEILING AT FUSELAGE STATION 1320, RBL-44, INSPECTION REVEALED INTERCOSTAL WEB CRACKED. CRACK LENGTH APPROX 2".

Source: SDR U2RA486DHN049
OTHER · 2011-07-28 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — DAMAGED (BS 1681) · airframe 53,893 hrs · 23,065 cycles

INSPECTION REVEALED THAT THE FLOORBEAM LOCATED AT FUSELAGE STATION 1681 AND LBL 10.5 HAS A HOLE.

Source: SDR U2RA486DHN050
OTHER · 2011-07-14 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FUSELAGE STA 1683 TO 1705 AT RBL 48, SEVERAL AREAS OF CORROSION ON SHEAR WEB.

Source: SDR U2RA486DHN048
OTHER · 2011-07-11 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN, FUSELAGE STATION 1640 AT LBL55 - LBL61, CORROSION ON TOP CAP OF THE FLOORBEAM.

Source: SDR U2RA486DHN044
OTHER · 2011-07-11 Matched by certificate designator
ATA 5320

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FUSELAGE STA BS1688 TO BS1714 AT BL0, CORROSION ON CENTER HAT CHANNEL IN SEVERAL AREAS.

Source: SDR U2RAA486DHN047
OTHER · 2011-07-11 Matched by certificate designator
ATA 5320

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FUSELAGE STA 1681, THRESHOLD SUPPORT ANGLE HAS CORROSION, AT RBL55/WL210.

Source: SDR U2RA486DHN041
OTHER · 2011-07-11 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN AREA, FLOOR SUPPORT BETWEEN FUSELAGE STA BS1681.5 AND BS1701 AT LBL52 HAS CORROSION AT FASTENER HOLES.

Source: SDR U2RA486DHN043
OTHER · 2011-07-11 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE 1701, AT RBL 24, CORROSION ON SHEAR WEB (AFT DECK PLATE) AROUND FASTENER HOLES.

Source: SDR U2RA486DHN039
OTHER · 2011-07-11 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

REMOVED R4 DOOR SURROUNDING WEB & ATTACHING SUPPORTS FOR FLOORBEAM REPLACEMENT. THRESHOLD WEB - CORRODED OUT OF LIMITS. WEB SUPPORTS, (PN 146N5246-6 & -8) 100 PERCENT EXFOLIATION CORROSION. WEB SUPPORTS, (PN 146N8769-23 & -41) CORRODED OUT OF LIMITS. TOP OF FLOORBEAM CAP CORRODED AT FUSELAGE STA 1640, BETWEEN LBL55 - LBL61.

Source: SDR U2RA486DHN046
OTHER · 2011-07-11 Matched by certificate designator
ATA 5320

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT, NR2 AFT WET AREA FLOOR STRUCTURE UNDERNEATH OF WEB, STIFFENER HAS CORROSION AT FUSELAGE STA BS 1714/RBL23.

Source: SDR U2RA486DHN040
OTHER · 2011-07-11 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FLOORBEAM AT FUSELAGE STA 1320 AT LBL19 TO RBL19 CORROSION AROUND FASTENER HOLES.

Source: SDR U2RA486DHN042
OTHER · 2011-07-11 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, FLOOR SUPPORT "Z" CHANNELS HAS CORROSION UNDER ALL DOUBLE NUTPLATES AT FUSELAGE STATION 1330 AT RBL20 - LBL20.

Source: SDR U2RA486DHN045
OTHER · 2011-07-08 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE 1200 AT BL 0, INTERCOSTAL HAS MULTIPLE CRACKS.

Source: SDR U2RA486DHN037
OTHER · 2011-07-08 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (BS 700-720) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN BETWEEN FUSELAGE STA BS 700 AND BS 720, NR2 DOOR SILL LT PLATE, 1 EA NUTPLATE CORRODED AND 1 EACH MISSING, (FLOOR PANEL MOUNT).

Source: SDR U2RA486DHN035
OTHER · 2011-07-08 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

INTERCOSTAL, CRACKED 2 EA PLACES AT FUSELAGE STA BS 1620 - 1640 AT LBL46. 1ST CRACK LENGTH APPROX 1.00 INCHES, 2ND CRACK LENGTH APPROX 0.75 INCHES.

Source: SDR U2RA486DHN038
OTHER · 2011-07-07 Matched by certificate designator
ATA 5320

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT, NR2 AFT WET AREA MAIN CABIN FLOOR STRUCTURE UNDERNEATH OF FLOOR WEB, 1 EACH STIFFENER HAS CORROSION, FUSELAGE STA 1714 AT RBL35.

Source: SDR U2RA486DHN036
OTHER · 2011-06-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 344-365) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN, STATION 344-365, BUTT LINE 0, FLOOR SUPPORT CORROSION AROUND HOLES.

Source: SDR U2RA486DHN034
OTHER · 2011-06-17 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (BS 720 S23L) · airframe 53,893 hrs · 23,065 cycles

DENT IN TOP OF FRAME AT STA 720, STR 23L.

Source: SDR U2RA486DHN033
OTHER · 2011-06-10 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, FUSELAGE STA BS1420 AT RBL 10.40, FOUND INTERCOSTAL CRACKED. CRACK LENGTH 1.5".

Source: SDR U2RA486DHN032
OTHER · 2011-05-16 Matched by certificate designator
ATA 5315

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN PASSENGER CABIN FLOOR SUPPORT BETWEEN BS 1681.8 - 1701 AT RBL 52 CORRODED AT FASTENER HOLE.

Source: SDR U2RA486DHN030
OTHER · 2011-05-16 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 1701) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FLOORBEAM STA 1701, RBL 24 CORROED ON UPPER FLANGE.

Source: SDR U2RA486DHN031
OTHER · 2011-04-26 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

CORROSION ON WEB SUPPORT BETWEEN FUSELAGE STATION BS1660 TO BS1680, AT RBL12, AS WELL AS REPAIR FASTENERS TOO CLOSE TO FLOORBOARD MOUNTING HOLES.

Source: SDR U2RA486DHN029
OTHER · 2011-04-21 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

STRINGER AT FUSELAGE STATION BS 670 AT RBL 2.9, CORROSION UNDER NUTPLATE.

Source: SDR U2RA486DHN028
OTHER · 2011-04-20 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO COMPARTMENT AT FUSELAGE STA BS 1340, BETWEN STRINGER S22L AND S23L. FRAME TOP LEG DENTED ABOVE SPLICE.

Source: SDR U2RA486DHN027
OTHER · 2011-04-20 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 53,893 hrs · 23,065 cycles

BS 1320 - 1340 AT LBL 24 INTERCOSTAL CRACKED AT FASTENER HOLE. CRACK LENGTH 1.5".

Source: SDR U2RA486DHN026
OTHER · 2011-04-08 Matched by certificate designator
ATA 5340

Part: STRINGER CLIP — CRACKED (BS 1240 S27L) · airframe 53,893 hrs · 23,065 cycles

EXTERIOR FUSELAGE AT FUSELAGE STA BS 1240, LT STRINGER S27L INTERCOSTAL SUPPORT CLIP CRACKED, CRACK LENGTH APPROX 1.5" LONG.

Source: SDR U2RA486DHN025
OTHER · 2011-03-25 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, NR 3 EMERGENCY EXIT LOWER SILL, BETWEEN BS1320-1360 AT S17L, HAS CORROSION AROUND SEVERAL HOLES.

Source: SDR U2RA486DHN024
INADEQUATE Q C · 2011-03-21 Matched by certificate designator
ATA 5330

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 52,008 hrs · 18,231 cycles

FUSELAGE REPAIR AT STA BS1520, BETWEEN S8L AND S10L REQUIRES REWORK. DOES NOT MEET THE REQUIREMENTS OF SRM 53-00-01, REPAIR NR 2.

Source: SDR U2RA227DHN041
OTHER · 2011-03-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT "Z". CHANNEL HAS CORROSION UNDERNEATH NUTPLATE AT STA BS1355, LBL4.

Source: SDR U2RA486DHN022
OTHER · 2011-03-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 53,893 hrs · 23,065 cycles

F/O SEAT TRACK GUIDE PIN HOLES ARE ALL GOUGED AND ELONGATED.

Source: SDR U2RA486DHN023
OTHER · 2011-03-15 Matched by certificate designator
ATA 5340

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE EXTERIOR BODY STA 1180 AT L29L ATTACH ANGLE CRACKED. CRACK LENGTH 0.5"

Source: SDR U2RA486DHN021
OTHER · 2011-03-14 Matched by certificate designator
ATA 5230

Part: STRINGER — CRACKED (CARGO DOOR) · airframe 53,893 hrs · 23,065 cycles

FWD CARGO DOOR STRINGER CRACKED AT S19L, STA 618.

Source: SDR U2RA486DHN019
OTHER · 2011-03-14 Matched by certificate designator
ATA 5230

Part: STRINGER — CRACKED (CARGO DOOR) · airframe 53,893 hrs · 23,065 cycles

FUSELAGE STA BS440 AT S19L FWD CARGO DOOR STRINGER IS CRACKED.

Source: SDR U2RA486DHN020
OTHER · 2011-03-13 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 1445-1500) · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT Z CHANNEL STA 1445-1500, RBL 8, CORROSION UNDER 4 EA NUTPLATES.

Source: SDR U2RA486DHN017
OTHER · 2011-03-13 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, FLOOR SUPPORT Z CHANNEL STA 1445-1500, RBL 3 CORROSION UNDER 4 EA NUTPLATES.

Source: SDR U2RA486DHN018
OTHER · 2011-03-11 Matched by certificate designator
ATA 5320

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FWD BELLY PIT EQUIPMENT COOLING RACK 212B, FWD CARGO STRAP HAS CORROSION ON AND AROUND SEVERAL NUTPLATES.

Source: SDR U2RA486DHN016
OTHER · 2011-03-09 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, FLOOR SUPPORT Z CHANNEL STA 1480-1490, LBL 15 CORROSION UNDER 2 NUT PLATES.

Source: SDR U2RA486DHN015
OTHER · 2011-03-08 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

FLOOR LEVEL WEB AT STA 1350-1360 LT OTBD CORROSION AT AND AROUND FASTENER HOLES.

Source: SDR U2RA486DHN014
OTHER · 2011-03-03 Matched by certificate designator
ATA 5320

Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

SHEAR WEB CORRODED, STA 1701-1720 AT RBL 53.

Source: SDR U2RA486DHN013
OTHER · 2011-03-02 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

STA 650, LBL 13, CORROSION ON FLOOR SUPPORT UNDER NUTPLATE.

Source: SDR U2RA486DHN009
OTHER · 2011-03-02 Matched by certificate designator
ATA 5300

Part: MOUNT — CORRODED (BS 1685) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN CTR GALLEY MOUNT STA 1685, BL 0 CORROSION.

Source: SDR U2RA486DHN010
OTHER · 2011-03-02 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

CORROSION UNDER NUTPLATE ON FLOOR SUPPORT, STA 655, LBL 9.

Source: SDR U2RA486DHN011
OTHER · 2011-03-02 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO STA 1460-1480, LBL 4, FLOOR SUPPORT CORRODED AROUND FASTENER HOLES.

Source: SDR U2RA486DHN008
OTHER · 2011-03-02 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, STA 1340, LBL8 VERTICAL SUPPORT FLOOR SUPPORT HAS CORROSION.

Source: SDR U2RA486DHN012
OTHER · 2011-03-01 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT "Z" CHANNEL STA. 1390 RBL 20, CORROSION UNDER 2 EACH NUTPLATES.

Source: SDR U2RA486DHN006
OTHER · 2011-03-01 Matched by certificate designator
ATA 5300

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO, STA. 1340-1360, RBL 8,FLOOR SUPPORT HAS CORROSION AROUND NUTPLATES.

Source: SDR U2RA486DHN007
OTHER · 2011-02-28 Matched by certificate designator
ATA 5320

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

CUSP ANGLE STA 740-760 RBL 66 HAS CORROSION AROUND SEVERAL FASTENER HOLES.

Source: SDR U2RA486DHN005
OTHER · 2011-02-21 Matched by certificate designator
ATA 5320

Part: SUPPORT CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

AFT CARGO FLOOR SUPPORT -Z- CHANNEL HAS CORROSION UNDERNEATH NUT PLATES AT STA 1440 STR. 29R.

Source: SDR U2RA486DHN002
OTHER · 2011-02-21 Matched by certificate designator
ATA 5340

Part: MOUNT — CORRODED (ZONE 900) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN GALLEY MOUNT HAS CORROSION AT STA. 333 LBL 60.

Source: SDR U2RA486DHN004
OTHER · 2011-02-21 Matched by certificate designator
ATA 5340

Part: MOUNT — CORRODED (BS 338) · corrosion level 2 · airframe 53,893 hrs · 23,065 cycles

MAIN CABIN GALLEY MOUNT HAS CORROSION AT STA. 338 LBL 20.

Source: SDR U2RA486DHN003
OTHER · 2011-02-21 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (ZONE 100) · airframe 53,893 hrs · 23,065 cycles

4 CRACKS ON FLOOR WEB, STATION 1620-1640BLO; AT FASTENER HOLES (2").

Source: SDR U2RA486DHN001

2002

OTHER · 2002-08-02 Unresolved
ATA 3510

Part: LINE — CHAFED (OXYGEN SYSTEM)

OXYGEN SUPPLY LINE WAS FOUND TO HAVE A HOLE RUBBED INTO IT FROM RAM AIR DUCT (THE DUCT SUPPORT COIL). A VISUAL INSPECTION OF THE AREA, WHEN ON GROUND, APPEARS TO HAVE CLEARANCE. BUT OUT BELIEF IS THAT IN THE AIR WITH RAM AIR COMING IN IT BOTH EXPANDS AND MOVES THE DUCT TO RUB THE OXYGEN LINE.

Source: SDR IBU2002F00000
FLT CONT AFFECTED · 2002-01-17 Unresolved
ATA 8530

Part: PISTON — FAILED (ENGINE)

TRANSISITIONING FROM TAKE-OFF TO CLIMB PHASE OF FLIGHT, AFTER REDUCING POWER NR 1 ENGINE SHUTDOWN. PILOT FEATHERED PROP AND MADE UNEVENTFUL LANDING. REMOVAL OF NR 5 CYLINDER REVEALED SEVERE DAMAGE TO THE TOP OF THE PISTON, WITH BROKEN RINGS. VALVE WERE REALITIVELY INTACT. FURTHER INSPECTION REVEALED DAMAGE TO ALL PISTONS, THOUGH NOT AS SEVERE.

Source: SDR 2002F00038