N936FR
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.
27 reports on file, 2006-07-29 – 2011-10-14.
Part: SOLENOID VALVE — FAILED (A/C PACK) · airframe 24,002 hrs · 11,771 cycles
A/C PACK 2 FAILED IN FLIGHT. PACK 1 ON MEL SO PACK 2 FAIL CAUSED A CABIN DEPRESSURIZATION AND 02 MASK TO DEPLOY. R & R PRESSURE REGULATOR VALVE SOLENOID 10HA2 IAW AMM 36-11-55, PB 401. OP'S AND LEAK CHECKED GOOD.
Part: SERVO — SLOW (ELEVATORS) · airframe 21,989 hrs · 10,784 cycles
ON ROTATION ACFT ROLLS RT REGARDLESS OF WIND. PERFORMED FLT CONTROL MOVEMENT CHECKS FOUNFD LT ELEVATOR SERVO SLOW TO REACT. REF LP 596444, ITEM 1, R & R SERVO CONTROL ELEVATOR LT GREEN HYD REF AMM 27-34-51-400-001 AND 27-34-51-0000.001, OPS CHECK NORMAL.
Part: COMPUTER — MALFUNCTIONED (FLT CONTROL) · airframe 21,732 hrs · 10,665 cycles
AT LIFT OFF, AN UNCOMMANDED ACFT ROLLED RT. AT TOUCHDOWN, AT SPEEDBRAKE DEPLOYMENT, ACFT AGAIN ROLLED RT AND REQUIRED SIGNIFICANT LT AILERON INPUT TO KEEP LT MLG ON THE GROUND. REPLACED NR 1 SEC IAW AMM 27-94-34, PB 401. OPS CHECKED GOOD AND OPS CHECK FIGHT WAS SATISFACTORY.
Part: SHOCK ABSORBER — SCRATCHED (LT MLG) · airframe 21,353 hrs · 10,491 cycles
LT MLG SHOCK ABSORBER SCRATCHED IN CHROME AREA. 60 TO 80 SCRATCHES 18 INCHES LONG X .003 INCHES DEEP ON FWD SIDE OF STRUT. R & R LT MLG SHOCK ABSORBER IAW AMM 32-11-13-020-058B AND 32-11-13-420-054B.
Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 21,353 hrs · 10,491 cycles
LT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 3 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.
Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,353 hrs · 10,491 cycles
R2 DOOR SILL BEAM HAS 1 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R R2 DOOR SILL BEAM IAW SRM 51-72-11 PG 1-2.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 21,353 hrs · 10,491 cycles
RT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 8 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO53EO31434.
Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,353 hrs · 10,491 cycles
L2 DOOR SILL BEAM HAS 3 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R L2 DOOR SILL BEAM IAW SRM 51-72-11, PG 1-2.
Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE N0660; AFT CARGO COMPARTMENT FLOOR PANEL 151DE HAS 2 EA PUNCTURES. REPAIRED 2 EACH PUNCTURES IAW SRM 53-02-00, PARA 8B.
Part: FLOORBOARD — PUNCTURED (ZONE 100) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE NR N0657; AFT CARGO COMPARTMENT FLOOR PANEL 162CF PUNCTURED. REPAIR PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B.
Part: COWL DOOR — DENTED (THRUST REVERSER) · airframe 24,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE NR N0636; NR 2 ENGINE OTBD THRUST REVERSERS INNER PERFORATED COWL BELOW THE UPPER BLOCKER DOOR THERE IS A DENT MEASURING .1250 INCH CIRCUMFERENCE AND .030 INCHES DEEP. REPAIRED 1 INCH DENT IAW CMM 78-32-36, REPAIR NR8.
Part: SKIN — GOUGED (THRUST REVERSER) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE N0633; NR 2 ENGINE OTBD THRUST REVERSER LOWER BLOCKER INTERNAL SIDE THE PERFORATED SKIN HAS A GOUGE MEASURING .7500 INCH LONG, .2500 INCH WIDE AND .115 INCH DEEP. REPAIRED IAW CMM 78-32-36, REPAIR NR8.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE NR N0282; AFT CARGO FLOOR PANEL 152WG DAMAGED, SKIN SEPARATED FROM HONEYCOMB. FABRICATED REPLACEMENT PANEL IAW IRM 9701, REV G.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE N0644; CABIN FLOOR PANEL 242BF DELAMINATED. REPAIRED 56 SQUARE INCHES OF DEBONDED TOP GLASS LAYER OF PANEL 242BF USING MYLAR FOIL IAW SRM 53-02-00, PARA 8J.
Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE N0659; AFT CARGO COMPARTMENT FLOOR PANEL 152TG HAS 1 INCH PUNCTURE. REPAIRED PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B.
Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE N0665; AFT CARGO COMPARTMENT FLOOR PANEL 151AE HAS 3 EACH PUNCTURES. REPAIRED 3 EACH PUNCTURES WITH WET LAYUP IAW SRM 53-02-00, PARA 8B.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 21,354 hrs · 10,491 cycles
C-CHECK: NON ROUTINE N0278; MAIN CABIN FLOORBOARD 252NF HAS COMPOSITE DAMAGE DAMAGE 40 SQUARE INCHES. REPAIRED 40 SQUARE OF COMPOSITE DAMAGE, IAW A319 SRM 53-02-00 PARAGRAPH 8J.
Earlier reports · 2006–2009 · 10 reports
2009
Part: FLOOR PANEL — CRACKED (ZONE 800) · airframe 16,257 hrs · 8,081 cycles
REF: NON ROUTINE C064113. DURING C3 C-CHECK, INSP NOTED THE L2 DOOR FWD SIDE FLOOR PANEL IS CRACKED. MX REMOVED AND REPLACED THE FWD L2 DOOR BLANKING PLATE IAW AMM 52-13-31-000-007 AND 52-13-31-400-007.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 RT, BETWEEN FR 66 AND FR 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-72-11 AND EO A0-53T-11472.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED THE LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW A319 SRM 51-42-11 PARAGRAPH 6 AND 7.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 LT, BETWEEN FRAME 66 AND FRAME 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX REMOVED AND REPLACED THE FLOORBEAM IAW A319 SRM 51-42-11 AND DWG D53475815.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED THAT THE RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT, SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.
Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.
Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED THAT RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.
Part: STRUT — CHAFED (NLG) · airframe 16,257 hrs · 8,081 cycles
DURING C3 C-CHECK, INSP NOTED THE ELECTRICAL CABLE FOR THE TOWING BYPASS SWITCH WAS RUBBING ON THE NLG STRUT. MX REMOVED DAMAGE, PERFORMED FLUORESCENT PENETRANT INSP AND ROTORY FLAP PEENED BLENDED AREAS IAW SRM 51-73-00 AND EA A9-32R-31199. (MAJOR REPAIR)
2007
Part: LIGHT — INOPERATIVE (EXTERIOR OVWING) · airframe 7,564 hrs · 3,756 cycles
MAINTENANCE REPORTED RT AFT EMERGENCY OVERWING OUTSIDE LIGHT (62WL) INOP. REPLACED LIGHT ASSY (62WL) IAW 33-51-15-400-001.
2006
Part: LIGHT — FAILED (EMERGENCY EXIT) · airframe 5,322 hrs · 2,580 cycles
EPSU TEST FAILED IAW HEAVY CHECK WORK CARD. REPLACED RT OVERWING EXIT HATCH HANDLE LIGHT IAW MM 23-73-47, PB 401 AND 33-51-11-420-052A, PERFORMED ANOTHER EPSU TEST AND CHECKED GOOD.