N936DN
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.
126 reports on file, 2009-03-27 – 2019-11-07.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,518 hrs · 30,244 cycles
DURING SVC FOUND CON EXIT FLOOD LIGHTS INOP.REPLACED EMERGENCY BATTER B5-239 PER MD90MM 33-51. OPS CHECK NORM(6611867)
Part: APU BAY — CONTAMINATED · airframe 46,463 hrs · 30,208 cycles
DURING TAKEOFF AND CLIMBOUT. FLIGHT ATTENDANT COULD SMELL A BURNT RUBBER SMELL THROUGHOUT THE ENTIRE A/C. IN THE COCKPIT IT SMELLED LIKE A PETROLEUM PRODUCT OIL OR HYDRAULIC FLUID. IT SEEMED TO DISSIPATE AS WE CLIMBED OUT AND REDUCED POWER / FOUND OIL AROUND AND IN APU COMPARTMENT. T/S IN REF TO AMM TASK21-53-00-720-802. CHANGED SOCK IN REF TO 21-54. C/W NO GO ODI PREVENTION.(4633310)
Part: SENSOR — FAILED (ELEVATORS) · airframe 46,402 hrs · 30,161 cycles
ELEVATOR SPLIT INDICATION IN FLIGHT 12000 MSL 320 KTS. T/S PER NO-GO ODI PROCEDURES. CONFIRMED CONTORL COLUMNS NOT DISCONNECTED. VISUALLY CONFIRMED ELEVATOR SURFACES MOVE TOGETHER . DFGC FAULT REVIEW SHOWED ELEVATOR POS 1 SENSOR SIGNAL FAILURE FOR LAST 4 FLIGHT LEGS. REMOVED AND REPLACED LT ELEVATOR 1 POS 1 SENSOR IAW MD90 AMM 27034. ADJ TEST GOOD. A/C OK FOR SVC. (LP# 6106470)
Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 46,320 hrs · 30,105 cycles
C/W HFEC OF RT HORIZ STAB UPPER REAR SPAR AFT 2 BARREL NUT HOLES PER CARD 5510-01099-01B. AFT BARREL NUT HOLE HAS CRACK INDICATION. END OF CRACK MARKED. HORIZONTAL STABILIZER REPLACED ON R/C 5510-4001 UNSUCCESSFUL PARTS CHANGE SENT TO RECORDS 02888 (LP# 6106412)
Part: PLATE — GALLED (HORIZ STAB) · airframe 46,320 hrs · 30,105 cycles
THE RIGHT INBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-4001/004 00004. REWORKED HINGE PLATE FACES AND BORES IAW SRM 55-30- 05 PARAGRAPH 7. SELECTED MAJOR REPAIR CLOSING REQUIREMENTS RII. (LP# 1279016)
Part: PLATE — GALLED (HORIZ STAB) · airframe 46,320 hrs · 30,105 cycles
THE LEFT OUTBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-4001/005 00005 INSTALLED BUSHINGS AND FINAL SIZED PER SRM 55-30-05 SELECTED MAJOR REPAIR CLOSING REQUIREMENTS. (LP# 1278948)
Part: PLATE — GALLED (HORIZ STAB) · airframe 46,320 hrs · 30,105 cycles
THE RIGHT OUTBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-4001/003 00003. REWORKED HINGE PLATE FACES AND BORES IAW SRM 55-30-05 PARAGRAPH 7. SELECTED MAJOR REPAIR CLOSING REQUIREMENTS. (LP# 1278963)
Part: PLATE — GALLED (HORIZ STAB) · airframe 46,320 hrs · 30,105 cycles
THE LEFT INBOARD AFT ATTACH POINT MOUNTING PLATE FOR THE HORIZONTAL STABILIZER SHOWS SIGNS OF GALLING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 014-0003:5510-4001/006 00006 REWORKED HINGE PLATE FACES AND BORES IAW SRM 55-30-05 PARAGRAPH 7. SELECTED MAJOR REPAIR CLOSING REQUIREMENTS. (LP# 1278964)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,045 hrs · 29,247 cycles
DURING SVC CHECK FOUND LOWER AFT BULKHEAD EMERGENCY EXIT LIGHT INOP. FOUND EMERGENCY LIGHT BATTERY DEAD. R+R BTTERY PACK PER AMM 33-51. OPS CHECK GOOD. A/C OK FOR SVC. (LP# 5606332)
Part: DEFLECTOR — MISSING (RT MLG) · airframe 44,533 hrs · 28,923 cycles
RT MLG DEBRIS DEFLECTOR O/B MISSING. FWD TO MCO PER CDL 32-12-03. PLACARDS INSTALLED. REMOVED AND REPLACED RT MLG O/B SPRAY DEFLECTOR PER AMM 32-12. CDL AND PLACARD REMOVED. (LP # 4451198)
Earlier reports · 2009–2018 · 116 reports
2018
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,143 hrs · 28,684 cycles
CABIN EMER LIGHTS AT ROW 34 INOP. REMOVED & REPLACED BATTERY AT POWER SUPPLY B5-231. OPS CHECK GOOD. (LP# 3762934)
Part: SKIN — CRACKED (VERTICAL STAB) · airframe 44,152 hrs · 28,692 cycles
WHILE IN ATL FOR C-CHECK MTC REPORTED A CRACK COMMON TO THE V. STAB. RAM INLET SKIN. THE CRACK IS LOCATED AFT OF WHERE THE REMOVABLE SKIN ATTACHES. THE ER/A 00-563320 ASSOCIATED WITH THIS LOGPAGE AUTHORIZES A CUTOUT AND DOUBLER. (LP# 0300535, 0296632)
Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 44,143 hrs · 28,684 cycles
DOOR 1L & 1R EMER LIGHTS FLASH ON THEN OFF. REMOVED & REPLACED BATTERY AT POWER SUPPLY B5-211. OPS CHECK GOOD. (LP# 3762933)
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 43,252 hrs · 28,115 cycles
FWD GALLEY EMER. EXIT SIGN HAS SEVERAL INOP BULBS. RELAMPED FWD GALLEY EMER EXIT SIGN LIGHT BULBS PER AMM 33-51-18. OPS CHECKS GOOD.
2017
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,833 hrs · 27,257 cycles
L2 DOOR EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-241 PER MM. OPERATION CHECKS GOOD.
Part: SKIN — DAMAGED (BS 408) · airframe 41,758 hrs · 27,204 cycles
FUSELAGE FWD CARGO BELLY SKIN IS CREASED AT BS 408 BETWEEN LONGERONS 29 AND 30R AT THE FRAME SHEAR TIE. REPAIRED IAW ERA 563268-14, REV C.
Part: STRUCTURE — CORRODED (BS 900 & 904) · airframe 41,758 hrs · 27,204 cycles
CORROSION ON STRUCTURE BS 904 LBL 22 AND BS 900 LBL 21. REPAIRED IAW ERA 563304-14.LP# 0308510.
Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 40,625 hrs · 26,540 cycles
1/2 OF THE CEILING EMERGENCY LIGHTS REMAINED ILLUMINATED FOR ENTIRE FLIGHT. CYCLED EMERGENCY POWER SWITCH. OPERATION CHECKS NORMAL.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 39,696 hrs · 26,061 cycles
EMERGENCY CEILING LIGHTS ILLUMINATED WITH CABIN AND FLIGHT DECK SWITCH IN NORMAL POSITION. CYCLED EMERGENCY POWER SWITCH. OPS CHECKED GOOD.
Part: LIGHT — UNSECURE (ROW 26A) · airframe 39,577 hrs · 25,985 cycles
EMERGENCY LIGHT UNSECURE AT ROW 26A. SECURED THE LIGHT.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,500 hrs · 25,942 cycles
CABIN EMERGENCY CEILING LIGHTS INOPERATIVE AT ROW 33 LEFT AND RIGHT. REMOVED AND REPLACED BATTERY PACK.
2015
Part: SKIN — DAMAGED (BS 807) · airframe 36,580 hrs · 24,220 cycles
LIGHTNING STRIKE ON RT WINDOW BELT, BS 807. REMOVED AND REWORKED IAW SRM 53-30-03 AND 51-10-03. FOUND TO BE OUT OF LIMITS.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON LT BARREL NUT HOLE NR 10 AT HORIZONTAL STABILIZER. REPAIRED IAW ETI 90-15-108, REV 1 AND ERA 541540-14 REV O.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT BARREL NUT HOLE NR 15 AT HORIZONTAL STABILIZER. REPAIRED IAW ETI 90-15-108, REV 1 AND ERA 541540-14, REV.
Part: SPAR CAP — CORRODED (RT WING) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON INTERNAL DOUBLER AT RT WING FRONT SPAR LOWER CAP, XOS 257. REPAIRED IAW ETI 90-15-100, REV 2 AND ERA 539955-14, REV O.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON BARREL NUT HOLE NR 12, BS 7.2 LT SIDE AT HORIZONTAL STABILIZER. REPAIRED IAW ETI 90-15-107, REV 2 AND ERA 541538-14, REV O.
Part: CARGO TRACK — CORRODED (BS 1136-1307) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON LT CARGO TRACK FROM BS 1136 TO 1307, TASK 53-100-61. NEW CARGO TRACK INSTALLED IAW SRM 51-10-05, 51-30-02, 51-30-01 AND 51-10-03.
Part: RIB — CRACKED (LT WING) · airframe 36,580 hrs · 24,220 cycles
CRACK ON FORMER RIB, XOS=456, FIXED L/E INTERIOR SURFACE LEFT WING. REPAIRED FORMER RIB IAW ETI-90-15-112 AND SRM 51-30-05, 51-30-02, 51-10-03 AND ERA 541549-14, REV O.
Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON WEB AND STRAP BS 1269 DOOR JAMB AFT CARGO COMPARTMENT. REPAIRED IAW ERA 541577-14, REV O.
Part: FRAME — CORRODED (BS 1520) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON FRAME CLIP, BS 1520 CANT BETWEEN LONGERON 23L TO VENTRAL STAIRWAY DOORJAMB IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW ETI-90-15-116 AND SRM 51-30-05, ERA 541570-14, REV O.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 36,580 hrs · 24,220 cycles
CORROSION AT BORES INNER DIAMETER OF HORIZONTAL STABILIZER LT SIDE HINGE NR 1. REPAIRED IAW ETI-90-15-105, REV 1 AND ERA 541536-14, REV O.
Part: ACCESS PANEL — WORN (HORIZONTAL STAB) · airframe 36,580 hrs · 24,220 cycles
WEAR AT HOLE DIAMETER OF ACCESS PLATE-MID. REPAIRED HOLES IAW ETI 90-15-111, REV O AND ERA 541543-14, REV O.
Part: STRUCTURE — WORN (HORIZONTAL STAB) · airframe 36,580 hrs · 24,220 cycles
WEAR ON INNER BORES, 3 EA OF HORIZONTAL STABILIZER UPPER FORWARD ACCESS PLATE. REPAIRED IAW ETI 90-15-111, REV O AND ERA 541543-14, REV O.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620EB. NEW BUSHING WAS FABRICATED AND INSTALLED IAW SRM 57-00-04.
Part: INTERCOSTAL — CRACKED (SERVICE DOOR) · airframe 36,580 hrs · 24,220 cycles
CRACK ON LOWER INTERCOSTAL OF HYDRAULIC SERVICE PANEL AT LT WHEEL WELL JAMB. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5930584.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 620JB. REAMED HOLES, FABRICATED AND INSTALLED BUSHINGS IAW SRM 51-10-03.
Part: LONGERON — CRACKED (BS 1494) · airframe 36,580 hrs · 24,220 cycles
CRACK ON LONGERON 12L AND 4L, BS 1494 IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-01.
Part: CHANNEL — CRACKED (BS 120-148) · airframe 36,580 hrs · 24,220 cycles
CRACK ON CHANNEL OF FLOOR PANEL BETWEEN BS 120-148. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-02-04, 51-10-01, 53-20-03 AND 51-30-02.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON CONTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 620FT. BUSHING FABRICATED AND INSTALLED IAW SRM 57-00-01.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL 620FT. BUSHINGS WERE REPLACED IAW SRM 57-00-04 AND 51-10-03.
Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 36,580 hrs · 24,220 cycles
CRACK ON LT MLG INBD DOOR AFT CHANNEL BETWEEN BS 1044.8 - 1052.813. R & R CHANNEL IAW SRM 51-30-02.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL NR 520EB. FOUND TO BE OUT OF LIMITS. REPLACED FUEL PANEL IAW SRM 57-00-04.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 36,580 hrs · 24,220 cycles
CRACKS ON DORSAL FIN ATTACH INTERNAL ANGLES. R & R IAW SRM 51-30-05.
Part: INTERCOSTAL — CRACKED (BS 1046) · airframe 36,580 hrs · 24,220 cycles
CRACKS ON LOWER INTERCOSTAL, BS 1046 AT KEEL BEAM. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5936395, REV BF.
Part: CARGO TRACK — CORRODED (BS 1136-1212) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT CARGO TRACK BS 1136 TO 1212. R & R IAW SRM 53-20-01, 51-30-01, 51-30-02 AND 51-10-03.
Part: STIFFENER — CRACKED (BS 1556) · airframe 36,580 hrs · 24,220 cycles
CRACKED STIFFNER, BS 1556 CANT BETWEEN 7 HRS AND 8 HRS POSITIONS AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-10-03, FIG 17.
Part: BEAM — CORRODED (BS 1531-1542) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT BEAM OF VENTRAL STAIRWAY DOOR JAMB BS 1531 CANT TO 1542. X=-17.5. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL 520JB. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 620AT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: ACCESS PANEL — CORRODED (RT WING) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL ON RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACESS PANEL 620CT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: RUB STRIP — CORRODED (BS 790-883) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RUB STRIP AREAS AT BS 790-883 FROM LONGERON 26 TO 30 RT, BS 831, 827, 827.5, 832 AND 836 FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-30-01.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACESS PANEL 520AT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: SKIN — CORRODED (BS 521-836) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON FUSELAGE SKIN, RT RUB STRIP AREA, BS 521, 827, 827.5, 832 AND 836 FROM BS 2R - 30R. REPAIRED IAW SRM 53-30-01.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACESS PANEL 520FT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: WEB — WORN (BS 1435) · airframe 36,580 hrs · 24,220 cycles
WEAR ON WEB AND REPAIR FILLER AT BS 1435 BETWEEN LONGERONS 4LT AND 5LT. FABRICATED AND INSTALLED FILLER REPAIR IAW SRM 51-30-02, 53-00-01, 53-10-03 AND 51-10-03.
Part: RIB — CRACKED (LT WING) · airframe 36,580 hrs · 24,220 cycles
CRACKED RIB FORMER, FIXED L/E INTERIOR SURFACE, LT WING, XOS=450. REPLACED IAW SRM 51-30-02 AND 51-30-05.
Part: SPLICE — CRACKED (RT WING) · airframe 36,580 hrs · 24,220 cycles
CRACKED INTERNAL SPLICE AT RT WING L/E, XFS=196. REPLACED IAW SRM 57-30-01, 51-10-03, 51-30-02, 51-30-05.
Part: LONGERON — CRACKED (BS 1494) · airframe 36,580 hrs · 24,220 cycles
CRACK ON LONGERON 3L BS 1494. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 51-30-02, 51-10-05, 51-10-03, 53-10-01.
Part: SKIN — CRACKED (BS 1494) · airframe 36,580 hrs · 24,220 cycles
CRACKS ON FUSELAGE SKIN, BS 1494 BETWEEN LONGERON 2R. REPAIRED IAW ERA 539941-14, REV A.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 520CT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.
Part: STRUCTURE — WORN (CARGO DOOR) · airframe 36,580 hrs · 24,220 cycles
WEAR ON LOWER EDGE OF REPAIR FILLER AT FORWARD CARGO DOOR. REPAIR FILLER WAS REPLACED IAW SRM 51-30-01 AND 51-30-02.
Part: FLOORBEAM — CORRODED (BS 200) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON FLOOR SUPPORT AT BS 200, BETWEEN SEAT TRACKS X=-44 AND -54. REPLACED SUPPORT IAW SRM 51-30-02, 51-10-03, AND 51-30-05.
Part: CUSP WEB — CORRODED (BS 937) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT CUSP WEB, BS 937 BETWEEN X=-54 AND X=-60. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, 51-10-03 AND 51-30-02.
Part: SEAT TRACK — CORRODED (BS 200-260) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SEAT TRACK X=-22, BS 200-260. REPLACED IAW SRM 53-40-01.
Part: SKIN — DAMAGED (PAX DOOR) · airframe 36,580 hrs · 24,220 cycles
DAMAGE ON PREVIOUS REPAIR DOUBLE ON FORWARD ENTRY DOOR LOWER SURFACE, OUTER SKIN. REPLACED IAW SRM 51-30-02 AND 52-10-01.
Part: ANGLE — CRACKED (BS 1250) · airframe 36,580 hrs · 24,220 cycles
CRACKED T-SUPPORT AND CLIP ON LOWER ANGLE AND INTERCOSTAL, BS 1250 AT AFT CARGO DOOR. FORMER AND FITTING WERE REPLACED IAW SRM 51-30-02 AND 51-30-05.
Part: CUSP WEB — DAMAGED (BS 522-541) · airframe 36,580 hrs · 24,220 cycles
REWORK OUT OF LIMITS AT LT CUSP WEB, BS 522-541, X=-56 TO X=-60. REPAIRED IAW SRM 53-20-02, 51-30-02 AND 51-10-03.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREAS OF FUEL ACCESS PLANELS 620DT. REPLACED IAW SRM 57-00-04.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREAS OF FUEL PANEL, 520DT. REPLACED FUEL PANEL IAW 57-00-04.
Part: CUSP WEB — CORRODED (BS 560-579) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT CUPS WEB, BS 560-579 BETWEEN X=-54 TO X=-60. REPLACED IAW SRM 51-10-03, 53-20-02 AND 51-30-02.
Part: WEB — CRACKED (BS 207) · airframe 36,580 hrs · 24,220 cycles
CRACK ON WEB AT L1 DOOR JAMB, STA 207, LONGERON 15LH. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-60-02 AND 51-10-03.
Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON REPAIR SPACER LOWER DOOR JAMB BEAM OUTBOARD SURFACE AFT CARGO COMPARTMENT. TASK 53-123-02. INSTALLED NEW SPACER IAW SRM 53-60-02.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL PANEL 620GB. FOUND OUT OF LIMITS. REPLACED IAW SRM 57-00-04.
Part: CUSP WEB — CORRODED (BS 845-864) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE, BS 845-864, X=-54 AND X=-60. FABRICATED AND INSTALLED CUSP WEB IAW SRM 53-20-02, 51-30-02 AND 51-10-03.
Part: SEAT TRACK — DAMAGED (BS 735-738) · airframe 36,580 hrs · 24,220 cycles
REWORK OUT OF LIMITS ON RT SEAT TRACK X=-54 BETWEEN BS 735-738. NEW CHANEL WAS INSTALLED IAW SRM 51-30-03 AND 53-40-01.
Part: ANGLE — CRACKED (BS 1437) · airframe 36,580 hrs · 24,220 cycles
CRACK ON FRAME CLIP AT BS 1437 BETWEEN LONGERON 15 AND 16R AFT ACCESSORY. REMOVED FRAME CLIP. FABRICATED AND INSTALLED IAW SRM 51-30-05.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREAS OF FUEL ACCESS PANEL 620QB. REPLACED FUEL PANEL IAW SRM 57-00-04.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREAS OF FUEL ACCESS PANEL 520DB. REPLACED FUEL PANEL IAW SRM 57-00-04.
Part: CUSP WEB — CORRODED (BS 624-769) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT CUSP WEB BETWEEN X=54 AND X=60, BS 624 TO 769. REPLACED CUSP WEB IAW SRM 53-20-02 AND DWG 9940443, REV A.
Part: SEAT TRACK — CORRODED (BS 484-486) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON SEAT TRACK, BS 484-486, X=-54. TASK 53-211-02. NEW PLUG INSTALLED IAW SRM 53-40-01, 53-10-01, AND 51-30-01.
Part: CUSP WEB — CRACKED (BS 218) · airframe 36,580 hrs · 24,220 cycles
1" CRACK IN CUSP WEB LOWER SIDE AT BS 218 UNDER SEAT TRACK. CRACK WAS ATTENDED TO IAW SRM 53-20-02, FIG 24.
Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON COUNTERSINK AND SETTLEMENT AREAS OF FUEL ACCESS PANEL 520LB. REPLACED FUEL PANEL IAW SRM 57-00-04.
Part: INTERCOSTAL — CRACKED (BS 184) · airframe 36,580 hrs · 24,220 cycles
CRACK ON INTERCOSTAL APPROXIMATELY BS 184 BETWEEN BEAM NR 4 AND NR 5 AT FWD PASSENGER DOOR. REPLACED IAW SRM 51-30-02.
Part: CUSP WEB — CORRODED (BS 789-792) · airframe 36,580 hrs · 24,220 cycles
CORROSION ON RT CUSP WEB BS 789-792, BETWEEN X=-54 TO -60. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02 AND 51-30-02.
Part: ANGLE — WORN (CARGO DOOR) · airframe 36,580 hrs · 24,220 cycles
WEAR ON FORWARD/AFT ANGLES OF BAR LATCH AT AFT CARGO DOOR. REPLACED IAW SRM 51-30-01.
Part: PIN — DISENGAGED (DOOR SLIDE) · airframe 36,203 hrs · 23,989 cycles
FOUND FORWARD ENTRY DOOR SLIDE PACK PINS DISENGAGED. R & R FORWARD ENTRY DOOR SLIDE.
Part: PIN — MISSING (L1 DOOR SLIDE) · airframe 34,556 hrs · 22,996 cycles
L1 DOOR SLIDE PIN MISSING. R & R SLIDE ASSEMBLY.
Part: FUEL NOZZLE — LEAKING (APU) · airframe 34,308 hrs · 22,837 cycles
REPORTED AN ODOR/FUME EVENT. STRONG ODOR PRESENT IN FLIGHT DECK AND CABIN. F/A AND PASSENGERS COMPLAINED. NORMAL LANDING. NO EMERGENCY DECLARED. APU FUEL NOZZLE FOUND LEAKING. R & R APU. OPS CHECK OK. PERFORMED DUCT BURNOUT. REPLACED COALESCER BAGS.
2014
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,855 hrs · 21,905 cycles
MAIN ENTRANCE EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM. OPS CHECKED GOOD.
Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 31,734 hrs · 21,233 cycles
DURING SERVICE CHECK, EMERGENCY LIGHTS ILLUMINATE WITH POWER SURGE. R & R OVERWING EMERGENCY LIGHT POWER SUPPLY IAW AMM. OPS CHECKED GOOD.
Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 31,734 hrs · 21,233 cycles
DURING SERVICE CHECK, FOUND TAILCONE RELEASE CABLE FRAYED. R & R CABLE IAW AMM. RIGGED IAW AMM.
Part: FLOOR SUPPORT — CORRODED · airframe 31,734 hrs · 21,233 cycles
FOUND CORROSION ON FLOOR SUPPORT BETWEEN PANELS 221H AND 221JF/LF. INSTALLED NEW FLOOR SUPPORT IAW DWGS 3932140 AND SRM 51-30-01.
2013
Part: DOOR FRAME — CRACKED (LT MLG) · airframe 31,518 hrs · 21,120 cycles
LEFT MLG DOOR SURRROUND, CRACKED AT FORWARD ANGLE, JUST AFT OF HYD SERVICE PANEL. CRACK MEASURES APPROXIMATELY 3.25". R & R FRAME IAW SRM 51-00-01.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,494 hrs · 21,104 cycles
DURING SERVICE CHECK, FOUND CEILING EMERGENCY EXIT LIGHT AT ROW 26 INOPERATIVE. FOUND BROKEN WIRES. REPLACED IAW WDM AND CONNECTED. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,745 hrs · 20,637 cycles
AUXILARY EXIT LIGHTS INOPERATIVE AT BS 916. R & R EMERGENCY LIGHTS BATTERY PACK B5-105 IAW AMM. OPS CHECKED GOOD.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 30,368 hrs · 20,414 cycles
UPPER RT AFT HORIZONTAL STAB SKIN PANEL CRACKED. COMPLIED WITH ERA 516568-14AD, REV O.
Part: SKIN — CORRODED (BS 1475) · airframe 30,018 hrs · 20,210 cycles
FUSELAGE SKIN, BS 1475, L2L-L2R REPAIRED IAW ERA 500057-14.
Part: CABLE — FRAYED (GIRT BAR) · airframe 29,955 hrs · 20,175 cycles
DURING SERVICE CHECK, FOUND L1 DOOR GIRT BAR CABLE FRAYED. R & R L1 GIRT BAR CABLE IAW AMM.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,810 hrs · 20,096 cycles
EMERGENCY LIGHTS AND AREA LIGHT ABOVE R1 DOOR INOPERATIVE. REPLACED POWER SUPPLY IAW AMM 33-51-03. SYS TESTS OK.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,789 hrs · 20,087 cycles
ROW 36 EMERGENCY LIGHT IN OVERHEAD CEILING PANEL INOPERATIVE. R & R EMERGENCY POWER SUPPLY AND BATTERY. OPS CHECKED GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,789 hrs · 20,087 cycles
ROW 38, EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY. OPS CHECKED GOOD.
2012
Part: FASTENER — LOOSE (NR 1 PYLON) · airframe 26,683 hrs · 18,315 cycles
CW EA 02-476701-12AD INSPECTED PYLON SUPPORT FITTING FOR LOOSE OR MISSING FASTENERS. REMOVED & REPLACED FASTENERS IN ROW A PER OPN 0301 NR 1 PYLON.
Part: FASTENER — LOOSE (NR 2 PYLON) · airframe 26,683 hrs · 18,315 cycles
CW PYLON SUPPORT FITTING FASTENER INSPECTION FOR LOOSE, DAMAGE OR MISSING FASTENERS CONDITION PER EA02-476701-12AD.
Part: SUPPORT FITTING — NOT REPORTED (MLG) · airframe 26,683 hrs · 18,315 cycles
MLG ACTUATOR SUPPORT FITTING REPAIRED IAW AA 5740-01140.
Part: STOP FITTING — NOT REPORTED (CARGO DOOR) · airframe 26,683 hrs · 18,315 cycles
CARGO DOOR STOP PAD FITTINGS REPAIRED IAW AA 5230-01136.
Part: SPAR CAP — NOT REPORTED (VERTICAL STAB) · airframe 26,683 hrs · 18,315 cycles
VERTICAL STABILIZER, L/E FRONT SPAR CAP REPAIRED IAW AA5530-01044.
Part: SUPPORT FITTING — NOT REPORTED (PYLON) · airframe 26,683 hrs · 18,315 cycles
PYLON AFT SUPPORT FITTING UPPER FASTENERS REPAIRED IAW AA5440-01069.
Part: SPAR — CRACKED (WING) · airframe 26,683 hrs · 18,315 cycles
WING REAR SPAR CRACKED. REPAIRED IAW AA5710-01119.
Part: DOOR FRAME — NOT REPORTED (OVERWING EXIT) · airframe 26,683 hrs · 18,315 cycles
BS 883-962 OVERWNG FRAMES REPAIRED IAW AA 5310-01375.
Part: FITTING — NOT REPORTED (MLG) · airframe 26,683 hrs · 18,315 cycles
MLG - INSP/REPLACED RETRACT ACTUATOR SUPPORT FITTINGS. REPAIRED IAW EA 02-093855-03.
Part: MOTOR — NOT REPORTED (HYD SYS) · airframe 26,683 hrs · 18,315 cycles
HYDRAULIC ACMP MOTOR REPAIRED IAW AA 2920-01077.
Part: JACKSCREW — NOT REPORTED (HORIZONTAL STAB) · airframe 26,683 hrs · 18,315 cycles
HORIZONTAL STABILIZER, JACKSCREW ASSY REPAIRED IAW AA 2740-01071.
Part: STATIC PORT — NOT REPORTED · airframe 26,683 hrs · 18,315 cycles
STATIC PORT HEATING REPAIRED IAW AA 3032-01002.
Part: SKIN — NOT REPORTED (HORIZONTAL STAB) · airframe 26,683 hrs · 18,315 cycles
HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01085.
Part: LUG — NOT REPORTED (HORIZONTAL STAB) · airframe 26,683 hrs · 18,315 cycles
HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA5510-01083.
2011
Part: SKIN — UNKNOWN (FUSELAGE) · airframe 26,663 hrs · 18,308 cycles
REPLACE SKIN SECTION ON RT SIDE FUSELAGE STA 229-332 IAW SRM 53-30-01 VOL 1 REV 42.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,663 hrs · 18,308 cycles
FWD FLOORS: LT CENTER SEAT TRACK CORRODED BSTA 200-294 IAW SRM 53-40-01 FIG 4 SHEET 1 VOL 1 REV 42.
Part: INTERCOSTAL — DAMAGED (ENTRY DOOR) · airframe 26,663 hrs · 18,308 cycles
CRACK ON LOWER INTERCOSTAL FWD EDGE, INTERNAL STRUCTURE. REPAIR IAW DRAWING J060213 AND BOEING MESSAGE HLO-HLO-11-0019-07B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,663 hrs · 18,308 cycles
FWD FLOORS: LT INBOARD SEAT TRACK CORRODED BSTA 200-275. REPAIRED IAW SRM 53-40-01 FIG 6 SHEET 1 VOL 1 REV 42.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 26,663 hrs · 18,308 cycles
RT CABIN CUSPS: CUSP PANELS CRACKED BSTA 1344-134 LT SIDE WERE ENGINE WIRING IS LOCATED IAW SRM 53-20-02 SG09530019.
Part: SKIN — CRACKED (FUSELAGE) · airframe 26,663 hrs · 18,308 cycles
CRACKS ON SKINS AT BSTA 1475 BETWEEN L2LT 7 L2RT REPAIR IAW BOEING MESSAGE HLO HLO-11-0021 10B.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 26,663 hrs · 18,308 cycles
VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT BSTA 1542-1587. REPAIRED IAW TECHNICAL ORDER PAM-TO-51-10.
Part: SKIN — DENTED (FUSELAGE) · airframe 26,663 hrs · 18,308 cycles
DEPRESSION ON FUSELAGE WINDOW BELT AREA AT STA 229-294 L10-L16LT . LARGE DENT ON FUSELAGE.
2010
Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 26,679 hrs · 18,313 cycles
AFT CARGO DOOR FRAME BEAM, L28R, CORRODED. REPAIRED IAW ERA 398119-14.
2009
Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,076 hrs · 17,219 cycles
REPAIR SKIN AT STA 168.750 STR 26-27RT IS WRINKLED IAW SG09530002 AND BOEING MESSAGE NR 1-1253793814 AND TECHNICAL ORDER PAM-TO-51-02.