N6813
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.
42 reports on file, 1995-06-05 – 2001-12-12.
Part: SKIN — CRACKED · airframe 82,273 hrs · 57,044 cycles
FUSELAGE SKIN BS 211, STR 25R GOUGED AND CRACKED AT FWD E/E DOOR CUTOUT.FOUND ON SERVICE CHECK--N/R CARD 431 WRITTENCORRECTIVE ACTION: STOP DRILLED CRACK IAW B727 SRM 51-10-1. DYE PEN. IAW BOEING S.O.P. 20-50-2. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B727 SRM 53-30-3 FIG. 1 & 51-30-2.
Part: STIFFENER — CORRODED · airframe 82,273 hrs · 57,044 cycles
VERTICAL STIFFENER CORRODED BS 336 RBL 14.6 BELOW FLOOR PAN.FOUND ON CPCP C53-111-03 PAGE 4, N/R CARD 405 WRITTENCORRECTIVE ACTION:REMOVED AND REPLACED STIFFENER IAW B727 SRM 51-30-2.
Part: SKIN — CORRODED · airframe 82,273 hrs · 57,044 cycles
FUSELAGE SKIN CORRODED AT BS 336, STR 25R.WRITTEN FROM NON-ROUTINE CARD 405 FROM CPC C53-111-03 PAGE 4--N/R CARD 435 WRITTENCORRECTIVE ACTION:REMOVED DAMAGED SKIN, HFEC AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. 53-01630-1, BOEING MESSAGE EOI-DAL-1-00024H.
Part: STIFFENER — CRACKED · airframe 82,273 hrs · 57,044 cycles
L/H MLG W/W BS 870 LBL 45 VERTICAL STIFFENER CRACKED.FOUND ON CPCP INSP. C-53-100-01 PAGE 1, N/R CARD 410 WRITTENCORRECTIVE ACTION:FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-4 & 51-30-2.
Part: FRAME — CORRODED (FUSELAGE) · airframe 82,273 hrs · 57,044 cycles
NOSE WHEEL WELL STA 296, RBL 12 UPPER CHORD CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51-10-1 & 51-30-2.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 82,273 hrs · 57,044 cycles
CHORD CORRODED BS 312-348 LBL 14.6, WL 169. FOUND ON CPCP C53-111-03 PAGE 4 N/R CARD 401 WRITTEN. REMOVED CHORD IAW B727 SRM 51-30-2, INSTALLED NEW CHORD IAW B727 SRM 51-30-2-51-10-1.
Part: ANGLE — CORRODED · airframe 82,273 hrs · 57,044 cycles
ANGLE IN R/H W/W CORRODED, BS 870 RBL 48.0FOUND DURING CPCP C53-100-01 PAGE 1, N/R CARD 411 WRITTENCORRECTIVE ACTION:REMOVED ANGLE, FABRICATED NEW ANGLE FROM 7075-T6-063 AND INSTALLED IAW B727 SRM 51-30-2.
Part: FRAME — CORRODED (FUSELAGE) · airframe 82,273 hrs · 57,044 cycles
NOSE WHEEL WELL STA 296, LBL 12 UPPER FRAME CORRODED. FOUND ON CPCP CHECK. REMOVED AND REPLACED FRAME IAW B727 SRM 51-10-1 & 51-30-2.
Part: PANEL — CORRODED · airframe 82,273 hrs · 57,044 cycles
NOSE W/W PANEL BS 330 TO 350 STR L27 CORRODEDFOUND ON CPCP C53-100-01 PAGE 1, N/R CARD 444 WRITTENCORRECTIVE ACTION:REMOVED CORROSION IAW B727 SRM 51-10-6 FABRICATED REPAIR IAW 51-40-2 AND INSTALLED REPAIR IAW B727 SRM 51-40-2 & 51-30-2.
Part: DOOR — OUT OF ADJ (MAIN CARGO DOOR) · airframe 82,205 hrs · 57,001 cycles
F/E PANEL MAIN CARGO DOOR WARNING LIGHT ILLUMINATE, PRESSURIZATION NORMAL, ALT FL310 PSID 8.0. MAIN CARGO DOOR PANEL, DOOR WARNING LIGHT, VENT DOOR OPEN, AND MAIN CARGO DOOR NOT CLOSED. ADJUSTED MAIN CARGO DOOR, DOOR CLOSED, AND LATCH CLOSED SWITCHES AND OPS CHECKED GOOD IAW AEI MM.
Part: SWITCH — INOPERATIVE (MAIN CARGO DOOR) · airframe 82,203 hrs · 57,000 cycles
DURING CLIMB, RED MCD LIGHT ALONG WITH AMBER VENT DOOR NOT CLOSED ILLUM. ALONG WITH UNSCHEDULED CLIMB IN CABIN ALT. ACC. AERONAUTICAL MCD WARNING ILLUM. IN FLT. AFTER RAPID DEPRESS. CHECKLIST COMPLETED LAND AT NEAREST SUITABLE AIRPORT.CORRECTIVE ACTION:DUPLICATED MALFUNCTION ON GROUND AND FOUND VENT DOOR SWITCH ITNERMITTENTLY DEFECTIVE ALLOWING THE VENT DOOR NOT TO CLOSE FULLY. REPLACED VENT DOOR SWITCH AND SYS CHECKED NORMAL WITH A/C PRESSURIZED.
Part: RIVET — SHEARED · airframe 81,944 hrs · 56,817 cycles
RIVET MIGRATED AT 1183 BULKHEAD AFT LT. SIDE 12" O/B OF DOOR CUT-OUT & 10" BELOW DOOR TOP (EO)FOUND DURING B-2 CHECKCORRECTIVE ACTION:CUT-OFF HEAD OF TRAPPED (MIGRATING) RIVET PER E.O. #01-163. INSTALLED TWO EACH HLT 428-6 HILOCS IAW E.O. #01-163 & SEALED WITH PR 1422 B1/2 IAW E.O. #01-163 WITH APPROVED 8110-3 DATED 6/7/01
Earlier reports · 1995–2000 · 30 reports
2000
Part: CONTROLLER — FLUCTUATES (CABIN) · airframe 81,261 hrs · 56,356 cycles
NR 1 GENERATOR UNDERVOLTAGE LIGHT ILLUMINATED, TRIPPED NR 1 BUS TIE AT 5000 FT, AIR TURNBACK. REMOVED AND REPLACED NR 1 GENERATOR LOAD CONTROLLER AND GCU, OPS CHECK GOOD.
Part: UPLOCK SWITCH — FAILED (NLG) · airframe 81,165 hrs · 56,236 cycles
AFTER GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED, AS WELL AS AFTER MANUAL GEAR EXTENSION. FOUND BROKEN WIRE ON NOSE GEAR UPPER LOCK SWITCH, RE-CRIMPED WIRE IAW M/M 20-11. OPS CHECK NORMAL.
1999
Part: MECHANISM — FAILED (L1 DOOR)
AIRCRAFT LOST PRESSURIZATION, DIVERTED TO BRU AT 0200Z) UNABLE TO OPEN L1 DOOR. (M)
Part: BATTERY — DISCHARGED (BATT COMPT)
ON LANDING, APU FAILED TO START FOUND BATTERY VOLTAGE AT 4, BATTERY CHARGER C/B POPPED. BATTERY WARMS TO TOUCH. NOTICED SMOKE IN COCKPIT. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER. (M)
Part: COMPRESSOR — STALLED (NR 2 ENGINE)
NR 2 ENGINE COMPRESSOR STALLS. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK GOOD. REPLACED 13TH STAGE SURGE BLEED VALVE. (M)
Part: SWITCH — FAILED (NLG)
AFTER NOSE GEAR EXTENSION, BOTH GREEN AND RED ILLUMINATED. AFTER MAIN GEAR EXTENDED, ONLY GREEN LIGHT ON. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH, PERFORMED GEAR SWING NUMEROUS TIMES. OPS CHECK GOOD PER MM 32-61-7. (M)
Part: WIRE — BROKEN (COCKPIT)
NOSE GEAR RED UNSAFE LIGHT ON AND GREEN LIGHT ON WITH GEAR EXTENDED. REPAIRED GROUND WIRE FROM LOCK SWITCH. (M)
Part: DUCT — CRACKED (FUSELAGE)
LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHILE ENGINE ANTI-ICE WING ANTI-ICE WERE IN USE. CLOSING THE WING ANTI-ICE AND A CO-INCIDENTAL REDUCTION IN POWER DURING AN APPROACH EXTINGUISHED LIGHT. LOG PAGE 58944 MEL 30-2 PLACARD 980. REMOVED AND REPLACED CRACKED PNEUMATIC DUCT ABOVE APU NEAR KEEL BEAM IAW MM 36-00-1, PAGE 201. LEAKS CHECK GOOD PER MM 30-13-0A, PAGE 506, PLACARD REMOVED. (M)
1998
Part: OVERHEAT LIGHT — ILLUMINATED (LOWER AFT BODY)
SHORTLY AFTER SELECTING WING ANTI-ICE ON, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, EXTINGUISHED AFTER TURNING OFF ENGINE NR 3 ANTI-ICE. ENGINE NR 1 OPENED NORMAL. OPS CHECKED IN AIR AND GROUND MODES, OPS CHECKED NORMAL IAW MM CHAPTER 26. (M)
Part: INDICATOR — MALFUNCTIONED (COCKPIT)
NR 2 ENGINE OIL TEMP EXCEEDED RED LINE DURING FLIGHT. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER FLIGHT MANUAL. FOUND NR 2 OIL TEMP BULB GROUND WIRE BROKEN AT TERMINAL BLOCK. SPLICED WIRE ON TERMINAL BLOCK IAW MM CHAPTER 20. (M)
1997
Part: DOUBLER — CRACKED (LT TE MID FLAP)
LT WING, OUTBOARD MID FLAP, LOWER FORWARD SKIN HAS SEVERAL CRACKS ON DOUBLER AT OUTBOARD FORE FLAP TRACK AREA. FABRICATED DOUBLER AND FILLER PER SRM 51-40-03. (M)
Part: FLOORBEAM — CORRODED (BS 328)
MAIN CABIN, FLOOR BEAM FS 320 HAS CORROSION ON TOP CAP. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-08. (M)
Part: SKIN — DELAMINATED (NR 7 SPOILER)
RT WING, NR 7 SPOILER DELAMINATED AT FWD CENTER SECTION. REPAIRED SPOILER DELAMINATION PER SRM 51-40-06 AND 51-40-09. (M)
Part: SUPPORT — CRACKED (BS 400-420)
MAIN CABIN, FLOOR SUPPORT WEB UPPER FLANGE HAS SEVERAL CRACKS FROM FS 400 T0 420. UPPER FLANGE REMOVED DUE TO CARGO MOD AND REPLACED BY CHANNEL, REF STC SA-1998 SO AND DRAWING AE 727-2-063. (M)
Part: SUPPORT — CRACKED (BS 720)
MAIN CABIN, SUPPORT WEB UPPER FLANGE HAS SEVERAL CRACKS FROM FS 720 TO 720B BL 0. UPPER FLANGE REMOVED DUE TO TRACK INSTALLATION FOR CARGO MOD, REF STC SA-1998-SO AND DRAWING AE 727-2-063. (M)
Part: FLOORBEAM — CORRODED (BS 360)
MAIN CABIN, FLOORBEAM FS 360 HAS CORROSION ON TOP CAP. REMOVED AND REPLACED TO CAP PER SRM 53-10-08. (M)
Part: STRINGER — CRACKED (BS 380)
STRINGER S-1 CRCKED AT FS 380. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M)
Part: STRINGER — CRACKED (BS 335)
CIRCULAR CRACK BETWEEN TWO FAST ON STRINGER 24R AT FS 335. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1 AND 51-30-02. (M)
Part: FLOORBEAM — CORROSION (BS 360)
MAIN CABIN, FLOORBEAM UPPER CAP HAS CORROSION AT FS 360 BL 15L TO BL 15R. FABRICATED AND INSTALLED NEW TOP CAP PER SRM 53-10-08. (M)
Part: ANGLE — CORRODED (BS 460)
MAIN CABIN, OUTBOARD ANGLE RIGHT SIDE HAS CORROSION AT FS 460. REMOVED AND REPLACED ANGLE PER SRM 51-10-06. (M)
Part: STRINGER — CRACKED (BS 360)
STRINGER S-1 CRACKED AT FS 360. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M)
Part: SKIN — CRACKED (WS 450)
LEFT WING LEADING EDGE UPPER SURFACE EXTERIOR SKIN HAS APPROX 0 INCH CRACK AT WS 450. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1 AND 51-30-02. (M)
Part: STRINGER — CRACKED (BS 400)
STRINGER S-1 CRACKED AT FS 400. REMOVED DAMAGED AREA AND REPAIR SECTION IAW SRM 53-10-3. (M)
Part: ANGLE — CORRODED (BS 400-420)
MAIN CABIN, FLOOR SUPPORT FS 400-420 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-04. (M)
Part: INTERCOSTAL — CRACKED (BS 740)
MAIN CABIN, INTERCOSTAL AT FS 740 BL 20L HAS PREVIOUS REPAIR DOUBLER WITH 2 INCH LONG CRACK. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 41-40-02. (M)
Part: ACTUATOR — BROKEN (RT MLG)
PHL - FLT 0512 - DURING APPROACH TO PHL WHEN LANDING GEAR EXTENDED, RT MAIN LANDING GEAR FAILED TO EXTEND NORMALLY, RECYCLED LANDING GEAR WITH SAME RESULTS. ACCOMPLISHED MANUAL GEAR EXTENSION IAW ABNORMAL PROCEDURES AND AIRCRAFT LANDED PHL WITHOUT INCIDENT. REPLACED RT MLG SEQUENCE DOOR LOCK ACTUATOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: WIRE — BROKEN (NLG)
DFW - FLT 475 - DURING APPROACH TO DFW, WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. VISUALLY CONFIRMED NOSE LANDING GEAR EXTENDED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPAIRED BROKEN WIRES ON NOSE LANDING GEAR LOCK SWITCH HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: SKIN — CRACKED (BS 410)
TUL - FOUND SKIN CRACKED AT 4 RIVITS HEADS, STATION 410. CUT OUT CRACKS IN SKIN INSTALLED REPAIR PER SRM 53-30-3 . (M)
1995
Part: WIRE — BROKEN (NLG)
ORD - FLT 1262 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT. RECYCLED LANDING GEAR WITH SAME RESULTS. WHILE ACCOMPLISHING A GO-AROUND RED NOSE LANDING GEAR LIGHT EXTINGUISHED AND GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT NOSE LANDING GEAR UP AND LOCKED SWITCH PIN A08. ALSO, REPLACED NOSE LANDING GEAR UP AND LOCKED SWITCH FOUND DEFECTIVE DURING TROUBLESHOOTING. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)