N844NN
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.
101 reports on file, 2011-07-25 – 2026-08-26.
Part: HYDRAULIC LINE — LEAKING (ZONE 700) · airframe 48,296 hrs · 20,671 cycles
AIRCRAFT WAS GROUNDED: HYD SYSTEM B FALED UPON STOPPING AIRCRAFT. COMPLETE LOSS OF HYDRAULIC FLUID. DECESION MADE TO RETURN TO PHX. EMERGENCY DECLARED AND AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO GATE. TROUBLE SHOOTING REVEALED R/H MLG RETRACT / EXTENSION ACTUATOR PRESS LINE RUPTURED. MAINTENANCE REPLACED R/H MLG EXT/RET ACTUATOR PRESSURE AND RETURN LINES PER AMM 32-32-11. REPLENISHED A & B HYD SYS'S 12GALLONS OF SKYDROL. CHECKED AND CYCLED FLIGHT CONTROLS INCLUDING FLAPS AND T/R'S AND ACTUATED LANDING GEAR FOR BLEED OUT OF SYSTEMS. LEAK CHECK'S GOOD.
Part: FILTER — LEAKING (ZONE 100) · airframe 48,181 hrs · 20,615 cycles
AIRCRAFT WAS GROUNDED: IN CRUISE HYD B PRESSURE DROPPED TO ZERO. DROPPED FROM 20 TO 10% IN 10 MINUTES. ZERO SHORTLY THERE AFTER. ALTERED BY DELLOIACONO 437809 STA DFW 12 AUG 26 AFTER SPEAKING WITH INBOUND CAPT. QTY WENT TO ZERO. MIC NUMBER 7 574321 "IN CRUISE HYD B PRESSURE DROPPED TO ZERO. DROPPED FROM 20% TO 10% IN 10 MINUTES". POST FLIGHT WALK AROUND SHOWED HYDRAULIC FLUID FROM THE WHEEL WELL TO THE APU. LARGE QUANTITY OF FLUID IN WHEEL WELL. FLUID ON NUMBER 2 TIRE. MISTIFIED HYDRAULIC FLUID ALSO PRESENT IN WHEEL WELL. MAINTENANCE FOUND RH WHEEL WELL ACOUSTIC FILTER LEAKING. REPLACED ACOUSTIC FILTER. ALL DONE IAW MM 29-11-27.
Part: STRINGER — CORRODED (ZONE 100) · airframe 47,584 hrs · 20,325 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER 25L AT STA 351.2. REPAIRED STRINGER PER EA 373444.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 46,764 hrs · 19,957 cycles
AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANTS RIGHT SIDE AISLE FLASHLIGHT REQUIRES MAINTENANCE. REMOVED AND REPLACED RIGHT INBOARD (AALA202602194409) FLIGHT ATTENDANTS SEAT FLASHLIGHT AND LEFT INBOARD (AALA202602190696) FLIGHT ATTENDANTS SEAT FLASHLIGHTS. PER DBF2000. OPS CHECK GOOD.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 46,764 hrs · 19,957 cycles
AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANTS RIGHT SIDE AISLE FLASHLIGHT REQUIRES MAINTENANCE. REMOVED AND REPLACED RIGHT INBOARD (AALA202602194409) FLIGHT ATTENDANTS SEAT FLASHLIGHT AND LEFT INBOARD (AALA202602190696) FLIGHT ATTENDANTS SEAT FLASHLIGHTS. PER DBF2000. OPS CHECK GOOD.
Part: AIR DUCT — BLOWN (ZONE 100) · airframe 46,492 hrs · 19,830 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING DECENT AT ALTITUDE 16000 FEET ON DECENT CABIN ALTITUDE WARNING LIGHT AND HORN SOUNDED. AIRCRAFT EMERGENCY LANDED SAFELY AT ABQ. FOUND BLOWN DUCK IN THE RIGHT PACK. REMOVED AND REPLACED BLOWN DUCT FROM ACM. ENGINE RUN AND LEAK CHECK NO LEAK FOUND. PER AMM 21-51-04.
Earlier reports · 2011–2025 · 95 reports
2025
Part: PRESSURE SWITCH — FAULTY (ZONE 100) · airframe 46,296 hrs · 19,749 cycles
AIRCRAFT WAS NOT GROUNDED: THE RIGHT AFT FUEL PUMP LOW PRESSURE LIGHT DOES NOT ILLUMINATE WHEN SWITCH IS TURNED OFF. REMOVED AND REPLACED RIGHT AFT PRESSURE SWITCH. PER AMM 28-42-11. OPS CHECKED GOOD, NO LEAKS NOTED.
Part: PRESSURE SWITCH — FAULTED (ZONE 100) · airframe 46,242 hrs · 19,725 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT FUEL PUMP LOW PRESSURE LIGHT DOES NOT ILLUMINATE WITH PUMP TURNED OFF. INSPECTED AND CLEANED RIGHT HAND AFT FUEL BOOST PUMP PRESSURE SWITCH ELECTRICAL CONNECTOR, OPS TESTED GOOD IAW AMM 28-42-11.
Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,249 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WHEEL WELL CUT OUT SEAL RETAINER AT BS 727, RBL 39. REMOVED, FABRICATED, AND INSTALLED WHEEL WELL CUT OUT SEAL RETAINER PER SRM 51-40-02-0G.
Part: RETAINER — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,249 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WHEEL WELL CUT OUT AFT SEAL RETAINER AT BS 727, RBL 57. REMOVED, FABRICATED, AND INSTALLED WHEEL WELL CUT OUT SEAL RETAINER PER SRM 51-40-02-0G.
Part: SKIN — WORN (ZONE 100) · airframe 44,249 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE OF FUSELAGE SKIN AT EXTERNAL POWER PANEL ACCESS DOOR TORN FROM STA 225 TO STA 235, S24R. REPAIRED SKIN PER SRM 53-10-15-2R-4.
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,249 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND WHEEL WELL CUT OUT WEB HAS CORROSION AT BS 667, RBL 57. REPAIRED PER SRM 51-40-02-0G.
Part: SKIN PANEL — WORN (ZONE 400) · airframe 44,250 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: WEAR MARKS ALONG THE RIGHT WING FIXED LEADING EDGE UPPER SKIN PANEL UPPER SURFACE, JUST INBOARD OF ENGINE STRUT. REMOVED AND INSTALLED NEW RIGHT WING FIXED LEADING EDGE SKIN PANEL. PER B737NG SRM 51-40-02.
Part: PANEL — EXCESS PLAY (ZONE 600) · airframe 44,250 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING LOWER TRANSLATE PANEL JUST INBOARD OF PYLON INBOARD FORWARD SUPPORT ROD HAS PLAY AT LOWER ATTACH POINT TO PANEL. REMOVED AND INSTALLED NEW SUPPORT ROD SUPPORT BEAM AT RIGHT HAND WING LOWER TRANSLATE PANEL JUST INBOARD OF PYLON. PER B737 NG SRM 51-40-02.
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 44,250 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT LEFT HAND SIDEWALL PANEL ATTACH ANGLE HAS CRACKED AT LOWER ATTACH CLIP AT BS 867. REMOVED AND REPLACED LOWER ATTACH CLIP AT AFT CARGO COMPARTMENT LEFT HAND SIDE WALL PANEL. PER B737, SRM51-40-02.
Part: SUPPORT ANGLE — EXCESS PLAY (ZONE 600) · airframe 44,250 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING LOWER TRANSLATE PANEL JUST INBOARD OF PYLON MIDDLE AFT SUPPORT ROD HAS PLAY AT LOWER ATTACH POINT TO PANEL. REMOVED AND INSTALLED NEW ANGLE SUPPORT BEAM AT RIGHT HAND WING LOWER TEPANEL JUST INBOARD OF PYLON MIDDLE AFT SUPPORT ROD AT LOWER ATTACH POINT TO PANEL. PER B737NG SRM 51-40-02.
Part: SKIN — TORN (ZONE 100) · airframe 44,250 hrs · 18,741 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE OF FUSELAGE EXTERNAL POWER PANEL ACCESS DOOR CUTOUT HAS TORN SKIN AT LOWER EDGE. REPAIRED AREA AT RIGHT HAND SIDE OF FUSELAGE EXTERNAL POWER PANEL ACCESS DOOR CUTOUT. PER B737-NG SRM 53-10-15-2R PROCEDURE 4 REPAIR 4.
2024
Part: THRUST REVERSER — WARNING MESSAGE (NR 2) · airframe 43,491 hrs · 18,413 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 2 THRUST REVERSE INDICATION ILLUMINATED, HAD TO SHUT DOWN ENGINE NUMBER 2; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT CLT. (OPEN).
Part: ACTUATOR — LEAKING (ZONE 400) · airframe 43,491 hrs · 18,413 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 2 THRUST REVERSE INDICATION ILLUMINATED, HAD TO SHUT DOWN ENGINE NUMBER 2; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT CLT. **SUPPLEMENTAL REPORT FOR (AALA202412029889): REMOVED AND REPLACED THE OUTBOARD UPPER HYDRAULIC ACTUATOR ON THE NUMBER 2 ENGINE THRUST REVERSER. PER J/C 08L40078005. OPERTIONAL CHECKS GOOD, LEAK CHECKS GOOD**(CLOSED).
Part: SIGN — DISLODGED (CABIN) · airframe 41,746 hrs · 17,555 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN FOUND ON THE FLOOR BY EXIT ROW. REATTACHED EMERGENCY EXIT SIGN COVER TO RIGHT HAND LOWER AFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, VERIFIED SYSTEM WORKING PROPERLY. PER AMM33-51-00.
Part: PRESSURE SWITCH — FAULTY (ZONE 600 - RH WI) · airframe 40,870 hrs · 17,143 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT FUEL LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT, AIRCRAFT WAS IN LEVEL FLIGHT. REMOVE AND REPLACED RIGHT AFT BOOST PUMP PRESSURE SWITCH. PER AMM 24-42-11. OPERATIONAL CHECK GOOD.
2023
Part: DOOR — STUCK (ZONE 200 - FUSE) · airframe 39,443 hrs · 16,461 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR STUCK. REMOVED LINT AND LUBRICATED DOOR PER FIM 52-50-00
2022
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: VERTICAL PRESSURE DECK IN RIGHT WHEEL WELL HAS A CRACK INDICATION LOCATED AT STA 663.75 BETWEEN RIGHT BUTT LINE 31.83 AND 40.00. REPAIRED WITH DOUBLER PER SRM 57-10-10-2R.
Part: VAPOR BARRIER — CRACKED (ZONE 100 - FUSE) · airframe 36,588 hrs · 15,081 cycles
AIRCRAFT IN BASE MAINTENANCE: AREA OUTBOARD OF RIGHT AC BAY - VERTICAL CRACK IN VAPOR BARRIER ALONG RIVET LINE INBOARD OF HYDRAULIC SYSTEM B SERVICE DISCONNECT MODULE. INSTALLED REPAIR AT STA 663 RIGHT BUTT LINE 52 PER AARD 57-10-10-9.
Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT TRANSITION PANEL HAS AREA OF CORROSION LOCATED AT 500E AND LEFT BUTT LINE 25. REMOVED AND REPLACED LEFT TRANSITION PANEL PER SRM 51-10-02.
Part: ANGLE — CRACKED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK IN UPPER AFT CORNER ANGLE LOCATED IN RIGHT HAND AIR CONDITIONING BAY, BS 663, RBL 64. REPAIRED ANGLE PER ARM 57-10-10-2R PROCEDURE 5.
Part: INTERCOSTAL — CRACKED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON INTERCOSTAL LOCATED AT STA 321 AND WATERLINE 49. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: INTERCOSTAL — CRACKED (ZONE 200 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON INTERCOSTAL NEAR DOORWAY LOCATED AT STA 323 AND WATERLINE 17I. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: WEB — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON WEB LOCATED AT STATION 986 AND RIGHT BUTT LINE 33 AND TOP OF K-WEB. INSTALLED NEW PART PER AARD 51-00-05-1.
Part: BRAKE ASSY — BROKEN (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR STRUCTURE ABOVE WING BOX AND FLOOR BOX ATTACHMENT BRACKET AT STA 540 AND BUTT LINE 0 TO LEFT BUTT LINE 24 IS BROKEN AT IN BOARD END FORWARD END AFT FLANGES. REMOVED AND REPLACED FLOOR SUPPORT BRAKE ASSEMBLY PER AARD 51-00-05-1.
Part: SKIN — CRACKED (ZONE 300 - STABS) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER HAS CRACK ON LOWER SKIN. LOCATED AT STA 184.70 AND LEFT BUTT LINE 175. DOUBLER REPAIR INSTALLED IN THE RIB LOWER LEG AT THE DAMAGE CUTOUT HOLE PER SRM AND EA 337755.
Part: BRAKE ASSY — CRACKED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR STRUCTURE ABOVE WING BOX. FLOOR BOARD ATTACHMENT BRACKET AT STA 540, AND BUTT LINE 0 TO RIGHT BUTT LINE 24 IS BENT CRACKED AND BROKEN AT INBOARD FASTENER HOLES.
Part: SKIN — CRACKED (ZONE 300 - STABS) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN CRACKED LOCATED AT STABILIZER STA 129.50, 9 INCHES FROM AFT SPAR. REPAIRED PER SRM 55-10-01-2R-11.
Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON LEFT TRANSITION PANEL LOCATED AT STA 500D AND LEFT BUTT LINE 25. REMOVED AND REPLACED LEFT TRANSITION PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 727A TO BS 727B AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 747 TO BS 767 AND RBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727E AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED AT BS 727I AND RBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 767 TO BS 787 AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 727A TO BS 727B AND RBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON LEFT TRANSITION PANEL LOCATED AT STA 500F AND LEFT BUTT LINE 25. REMOVED AND REPLACED LEFT TRANSITION PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED FROM BS 787 TO BS 807 AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727F AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: RAIL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FLOOR SUPPORT RAIL ASSEMBLY LOCATED AT BS 360 AND LBL 25. REPLACED LOWER RAIL ASSEMBLY PER BOEING DWG 143A9481 AND SRM 51-40-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED AT BS 727J AND RBL 25. REPAIRED PANEL PER SRM 51-10
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727I AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON LEFT TRANSITION PANEL LOCATED AT STA 500B AND LEFT BUTT LINE 25. REMOVED AND REPLACED LEFT TRANSITION PANEL PER SRM 51-10-02.
Part: STRINGER — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER S23L, LOCATED FROM BS 310 - BS 343. REPAIRED PER EA 337877.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727C AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED AT BS 727E AND RBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727G AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 500C, LBL 25. REPLACED TRANSITION PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED AT BS 727H AND LBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 100 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED AT BS 767 AND RBL 25. REPAIRED PANEL PER SRM 51-10-02.
Part: NONE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND CREASE ANGLE LOCATED FROM BS 986 TO BS 993 AT RBL 52. REPLACED CREASE ANGLE PER AARD 51-00-05-01.
Part: INTERCOSTAL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON INTERCOSTAL LOCATED AT STA 319 AND WATERLINE 57. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-00-05-1.
Part: SUPPORT ANGLE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON SUPPORT ANGLE LOCATED AT STA 304 AND STR 56. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.
Part: SUPPORT — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBOARD SUPPORT LOCATED FROM BS 947 TO BS 967, LBL 24. REPLACED SUPPORT PER BOEING DWG 147A5650 AND AARD 51-00-05-1**SUPPLEMENTAL REPORT FOR AALA202208026444: CORROSION LEVEL CHANGED TO LEVEL 2** (CLOSED)
Part: NONE — CORRODED (ZONE 200 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN 1L DOOR FORWARD GIRT BAR FLOOR MOUNT STRUCTURE, LOCATED AT STA 312 AND LBL 54. REPLACED GIRT BAR TIEDOWN PER AARD 51-00-05.
Part: FLOORBEAM — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR BEAM LOCATED AT BS 947.5 AND RBL 50. REPAIRED PER 53-70-51-2R-5.
Part: ANGLE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z-ANGLE FLANGE, LOCATED AT BS 990 AND RBL 34. REPLACED ANGLE PER AARD 51-00-05-1 AND DWG 147A5710.
Part: SUPPORT — CORRODED (ZONE 200 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBOARD SUPPORT LOCATED FROM BS 947 TO BS 967, LBL 24. REPLACED SUPPORT PER BOEING DWG 147A5650 AND AARD 51-00-05-1
Part: SUPPORT — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBOARD SUPPORT LOCATED FROM BS 947 TO BS 967, LBL 50. REPLACED SUPPORT PER AARD 51-00-05-1 AND BOWING DWG 147A5660.**SUPPLEMENTAL REPORT FOR AALA202208027553: CORROSION LEVEL CHANGED TO LEVEL 2** (CLOSED)
Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO DOOR LOWER SILL PLATE LOCATED FROM BS 455 TO BS 485, AT RBL 28. REPLACED SILL PLATE PER SRM 51-40-02, AARD51-00-05 AND BOEING DWG 143A8122.
Part: SUPPORT — CORRODED (ZONE 200 - FUSE) · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBOARD SUPPORT LOCATED FROM BS 947 TO BS 967, LBL 50. REPLACED SUPPORT PER AARD 51-00-05-1 AND BOWING DWG 147A5660.
Part: NONE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN 1L DOOR AFT GIRT BAR FLOOR MOUNT STRUCTURE, LOCATED AT STA 344 AND LBL 57. REPLACED GIRT BAR TIEDOWN PER AARD 51-00-05.
Part: NONE — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN 1L DOOR FORWARD GIRT BAR FLOOR MOUNT STRUCTURE, LOCATED AT STA 312 AND LBL 54. REPLACED GIRT BAR TIEDOWN PER AARD 51-00-05.**SUPPLEMENTAL REPORT FOR AALA202207296247: CORROSION LEVEL CHANGED FROM LEVEL 1 TO LEVEL 2.**(CLOSED)
Part: FLOORBEAM — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER COMPARTMENT FLOOR BEAM LOCATED AT BS 986 AND LBL 48. REPAIRED PER SRM 53-70-51-2R.
Part: FLOORBEAM — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LAVATORY MOUNT FLOORBEAM LOCATED FROM STA 927 TO STA 947 AND RBL 50. REPAIRED PER SRM 53-70-51-2R-5.
Part: FLOORBEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,288 hrs · 15,080 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FLOOR BEAM LOCATED AT STA 986 AND RIGHT BUTT LINE 48 NUT PLATE HOLE. INSTALLED A NESTED ANGLE FILLER REPAIR PER SRM 53-70-51-2R-6.
Part: THRESHOLD — STICKING (ZONE 800 - DOORS) · airframe 36,276 hrs · 14,926 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. RESECURED RIGHT AFT LAVATORY DOOR THRESHOLD PER CMM BE AEROSPACE 25-40-65.
Part: VALVE — INOPERATIVE (ZONE 700 - GEARS) · airframe 36,209 hrs · 14,898 cycles
AIRCRAFT WAS GROUNDED: ANTI SKID INOPERATIVE LIGHT ILLUMINATED MULTIPLE TIMES AFTER LIFTOFF. AIRCRAFT DIVERTED TO IAD DUE TO WET RUNWAYS AT DCA. REMOVED AND REPLACED ANTI-SKID VALVE PER JOB CARD 08L70032008.
Part: LIFE RAFT — LOW PRESSURE (ZONE 200 - FUSE) · airframe 35,595 hrs · 14,639 cycles
AIRCRAFT WAS NOT GROUNDED: AFT PASSENGER CABIN OVERHEAD COMPARTMENT LIFE RAFT PRESSURE LOW. REPLACED LIFT RAFT PER AMM 25-64-00.
2021
Part: WINDOW — DELAMINATED (R1) · airframe 33,168 hrs · 13,544 cycles
AIRCRAFT WAS GROUNDED: L1 WINDOW DELAMINATING AT UPPER RIGHT CORNER. R1 WINDOW DELAMINATING AT UPPER LEFT CORNER. L1 WINDOW REPLACED WITH SERVICEABLE UNIT (AALA202104229009) IAW WORKCARD 08C21156001 AND R1 WINDOW REPLACED WITH SERVICEABLE UNIT IAW WORKCARD 08C21256001, LEAK AND OPS CHECK GOOD.
Part: WINDOW — DELAMINATED (L1) · airframe 33,168 hrs · 13,544 cycles
AIRCRAFT WAS GROUNDED: L1 WINDOW DELAMINATING AT UPPER RIGHT CORNER. R1 WINDOW DELAMINATING AT UPPER LEFT CORNER. **SUPPLEMENTAL REPORT: L1 WINDOW REPLACED WITH SERVICEABLE UNIT IAW WORKCARD 08C21156001 AND R1 WINDOW REPLACED WITH SERVICEABLE UNIT (AALA202104229010) IAW WORKCARD 08C21256001, LEAK AND OPS CHECK GOOD.
2019
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,904 hrs · 11,673 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS ON CLIMBOUT, PASSING 10,000 FT, CABIN ALTITUDE WARNING LIGHT ILLUMINATED AND HORN WENT OFF. PF LEVELLED AIRCRAFT AT 10,000 FT. PNF RAN QRH TO COMPLETION, REGAINING PRESSURIZATION CONTROL IN MANUAL MODE. MAINTENANCE PERFORMED BITE TEST ON DCPC 1 AND 2 IAW FIM 21-31-00-810-801. NO FAULTS NOTED. TEST OKAY.
2018
Part: PITOT TUBE — DEFECTIVE (PITOT/STATIC SYS) · airframe 27,444 hrs · 11,013 cycles
AIRCRAFT WAS GROUNDED: FIRST OFFICER INSTRUMENT CLUSTER UNRELIABLE. EMERGENCY DECLARED INTO DFW. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PITOT TUBE PER AMM 34-11-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: PITOT TUBE — DEFECTIVE (FIRST OFFICER'S) · airframe 27,444 hrs · 11,013 cycles
AIRSPEED UNRELIABLE, FIRST OFFICER`S SIDE IN ICEING CONDITIONS. AIRSPEED OFF BY 150 KTS, ALTITUDE OFF 1800. THE AIRCRAFT WAS GROUNDED. FOUND FIRST OFFICER`S PITOT TUBE NOT HEATING. REPLACED FOS PITOT TUBE IAW AMM 34-11-01, CHECKED OK, LEAK CHECKED OK IAW AMM 34-11-00.
Part: LEVER — OUT OF POSITION · airframe 26,385 hrs · 10,546 cycles
CAPTAIN`S SLIDING WINDOW HOLD OPEN LOCK SPRING BROKEN. FOUND CAPTAIN SLIDING WINDOW HOLD LEVER OUT OF GROVE ON LEVER. REPOSITIONED THE HOLD ON LEVER SPRING ON LEVER GROVE IAW SRM 51-40-02. OPS CHECKED GOOD AND LOCK HOLDS IN POSITION. NO FURTHER ACTION REQUIRED. THE AIRCRAFT WAS GROUNDED.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,187 hrs · 10,472 cycles
THE AIRCRAFT WAS NOT GROUNDED. NR 1 FLIGHT ATTENDANT FLASHLIGHT OUT OF HOLDER AND INOPERATIVE. REPLACED NR 1 FLIGHT ATTENDANT FLASHLIGHT BATTERY PER AMM 25-64-00. OPERATIONS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,077 hrs · 10,431 cycles
AIRCRAFT WAS GROUNDED: REGARDLESS OF SWITCH POSITION, EMERGENCY EXIT LIGHTS ON AIRCRAFT LEFT WERE ON INTERMITTENT. MAINTENANCE REPLACED BATTERY PACK EQ M1670 AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-06.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,974 hrs · 9,970 cycles
EXIT LIGHT ON GALLEY WALL ADJACENT TO THE LEFT AFT ENTRY DOOR HAS A MISSING LENS. REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-01. OK FOR SERVICE.
2017
Part: LENS — BROKEN (EXIT SIGN) · airframe 24,330 hrs · 9,685 cycles
LENS BROKEN OFF THE EXIT SIGN AT ROW 14A SIDEWALL. REPLACED THE LENS IAW AMM 33-51-01.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 24,044 hrs · 9,554 cycles
FLIGHT ATTENDANT FLASHLIGHT AT THE FORWARD JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 22,278 hrs · 8,817 cycles
EMERGENCY EXIT LIGHT IN THE LEFT AFT CABIN HAS A DETACHED LENS COVER. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-04. OPS CHECKED GOOD.
Part: LENS — DETACHED (CABIN) · airframe 21,894 hrs · 8,662 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ON SIDE WALL NEAR FIRST CLASS GALLEY HAS A DETACHED LENS COVER. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-14. OPERATIONAL CHECK GOOD.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 21,719 hrs · 8,591 cycles
R2 DOOR SLIDE BALL IS NOT PROPERLY ENGAGED. REMOVED AND REINSTALLED THE SLIDE. OPERATIONAL CHECKED GOOD.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 21,719 hrs · 8,591 cycles
R1 DOOR SLIDE BALL IS NOT PROPERLY ENGAGED. REMOVED AND REINSTALLED THE SLIDE. OPERATIONAL CHECKED GOOD.
2016
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,188 hrs · 8,382 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT NEAR FIRST CLASS GALLEY IS MISSING LENS COVER. REPLACED THE LENS COVER IAW AMM 33-51-14. OPERATIONAL CHECKED GOOD.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,395 hrs · 7,665 cycles
AFT CARGO COMPARTMENT RT TRANSITION ANGLE IS CORRODED BETWEEN FS 787 AND FS 800. R & R TRANSITION ANGLE SECTION IAW SRM 51-10-02-0G.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 19,395 hrs · 7,665 cycles
MAIN CABIN FLOOR INTERCOSTAL APPROX 20 INCHES INBD OF THE FWD ENTRY DOOR IS CRACKED AT FS 338. R & R INTERCOSTAL IAW AARD 51-00-058-1.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,395 hrs · 7,665 cycles
AIRCRAFT WAS IN BASE MX. CABIN FLOOR INTERCOSTAL LOCATED APPROX 30 INCHES INBD OF THE FWD SERVICE DOOR, JAMB IS CRACKED AT APPROX FS 310. R & R INTERCOSTAL IAW AARD 51-00-05-1.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 19,395 hrs · 7,665 cycles
MAIN CABIN FLOOR INTERCOSTAL AT LBL 12 IS CRACKED AT FS 355. R & R INTERCOSTAL IAW AARD 51-00-05-1.
Part: LENS — MISSING (CABIN) · airframe 18,778 hrs · 7,404 cycles
AIRCRAFT WAS NOT GNDED. EMERGENCY LIGHT LENS FOUND MISSING DURING A CHECK INSPECTION. REPLACED MISSING LENS.
2015
Part: INDICATION SYS — UNKNOWN (FUEL SYSTEM) · airframe 15,180 hrs · 5,969 cycles
EMERGENCY DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RT TANK FUEL QTY INDICATES AS MUCH AS 900 POUNDS LESS THAN LT TANK QTY. DIFFERENCE FLUCTUATED BETWEEN 400 & 900 POUNDS. TRIM INDICATED NO IMBALANCE & MX CONFIRMED. REPORTED FUEL QTY WORKED PROPERLY, NO IMBALANCE. NO FURTHER ACTION TAKEN.
2014
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,633 hrs · 4,972 cycles
STATIONS 927 TO 947 & STRINGERS 21 TO 22 LT, SKIN AROUND MULTIPLE FASTERS SHOW EVIDENCE OF CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA 737-53-035119.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,633 hrs · 4,972 cycles
STATIONS 947 TO 967 & STRINGER 22 LT, SKIN AROUND MULTIPLE FASTENERS SHOW EVIDENCE OF CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA 737-53-035119.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,633 hrs · 4,972 cycles
STATIONS 967 TO 987 & STRINGER 22 LT, SKIN AROUND MULTIPLE FASTENERS SHOW EVIDENCE OF CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA 737-53-035119.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,633 hrs · 4,972 cycles
STATIONS 907 TO 927 & STRINGERS 22 TO 23 LT, SKIN AROUND MULTIPLE FASTENERS SHOW EVIDENCE OF CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA 737-53-035119.
2012
Part: SKIN — PUNCTURED (FUSELAGE) · airframe 6,417 hrs · 2,488 cycles
PUNCTURE DAMAGE ON THE FUSELAGE SKIN LEFT SIDE BETWEEN STATIONS 235 AND 243 BELOW WATERLINE 190. INSTALLED DOUBLER PER SRM 53-00-00-01-2R 3.
2011
Part: DISPLAY — FAILED (COCKPIT) · airframe 3,486 hrs · 1,285 cycles
ORD - INFLIGHT IAD-LAX. CREW REPORTED INTEGRATED STANDBY FLIGHT DISPLAY FAILED IN FLIGHT. FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. REPLACED INTEGRATED STANDBY FLIGHT DISPLAY. SYSTEM GROUND CHECK NORMAL OPERATION.