N865NN
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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.
111 reports on file, 2011-10-03 – 2026-08-18.
Part: FILTER — CONTAMINATED (ZONE 100) · airframe 46,495 hrs · 19,906 cycles
AIRCRAFT WAS GROUNDED: AIRCRAFT RETURN TO PHX DUE TO ODOR SMELL. NO EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE C/W J/C 08L00021001 AND R&R'ED HEPA FILTERS PER MOC AND TSI.
Part: STOP — UNSECURE (GIRT BAR) · airframe 45,437 hrs · 19,419 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS A WHITE PLASTIC STOP FELL OFF OF THE GIRT BAR AT AFT ENTRY DOOR. RESECURED AFT ENTRY GIRT BAR STOPPER. PER AMM 52-10-15.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 IAW 28-41-21
Part: FUEL — OUT OF BALANCE (NR 1 ENGINE) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. (OPEN).
Part: TRANSMITTER — FAULTED (ZONE 400) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12
Part: COMPENSATOR — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12, PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500 -) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12, PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. : REMOVEED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 PER 28-41-21,
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPUTER AND FUEL QUANTITY PROBES NUMBER 1 THRU 12, PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 , PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. **SUPPLEMENTAL REPORT FOR (AALA202601228764) SUBMITTED 01/22/2026 BY DFW: REMOVE AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 IAW 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12, PER 28-41-21.
Part: PROBE — FAULTED (ZONE 500) · airframe 44,687 hrs · 19,095 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT CRUISE NOTICED ENGINE #1 WAS IMBALANCED; EXPECTED FUEL AT DESTINATION WAS INDICATING 11K LBS AND WAS DROPPING FAST TO 10KLBS. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT PHX. VERIFIED LEFT HAND FUEL QUANTITY INOPERATIVE. REMOVED AND REPLACED NUMBER 1 ENGINE FUEL FLOW TRANSMITTER, PER AMM 73-31-01. ALSO, REMOVED AND REPLACED COMPENSATOR (AALA202603066245) AND FUEL QUANTITY PROBES NUMBER 1 THRU 12 PER 28-41-21.
Part: POWER PORT — INOPERATIVE (ZONE 200) · airframe 44,521 hrs · 19,025 cycles
AIRCRAFT WAS GROUNDED: FUMES REPORTED IN THE CABIN. DURING TROUBLESHOOTING FOUND (ISPS)-INSEAT POWER SUPPLY AT SEAT 15DEF INOP. REMOVED AND REPLACED ISPS AT SEAT 15DEF, PER AMM 23-81-05. OPERATIONAL CHECK GOOD. NO OTHER DEFECTS NOTED DURING TROUBLESHOOTING. NO ABNORMAL ODORS.
Earlier reports · 2011–2025 · 93 reports
2025
Part: SKIN — CORRODED (ZONE 100) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT WAS GROUNDED: CORROSION ON FUSELAGE SKIN AROUND AFT LAVATORY VENT LOCATED AT BS 917, BETWEEN S21L AND S22L. ACCOMPLISHED SKIN REPAIR PER EA 368982.
Part: FLAP — OUT OF ADJUST (GIRT BAR) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT IN BASE MAINTENANCE: R2 DOOR SLIDE GIRT BAR FLAP HANGING TO LOW. ADJUSTED R2 DOOR GIRT BAR FLAP. PER B737NG AMM 25-66-01-400.
Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER IN RIGHT HAND WHEEL WELL AT STA 663, RBL 50. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R-2.
Part: FUEL TANK — LEAKING (ZONE 100) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT IN BASE MAINTENANCE: FUEL CENTER TANK SHOWS LEAK FROM LEFT MIDDLE SIDE OF THE KEEL BEAM AREA. DESEALED, CLEANED AND RESEALED INTERNAL CENTER TANK AT FORWARD SIDE OF RIB 6. FROM LEFT WING RIB 1 TO RIGHT WING RIB 1. PERFORMED SATISFACTORY LEAK CHECK, NO LEAKS NOTED. PER B737 AMM 28-11-00.
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE, IN RIGHT HAND ECS BAY, AFT BULKHEAD, LOCATED AT BS 663, RBL 15. REPAIRED ANGLE PER SRM 57-10-10-2R-5.
Part: ROD — EXCESS PLAY (ZONE 500) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT WING, BETWEEN SPOILER NUMBER 5 AND 6, AFT OF AFT SPAR, INBOARD SIDE BOTH RODS HAVE EXCESSIVE PLAY. REMOVED AND REPLACED BEAM ASSEMBLY AT LEFT WING. PER B737NG SRM 51-40-02, SRM 51-40-05, SRM 51-20-01.
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 44,005 hrs · 18,795 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ECS BAY AFT BULKHEAD UPPER INBOARD CHORD CRACKED. REPAIRED RIGHT HAND ECS BAY AFT BULKHEAD UPPER INBOARD CHORD. PER B737 SRM 57-10-10-2R-5.
Part: FUEL CONTROL — LOW PRESSURE (ZONE 100) · airframe 43,680 hrs · 18,626 cycles
AIRCRAFT WAS NOT GROUNDED: DURING CLIMB AT FL 360 THE RIGHT FUEL TANK, FORWARD PUMP, "LOW PRESSURE" LIGHT ILLUMINATED. FUEL TANK QUANTITY WAS 8,600 LBS. REMOVE AND REPLACED TANK NUMBER 2 FORWARD FUEL BOOST PUMP. PER AMM 28-22-41. OPERATIONAL AND LEAK CHECKS GOOD.
Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 43,671 hrs · 18,619 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY DOOR DIFFICULT TO OPEN. READJUSTED AND LUBED LEFT AFT LAVATORY DOOR AND TRACKS. PER AMM 25-40-00.
Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 43,219 hrs · 18,403 cycles
AIRCRAFT WAS NOT GROUNDED: WHILE WORKING A-CHECK 024 JOB CARD 08C20025006 DVI EMERGANCY ESCAPE SLIDE AND PRESSURE BOTTLE, FOUND AFT RIGHT DOOR SLIDE INFLATION CYLINDER PRESSURE GAGE IN THE RED. REMOVE AND REPLACE R2 SLIDE.PER W/C 08L22125001.
Part: RADOME — DELAMINATED (ZONE 200) · airframe 43,049 hrs · 18,327 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: WEATHER RADAR ECHOES DOES NOT REFLECT ACCURATE WEATHER DEPICTION IN WINDSCREEN. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT DFW. PERFORMED WEATHER RADAR SYSTEM OPERATIONAL TEST AND BITE TEST, PER AMM 34-43-00. OPERTIONAL CHECK GOOD. NO ACTIVE FAULTS. PERFORMED NOSE RADOME MOISTURE INSPECTION, PER AMM 53-52-00. MOISTURE TEST FAILED MOISTURE LEVEL UNACCEPTABLE. DELAMINATION AND DAMAGE FOUND ON NOSE OF RADOME. MOISTURE TEST FAILED, MOISTURE LEVEL READS UNACCEPTABLE. REMOVED AND REPLACED RADOME. PER AMM 53-52-00.
2024
Part: HOLDER — BROKEN (ZONE 200) · airframe 40,846 hrs · 17,301 cycles
AIRCRAFT WAS NOT GROUNDED: EXIT LIGHT FIXTURE AT SEAT 28C LOOSE AND FALLING OFF. REPLACED EXIT LIGHT SHROUD AT SEAT 28C. OPERTIOBNAL CHECK GOOD. PER AMM 33-51-11.
2023
Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 38,709 hrs · 16,295 cycles
AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDAB RIGHT HAND INBOARD FLASHLIGHT DID NOT PASS TEST. MAINTENANCE REPLACED THE FLASHLIGHT BATTERIES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
Part: UNKNOWN — UNKNOWN (ZONE 900 - LAV/G) · airframe 38,701 hrs · 16,291 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS THE NUMBER 2 OVEN IN FIRST CLASS GALLEY, HAS A VERY STRONG ODOR OF BURNING PLASTIC, WHEN TURNED ON.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
Part: OVEN — CONTAMINATED (ZONE 900 - LAV/G) · airframe 38,701 hrs · 16,291 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS THE NUMBER 2 OVEN IN FIRST CLASS GALLEY, HAS A VERY STRONG ODOR OF BURNING PLASTIC, WHEN TURNED ON.**SUPPLEMENTAL REPORT FOR AALA202312131563: REPLACED NUMBER 2 OVEN PER AMM 25-32-03.**(CLOSED)
Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 38,545 hrs · 16,216 cycles
AIRCRAFT WAS NOT GROUNDED: L1 FLIGHT ATTENDANT FLASHLIGHT OUTBOARD POSITION IS INOPERATIVE. REPLACED BATTERY AND FUNCTIONAL CHECKED GOOD. PER AMM 25-64-00.
Part: FLASHLIGHT — NO TEST (ZONE 200 - FUSE) · airframe 38,330 hrs · 16,110 cycles
AIRCRAFT WAS NOT GROUNDED: AFT JUMPSEAT FLASHLIGHT NO TEST. REMOVED AND REPLACED AFT JUMPSEAT FLASHLIGHT. FUNCTIONAL CHECK GOOD. PER AMM 25-00-00.
Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 38,115 hrs · 16,001 cycles
AIRCRAFT WAS NOT GROUNDED: LAVATORY E DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED DOOR PER AMM 25-40-15.
Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 38,115 hrs · 16,001 cycles
AIRCRAFT WAS NOT GROUNDED: R4 LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED R4 LAVATORY DOOR HINGE, FUNCTIONAL CHECK GOOD.
Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 38,046 hrs · 15,975 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT AFT LEFT FLASHLIGHT INOPERATIVE. REMOVE AND REPLACE FLASHLIGHT BATTERY ON AFT LEFT FLIGHT ATTENDANT FLASHLIGHT PER AMM 25-64-00.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,747 hrs · 15,829 cycles
AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH TO CLT DUE TO LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED. USED ALTERNATE FLAPS TO EXTEND FLAPS TO 15. AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NO FAULTS. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS PER AMM 27-81-00.
2022
Part: BAFFLE — CRACKED (ZONE 100 - FUSE) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT RIGHT HAND BAFFLE LOCATED FROM BS 500G TO 500H AND RBL 25. REPLACED BAFFLE PER SRM 51-40-02, AARD 51-00-05-1 AND DWG 143A7505.
Part: BAFFLE — CRACKED (ZONE 200 - FUSE) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT RIGHT HAND BAFFLE LOCATED FROM BS 500F TO 500G AND RBL 25. REPLACED BAFFLE PER SRM 51-40-02, AARD 51-00-05-1, AND DWG 143A7505.
Part: ANGLE — CRACKED (ZONE 200 - FUSE) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR ANGLE LOCATED AT BS 394 AND LBL 13. REPLACED ANGLE PER AARD 51-00-05-1.
Part: INTERCOSTAL — CRACKED (ZONE 200 - FUSE) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FORWARD ENTRY AREA FLOORBOARD SUPPORT INTERCOSTAL LOCATED FROM BS 312 TO BS 328 AT LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05, SRM 51-00-05, AND DWG 141A5400.
Part: FLOOR SUPPORT — CRACKED (BS 328-344 LBL45) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD PASSENGER CABIN LEFT HAND INTERCOSTAL LOCATED FROM BS 328 TO BS 344 AT LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05-1 AND DWG 141A5400.
Part: PANEL — CRACKED (ZONE 200 - FUSE) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BREAK PANEL LOCATED AT BS 540 AND LBL 0. REPLACED BREAK PANEL PER SRM 51-40-02.
Part: PANEL — CRACKED (ZONE 200 - FUSE) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BREAK PANEL LOCATED AT BS 540 AND RBL 0. REPLACED BREAK PANEL PER SRM 51-40-02.
Part: ANGLE — CORRODED (BS 500A-500G) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE. RIGHT TRANSITION ANGLE HAD CORROSION, BS 500A-500G+9, RBL 24. INSTALLED A NEW ANGLE.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER RIB LOCATED AT STABILIZER STA 92.70. REPLACED RIB PER AARD 51-00-05-01 AND DWG 182A5301.
Part: FLOORBEAM — CORRODED (BS 986 RBL 43) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR BEAM LOCATED AT BS 986.5 AND RBL 43. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6 ALTERNATIVE 4.
Part: FLOORBEAM — CORRODED (BS 986 LBL43) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR BEAM LOCATED AT BS 986.5 AND LBL 43. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6 ALTERNATIVE 3 AND EA 341078.
Part: TRANSITION PANEL — CORRODED (BS 490-500G S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT TRANSITION PANEL HAS CORROSION LOCATED AT STA 490 AND 500G+9 AND STR 25L. REMOVED AND REPLACED TRANSITION PANEL.
Part: FLOOR SUPPORT — CORRODED (BS 957 LBL 48) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN LEFT HAND FLOOR SUPPORT INTERCOSTAL LOCATED AT BS 957 LBL 48. REPLACED INTERCOSTAL PER AARD 51-00-05-1 AND DWG 147A5650.
Part: TRANSITION PANEL — CORRODED (BS 727J-747) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 727J TO BS 747 AT S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727D S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727D AND S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727C S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727C AND S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727J-727I) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 727J TO BS 727I AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 767-807 S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 767 TO BS 807 AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: SHIELD — CORRODED (BS 767-787) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON CARGO SHIELD LOCATED BETWEEN STA 767 AND 787 AND RIGHT BUTT LINE 25. REMOVED AND REPLACED AFT CARGO SHIELD PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727B S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT TRANSITION PANEL LOCATED AT BS 727B AND S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-
Part: WEB — CORRODED (BS 787-847 S25R) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON THRESHOLD WEB. LOCATED AT BS 787+6 TO 847 AND STR 25. INSTALLED NEW WEB PER SRM 51-40-02.
Part: TRANSITION PANEL — CORRODED (BS 727H-727I) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 727H TO BS 727I AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727G-727F) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 727G TO BS 727F AT S25R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727B S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727B AND S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: WEB — CORRODED (BS 460 S26R) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO DOOR SILL LOCATED AT STA 460 AND STR 26R. REMOVED AND REPLACED CARGO DOOR SILL WEB PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 727E-727F) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 727E TO BS 727F AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: TRANSITION PANEL — CORRODED (BS 747-767 S25L) · corrosion level 2 · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 767 TO BS 747 AT S25L. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 8 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 101.90, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 157.10, 8 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 184.70, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 8 INCHES FROM FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 8 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 16 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 16 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
Part: SKIN — CORRODED (BS 540 RBL 53.2) · airframe 36,037 hrs · 15,030 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WING CENTER SECTION FORWARD RIGHT LOWER SKIN LOCATED AT BS 540 AN RBL 53.2. REPAIRED SKIN PER EA 341176A.
Part: LATCH — STICKING (ZONE 800 - DOORS) · airframe 33,363 hrs · 13,763 cycles
AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR LOCK DIFFICULT TO OPERATE. LUBED DOOR LATCH PER CMM 25-40-64.
Part: SCREW — LOOSE (ZONE 800 - DOORS) · airframe 33,286 hrs · 13,724 cycles
AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR STICKS. TIGHTEN HINGE SCREWS ON FIRST CLASS LAVATORY DOOR PER AMM 25-46-96.
2021
Part: WINDOW — DELAMINATED (COCKPIT L1) · airframe 32,307 hrs · 13,284 cycles
AIRCRAFT WAS GROUNDED: L1 WINDOW DELAMINATING NEAR CENTER POST. REPLACED L1 WINDOW WITH SERVICEABLE UNIT IAW WORKCARD 08L21056003.
2020
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 30,307 hrs · 12,403 cycles
AIRCRAFT NOT GROUNDED. R1 DOOR EXIT LIGHT COVER LOOSE. REPLACED MISSING HARDWARE IN EXIT LIGHT COVER, AMM 33-51-00. OPERATIONAL CHECK NORMAL, OKAY FOR SERVICE.
Part: OVEN — ODOR (GALLEY) · airframe 29,058 hrs · 11,873 cycles
AIRCRAFT WAS NOT GROUNDED: FIRST CLASS GALLEY OVEN #2 HAS AN ELECTRICAL ODOR. **SUPPLEMENTAL ACTION SECT 4 AND 5: REPLACED #2 F/C OVEN REF AMM 25-32-03.***(CLOSED)
2019
Part: UNKNOWN — FIRE (ENGINE) · airframe 26,076 hrs · 10,491 cycles
ADVANCING THRUST FOR TAKEOFF, A REPORT WAS RECEIVED FROM ANOTHER AIRCRAFT THAT FLAMES WERE OBSERVED FROM TAILPIPE AND SIDE OF ENGINE. ENGINE INDICATIONS WERE NORMAL. AFTER EXITING RUNWAY AND SECURING THE ENGINE, FIRE CHIEF REPORTED NO INDICATION OF FIRE OR SMOKE. ACCOMPLISHED FIM 71-05-00-810-811-F00. FOUND THE ENGINE TO BE ACCEPTABLE FOR CONTINUED SERVICE. THE AIRCRAFT WAS GROUNDED.
Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 25,832 hrs · 10,368 cycles
OVERWING EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-06.
2018
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 25,511 hrs · 10,231 cycles
LEFT OVERWING EXIT BATTERY PACK FAILED A CAPACITY CHECK. REPLACED THE BATTERY PACK IAW AMM 33-51-06.
Part: COVER — MISSING (DOOR HANDLE) · airframe 23,492 hrs · 9,353 cycles
ROW 15F OVERWING EMERGENCY EXIT HANDLE COVER MISSING. REPLACED THE EMERGENCY EXIT HANDLE.
2017
Part: SIGN — UNSECURE (CABIN) · airframe 21,722 hrs · 8,569 cycles
THE AIRCRAFT WAS NOT GROUNDED. LENS FELL OFF OF EXIT IDENTIFIER LIGHT AT LEFT AFT GALLEY DOOR. REPLACED LIGHT L01190 PER AMM 33-51-02.
Part: ACTUATOR — FAULTY (LT MLG) · airframe 21,265 hrs · 8,378 cycles
THE AIRCRAFT WAS GROUNDED. ON APPROACH, LEFT MAIN GEAR WOULD NOT EXTEND. THE FLIGHT PERFORMED A GO-AROUND AND ACCOMPLISHED MANUAL GEAR EXTENSION CHECKLIST. AN EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT GEAR MAIN UPLOCK ACTUATOR IAW 32-32-41-40. ALL OPS CHECK AND GROUND CHECKS NORMAL. (SEE ALSO SDR AALA20170609044)
Part: SELECTOR VALVE — FAULTY (COCKPIT) · airframe 21,265 hrs · 8,378 cycles
THE AIRCRAFT WAS GROUNDED. ON APPROACH, LEFT MAIN GEAR WOULD NOT EXTEND. THE FLIGHT PERFORMED A GO-AROUND AND ACCOMPLISHED MANUAL GEAR EXTENSION CHECKLIST. AN EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW 32-31-51-401. ALL OPS CHECK AND GROUND CHECKS NORMAL. (SEE ALSO SDR AALA201706089038)
Part: ACTUATOR — FAULTY (LEFT MLG) · airframe 21,163 hrs · 8,334 cycles
ON GEAR EXTENSION, LT MAIN LANDING GEAR REMAINED RED AND LEFT GEAR LIGHT ON UPPER PANEL WAS OFF. DURING GO AROUND, AND LEAVING GEAR DOWN, THE LEFT GREEN LIGHT CAME ON WHEN APPLYING SOME POSITIVE G-FORCE. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOWLOCK ACTUATOR IAW AMM 32-32-51. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,143 hrs · 8,328 cycles
AFTER GEAR EXTENSION LEFT MAIN GEAR LIGHT REMAINED RED. AFTER CYCLING GEAR WAS ABLE TO GET GREEN LIGHT BOTH ON FORWARD ) UPPER PANELS. ACCOMPLISHED PSEU BITE TEST IAW AMM TASK 32-09-10-740-801, OPS CKS OK. IAW FIM 32-09-00-810-801 VISUALLY INSPECTED ALL PROX SWITCHES, MLG, AND WHEEL WELLS, NO DEFECTS NOTED. THE AIRCRAFT WAS GROUNDED.
Part: SIGN — UNSECURE (CABIN) · airframe 20,778 hrs · 8,180 cycles
R1 DOOR FA REPLACED EMERGENCY SIGN FELL OFF FWD GALLEY ON TAKE OFF, REPORTED JUST BEFORE LANDING. REMOVED AND REPLACED FWD GALLEY EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-01 OPS CK GOOD. THE AIRCRAFT WAS NOT GROUNDED.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 20,617 hrs · 8,117 cycles
LEFT LAV IN AFT SMOKE ALARM GOING OFF. ACCOMPLISHED TASK 26-14-00 ALL CHECK GOOD OK FOR SERVICE. THE AIRCRAFT WAS NOT GROUNDED.
Part: LENS — MISSING (CABIN) · airframe 20,367 hrs · 8,018 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BY R1 DOOR HAS A MISSING LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,122 hrs · 7,910 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT AFT RIGHT INBOARD SIDE OF CABIN IS FLASHING RED. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
2016
Part: WIRE — EXPOSED (ESCAPE SLIDE) · airframe 19,592 hrs · 7,703 cycles
L2 EMERGENCY EVACUATION SLIDE HAS A TEST LEAD WIRE EXPOSED. RESTOWED WIRE IAW CMM 25-60-37. OPERATIONAL CHECK GOOD.
Part: SKIN — CORRODED (BS 1016) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
FUSELAGE SKIN AT BS 1016 BETWEEN S21 - 22L IS CORRODED IN PREVIOUSLY BLENDED AREA. REPAIRED THE SKIN IAW SRM 51-10-01 FIGURE 2 DETAIL A AND EA 265041.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO COMPARTMENT RIGHT TRANSITION ANGLE IS CORRODED BETWEEN FUSELAGE STATIONS 500H AND 500I. REMOVED AND REPLACED TRANSITION ANGLE BETWEEN STATIONS 500G AND 500I IAW SRM 53-00-53-2R.
Part: ANGLE — CORRODED (BS 500H-500I) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
FORWARD CARGO BAY LEFT TRANSITION ANGLE IS CORRODED BETWEEN BS 500H AND 500I. REPAIRED TRANSITION ANGLE IAW SRM 53-00-53-2R.
Part: FLOOR SUPPORT — CRACKED (BS 500H-500I) · airframe 19,524 hrs · 7,676 cycles
FORWARD CARGO BAY LEFT FLOOR SUPPORT AT LBL 25 BETWEEN BS 500H AND 500I IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
Part: ANGLE — CORRODED (BS 767-787) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
AFT CARGO BAY RIGHT TRANSITION ANGLE IS CORRODED BETWEEN BS 767 AND 787. REMOVED AND REPLACED THE TRANSITION ANGLE IAW 51-00-05-1 AND DRAWING 146A0081.
Part: RAIL — CORRODED (BS 500I) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
FORWARD CARGO BAY AFT BULKHEAD LOWER RAIL AT BS 500I IS CORRODED BETWEEN LBL 25 AND RBL 25. REMOVED AND REPLACED LOWER RAIL IAW SRM 51-10-02 AND BOEING DRAWING 143A9485.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO COMPARTMENT RIGHT TRANSITION ANGLE IS CORRODED AT FUSELAGE STATIONS 727J AND 767. REMOVED AND REPLACED TRANSITION ANGLE BETWEEN STATIONS 727J AND 767 IAW SRM 53-00-53-2R.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,524 hrs · 7,676 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. INTERCOSTAL AT RBL 31 IS CORRODED AT FUSELAGE STATION 991. REMOVED AND REPLACED INTERCOSTAL IAW AARD 51-00-05-1 AND DRAWING 147A5710.
2015
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,280 hrs · 6,385 cycles
LEFT & RIGHT AFT EMER LIGHTING BATTERY PACKS FAILED DURING MCM 2903 CARD. R & R LT & RT AFT EMER LIGHTING BATTERY PACKS IAW AMM 33-51-06, OPERATIONALLY CHECKED OK.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 13,439 hrs · 5,271 cycles
DURING SIC 2904 EMER LIGHT INSPECTION CHECK, DISCOVERED ROW 11 DEF & 21 DEF AISLE MARKER NOT ILLUMINATING. ROW 11 DEF & 21 DEF LOOSE CONNECTION, RECONNECTED. OPERATIONS CHECKED OK.
2014
Part: PUMP — FAILED (HYD SYSTEM) · airframe 13,330 hrs · 5,233 cycles
INBOUND, RT ENGINE HYD PUMP FAILED THEN LOST HYD SYSTEM B. EMERGENCY DECLARED & LANDING UNEVENTFUL. REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-11. SYSTEM CHECKED NORMAL.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,902 hrs · 5,053 cycles
FUSELAGE SIN HAS CORROSION AROUND LAVATORY VENT PORT AT STATION 917 BETWEEN STRINGERS 21 & 22 LT. REMOVED CORROSION & REPAIRED IAW ENGINEERING AUTHORIZATION B737-53-037298 DATED 6 NOV 2014.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,902 hrs · 5,053 cycles
FUSELAGE SKIN HAS SMALL AREAS OF CORROSION BETWEEN STATIONS 967 & 988 FROM STRINGERS 21 TO 22 LT. REMOVED CORROSION & REPAIRED IAW ENGINEERING AUTHORIZATION B737-53-037297 & SUPPLEMENT 037297 DATED 11/6/2014.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,902 hrs · 5,053 cycles
FUSELAGE SKIN HAS AREA OF CORROSION BETWEEN STATIONS 1004 & 1007 FROM STRINGER 21 TO 22 LT. REMOVED CORROSION & REPAIRED IAW ENGINEERING AUTHORIZATION B737-53-037297 & SUPPLEMENT 037297 DATED 11/6/2014.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,902 hrs · 5,053 cycles
FUSELAGE SKIN HAS AREAS OF CORROSION BETWEEN STATIONS 1014 & 1017 FROM STRINGERS 19 TO 23 LT. REMOVED CORROSION & REPAIRED IAW ENGINEERING AUTHORIZATION B737-53-037297 & SUPPLEMENT 037297 DATED 11/6/2014.
2012
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,157 hrs · 2,435 cycles
AFT LAVATORY VENT CORROSION FROM STATIONS 888 TO 907 AND STRINGERS 24 TO 25 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-027040.
2011
Part: LENS — MISSING (CABNI) · airframe 2,607 hrs · 971 cycles
RED EMERGENCY LIGHT LENS AT SEAT 14D MISSING. REPLACED RED LENS FOR EMERGENCY LIGHT AT SEAT 14D. OPS CHECK NORMAL.