N907NN
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2026-03-01 – 2026-03-01 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2026-03-01 – 2026-03-01 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT WAS NOT GROUNDED: AFT GALLEY EXIT LIGHT BROKEN. REPLACED AFT GALLEY RIGHT EXIT LIGHT.
AIRCRAFT WAS NOT GROUNDED: AFT GALLEY EXIT LIGHT BROKEN. REPLACED AFT GALLEY RIGHT EXIT LIGHT.
AIRCRAFT WAS NOT GROUNDED: ROW 27F EMERGENCY LIGHT IS OUT OF THE FITTING. VERIFIED LIGHT SECURED AT SEAT 27 ABC AND OPERATION CHECK GOOD. PER AMM 33-50-00.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT APPROXIMATELY FL 310 IN CLIMB, ENGINE NR 2 FAILED AFTER SEVERE VIBRATIONS AND COMPRESSORS STALL. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SAL.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT APPROXIMATELY FL 310 IN CLIMB, ENGINE NR 2 FAILED AFTER SEVERE VIBRATIONS AND COMPRESSORS STALL. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SAL. (OPEN).
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT APPROXIMATELY FL 310 IN CLIMB, ENGINE NUMBER 2 FAILED AFTER SEVERE VIBRATIONS AND COMPRESSORS STALL. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SAL. ACCOMPLISHED AMM 71-00-00-210-801-F00 AND FIM 71-05-00-810-805-F00. FOUND FAULTY HMU. REPLACED HMU PER J/C 08L40073001. ALL BORESCOPE LEAK AND OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 2 ENGINE FAILURE AT APPROXIMATELY 28,000 FEET, EGT RED LINE WITH TEMP 987 AND ENGINE FAILURE ANNUNCIATION, POST FLIGHT INSPECTION FOUND EXHAUST TURBINE IN PIECES. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SAL. REMOVED AND REPLACED NUMBER 2 ENGINE, PER J/C 08L40072003.OPS CHECK AND LEAK GOOD, PER J/C 08L40072006**(CLOSED).
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NR 2 ENGINE FAILURE AT APPROXIMATELY 28,000 FEET, EGT RED LINE WITH TEMP 987 AND ENGINE FAILURE ANNUNCIATION, POST FLIGHT INSPECTION FOUND EXHAUST TURBINE IN PIECES. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SAL. OPEN
AIRCRAFT WAS NOT GROUNDED: AUTO BRAKE DISARM LIGHT ILLUMINATES DURING PREFLIGHT WHEN SWITCH SELECTED TO RTO, THIS IS A REPEAT ITEM. **SUPPLEMENTAL REPORT FOR (AALA202503132003): REPLACED RIGHT HAND (ATSP)-AUTO THROTTLE SWITCH PACK ASSEMBLY, OPERTIONAL CHECK GOOD. PER J/C 08L11276002 FOR ALL SIGNATURES AND WORK ACCOMPLISHED**(CLOSED).
AIRCRAFT WAS NOT GROUNDED: AUTO BRAKE DISARM LIGHT ILLUMINATES DURING PREFLIGHT WHEN SWITCH SELECTED TO RTO, THIS IS A REPEAT ITEM. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED AFT SERVICE DOOR GIRT BAR HARD TO OPERATE. LEFT WITH TOO MUCH GREASE TO OPERATE SAFELY. VERIFIED AFT RIGHT EMERGENCY DOOR GRIT BAR RETAINER CLIPS ARE ABNORMALLY TIGHT. BENT RETAINER CLIPS TO THE RIGHT DIMENSIONS.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: DURING APPROACH AUTO THROTTLE MOVEMENT WAS NOT SYMMETRICAL WITH NUMBER 2 THRUST LEVER LEADING NUMBER 1 BY ONE KNOB LENGTH. AT GLIDESLOPE INTERCEPT NUMBER 2 THRUST LEVER ADVANCED TOWARD GO AROUND THRUST WITH NUMBER 1 THROTTLE LAGGING BY APPROXIMATELY 5 KNOB LENGTHS; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. REPLACED FLIGHT CONTROL COMPUTER-A. PER MM 22-11-33 AND ACCOMPLISHED DFCS TEST PER MM 23-11-00, OPERTIONAL CHECK NORMAL.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING CLIMB WE HAD A VERY STRONG BURNING SMELL. PLASTIC OR ELECTRICAL; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. ACCOMPLISHED W/C 08L00021001 AND NO ODOR FOUND, NO FAULT FOUND.
AIRCRAFT WAS NOT GROUNDED: AFT GALLEY FLASHLIGHT BLINKING RED. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT IN AFT FLIGHT ATTENDENT JUMPSEAT STOWAGE COMPARTMENT. OPERTIONAL CHECK GOOD. PER AMM 25-64-00.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL ANGLE FROM STA 380 TO STA 400, LBL 13. REPLACED ANGLE PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES IN AFT PASSENGER CABIN GALLEY FLOOR STRUCTURE Z ANGLE AT STA 993, FROM RBL 37 TO RBL 43. REPLACED ANGLE PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, LBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 320 TO STA 344, LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500B TO STA 500I, S25L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, RBL 53. REPAIRED CHORD PER SRM 53-70-51-2R-5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 948, RBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION SHIELD FROM STA 767 TO STA 787, S25R. REPLACED TRANSITION SHIELD PER AARD 51-00-05-1A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727 PLUS 4 INCHES TO 727B PLUS 7 INCHES, S25R. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R-5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 947, FROM LBL 13 TO RBL 13. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-70-51-2R-8.
AIRCRAFT WAS GROUNDED: FOUND GOUGE AFT OF RIGHT HAND AFT SERVICE DOOR BETWEEN BS 1000 TO 1016 AND STR 11R TO 12R. ACCOMPLISHED PERMINENT SKIN REPAIR. NO FURTHER DAMAGE NOTED. PER AARD 11-20-00.
AIRCRAFT WAS NOT GROUNDED: FIRST CLASS GALLEY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FLIGHT ATTANDENT FLASHLIGHT IN THE FIRST CLASS GALLEY. OPERTIONAL CHECK GOOD. PER AMM 25-64-00.
AIRCRAFT WAS NOT GROUNDED: LAVATORY-D ENTRY DOOR DIFFICULT TO OPEN OR CLOSE. SECURED DOOR SEAL BEARING, OPERTIONAL CHECK GOOD. PER AMM 25-40-14.
AIRCRAFT WAS NOT GROUNDED: ROW 8ABC EXIT LIGHTING HANGING FROM BOTTOM OF SEAT. RE-INSTALLED AND SECURED LIGHT COVER CAP ON ROW 8ABC. PER AMM 33-51-11.
AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN. REPOSITIONED AFT LEFT LAVATORY DOOR. PER AMM 25-40-00.
AIRCRAFT WAS NOT GROUNDED: FORWARD SERVICE DOOR IS DIFFICULT TO ARM. GIRT BAR IS HAVING TROUBLE TO SLIDE INTO PLACE. FOUND 'Z' FOLD NOT IN CORRECT R1 DOOR FRONT SIDE. RESTABLISHED 'Z' FOLD IN GIRT.
AIRCRAFT WAS NOT GROUNDED: 1R DOOR SLIDE IS FALLING OUT OF ITS HOLDER. MAINTENANCE REMOVED, ADJUSTED, REINSTALL SLIDE PACK I.A.W. AMM 25-66-01.
AIRCRAFT WAS NOT GROUNDED: LAVATORY-D VERY DIFFICULT TO LOCK AND UNLOCK.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT WAS NOT GROUNDED: 17A WINDOW SHADE CRUMPLED. **SUPPLEMENTAL REPORT FOR AALA202308014434: REPLACED WINDOW SHADE PER AMM 25-21-12.** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: 17A WINDOW SHADE CRUMPLED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
AIRCRAFT WAS NOT GROUNDED: AFT LEFT DOOR SLIDE IS VERY LOOSE. SECURED SLIDE MOUNTING SCREW PER AMM 25-66-00.
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE IS LOOSE AND DIFFICULT TO OPEN. TIGHTENED SCREW ON FORWARD LAVATORY HANDLE. OPERATES NORMAL.
AIRCRAFT WAS NOT GROUNDED: SLIDE 4L EMERGENCY EQUIPMENT AND FLAPS ARE HANGING OUT NOT SECURE. RE-SECURED SAFETY POUCH AT DOOR 4L PER AMM 25-66-01.
AIRCRAFT WAS GROUNDED: CLIMBING THROUGH 22,000 FEET WITH ENGINE ANTI ICE ON, NUMBER 1 ENGINE LOST THRUST AND EXHIBITED EXCESSIVE VIBRATION. REDUCED THRUST BUT COULD NOT ACHIEVE MORE THAN 40% WITHOUT VIBRATION SO SHUT ENGINE DOWN. EMERGENCY WAS DECLARED AND AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED LEFT ENGINE PER JOBCARD 08L40072003.
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE IS LOOSE. RESECURED DOOR HANDLE PER AMM 20-50-11.
AIRCRAFT IN BASE MAINTENANCE: R1 DOOR GIRT BAR ARM FLAG TOO SHORT. ADJUSTED R1 DOOR GIRT BAR ARM FLAG PER B737 NG AMM 25-66-00-840-801.
AIRCRAFT WAS NOT GROUNDED: FORWARD CARGO SMOKE DETECTOR M2240 FAILS BUILT IN TEST EQUIPMENT CHECK. REMOVED AND REPLACED CARGO SMOKE DETECTOR M2240, OPERATIONS TEST CHECKS GOOD PER B737NG AMM 26-16-01 & 26-16-00.
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT ASSEMBLY INSTALLED INCORRECTLY AT ROW 17. ADJUSTED EXIT LIGHT ASSEMBLY IAW BOEING 737NG AMM 33-51-01, OPS CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED: INFO TO MAINTENANCE ABORTED TAKE OFF TUL. TAKE OFF CONFIGURATION HORN AND LIGHT APPROXIMATELY 60 KNOTS CONSULTED QUICK REFERENCE HANDBOOK. RECYCLED FLAPS AND STABILIZERS TRIM SPOILERS, 2ND TAKE OFF ATTEMPT NORMAL.
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY LOCK DIFFICULT TO OPERATE. LUBRICATED DOOR LATCH.
AIRCRAFT WAS GROUNDED: AT APPROXIMATELY 10,000 FEET ENGINE 2 OVERHEAT LIGHT ILLUMINATED. ENGINE 1 FIRE LIGHT AND ENGINE 1 OVERHEAT DOES NOT TEST. RETURNED TO FIELD. REPLACED CHAFED HARNESS MW0325 (AALA202106189013) PER AMM 26-11-02 AND AMM 26-10-01. REPLACED ENGINE AND APU FIRE AND OVERHEAT DETECTION CONTROL MODULE (AALA202106219002) PER AMM 26-10-01.
AIRCRAFT WAS GROUNDED: AT APPROXIMATELY 10,000 FEET ENGINE 2 OVERHEAT LIGHT ILLUMINATED. ENGINE 1 FIRE LIGHT AND ENGINE 1 OVERHEAT DOES NOT TEST. RETURNED TO FIELD. **SUPPLEMENTAL REPORT: REPLACED CHAFED HARNESS MW0325 (AALA202106189013) PER AMM 26-11-02 AND AMM 26-10-01. REPLACED ENGINE AND APU FIRE AND OVERHEAT DETECTION CONTROL MODULE (AALA202106219002) PER AMM 26-10-01.
AIRCRAFT WAS GROUNDED: ENGINE 2 OVERHEAT INDICATION CLIMBING OUT OF 12000 MSL. REPLACED ENGINE 2 FIRE DETECTION HARNESS MW0326 PER AMM 26-11-00-710-801.
AIRCRAFT WAS NOT GROUNDED: ONE CABIN MEGAPHONE INOPERATIVE. REPLACED BATTERIES PER AMM 25-64-00.
AIRCRAFT WAS NOT GROUNDED: CLOSET DOOR HARD TO OPEN BY 1L DOOR. ADJUSTED LATCH MECHANISM ON CLOSET DOOR BY L1 ENTRY DOOR AS REQUIRED
AIRCRAFT WAS NOT GROUNDED. DOOR 1R INDICATION STRAP MISSING. AIRCRAFT DISPATCHED ON MEL 25-61A. REPLACED R1 DOOR ORANGE STRAP VISUAL INDICATOR, IAW AMM 52-11-31.
AIRCRAFT WAS GROUNDED: LEFT WING INBOARD AFT FLAP TRAILING EDGE DELAMINATED 29 INCHES OUT BOARD OF THE INBOARD END. REPAIRED FLAP PER EA 297024.
RIGHT WHEEL WELL BULKHEAD WEB, AT BS 663 WAS CRACKED. REPAIRED THE BULKHEAD WEB IAW 57-10-10-9, AND SRM 57-10-10-2R2.
CORROSION ON FORWARD CARGO BA7 LEFT TRANSITION PANEL BETWEEN BS 500B AND 500I. REPLACED THE TRANSITION PANEL IAW SRM 53-00-532-2R5.
CORROSION ON FORWARD CARGO COMPARTMENT RIGHT TRANSISTION PANEL, BETWEEN BS 500A AND 500I. REPLACED TRANSITION PANEL IAW SRM 53-00-53-2R5.
CRACKED CABIN FLOOR SUPPORT AT BS 540 AND RBL 2. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
CRACKED CABIN FLOOR SUPPORT AT BS 540 AND LBL 2. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
CORROSION FOUND ON THE AFT CARGO RIGHT TRANSITION PANEL BETWEEN BS 747 AND 767. REPLACED THE TRANSISTION PANEL IAW SRM 53-00-53-2R, AND 51-00-05-1.
CORROSION FOUND ON THE AFT CARGO, LEFT TRANSITION PANEL BETWEEN BS 727G AND 727H. REPLACED THE TRANSITION PANEL IAW 51-00-05-1, AND SRM 53-00-53-2R-5.
CRACKED FLOOR SUPPORT BETWEEN BS 344 -360, LBL 11. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
CRACKED FLOOR SUPPORT BETWEEN BS 312 AND 328, RBL 30. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
CRACKED CABIN FLOOR SUPPORT BETWEEN BS 312 TO 328, LBL 42. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.
AISLE EMERGENCY LIGHT LENS AT ROW 8 ABC IS DAMAGED. REPLACED THE LENS IAW AMM 33-21-03.
EXIT SIGN MISSING, AFT OF PASSNEGER DOOR NEXT TO TRASH CAN IN GALLEY RIGHT OF GALLEY DOOR. REPLACED THE EXIT SIGN AND LENS IAW 33-51-01.
AIRCRAFT WAS NOT GROUNDED: INTERMITTENT LAVATORY SMOKE MASTER CAUTION ON SIX PACK OVERHEAD LIGHTS IN CRUISE FLIGHT. MAINTENANCE ACCOMPLISHED LAVATORY SMOKE DETECTOR SYSTEM TEST PER AMM 26-14-00 ON ALL LAVATORIES. NO FAULTS NOTED AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AFT RIGHT EXIT DOOR EXIT SIGN IS MISSING. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-01.
AIRCRAFT WAS NOT GROUNDED. LAVATORY SMOKE LIGHT ILLUMINATED DURING CRUISE WITH NO KNOWN ISSUES, FLIGHT ATTENDANTS FOUND NO SMOKE OR HEAT IN LAVATORIES. SELF TESTED LAVATORY SMOKE DETECTORS PER AMM 26-14-00. UNABLE TO DUPLICATE FAULT. OPERATIONAL CHECK GOOD.
THE AIRCRAFT WAS NOT GROUNDED. LAVATORY SMOKE LIGHTS AND CHIME ON 2.5 HOURS INTO CRUISE. FLIGHT ATTENDANTS REPORTED NO FIRE OR SMOKE FROM LAVATORY L4, (AFT LEFT LAVATORY). ACCOMPLISHED CHECK AND UP TEST PER 26-14-00. OP CK NORMAL.
EMERGENCY EXIT SIGN BY THE R1 DOOR IS DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-00. OPS CHECKED GOOD.
LENS FOR THE EMERGENCY LIGHT ABOVE THE R4 DOOR MISSING. MAINTENANCE REPLACED THE LENS IAW AMM 33-51-02.
GALLEY LIGHT COVER BROKEN OFF. STRAIGHTENED LIGHT COVER AND INSTALLED, OK FOR SERVICE. THE AIRCRAFT WAS NOT GROUNDED.
AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR OUTBOARD SEAT HAS A LOW BATTERY. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
FLOOR SUPPORT CRACKED AT LBL 46 BETWEEN BS 312 AND 328. REMOVED AND REPLACED IAW SRM 51-40-02, AARD 51-00-05-01 AND DRAWING 141A5410.
FORWARD LOWER PRESSURE SEAL LANDING FITTING AT L2 DOOR CUTOUT IS CRACKED. REMOVED AND REPLACED LANDING IAW 51-00-05 REPAIR 1, DRAWING 147A8204 AND EA 264380.
FLOOR SUPPORT CRACKED AT LBL 46 BETWEEN BS 328 AND 344. REMOVED AND REPLACED IAW SRM 51-40-02, 51-00-05-01 AND DRAWING 141A5410.
EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT ROWS 16 AND 20. REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1671 IAW AMM 33-51-06. OPS CHECKED NORMAL.
AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE RT IRS FAULT & ALIGN LIGHT ILLUMINATED. R & R RT ADIRU IAW AMM 34-21-00. SYS CHECKED NORMAL.
DURING CRUISE PILOT REPORTED NUMBER 2 ENGINE OVERHEAT LIGHT ILLUMINATED. DIVERTED AND LANDED UNEVENTFULLY. FOUND NUMBER 2 ENGINE LOOP `A` WIRE CHAFED. R & R RT ENGINE OVERHEAT LOOP. PERFORMED OPERATIONAL CHECK IAW AMM 26-11-02. SYS CHECKED NORMAL.
LIGHT SURFACE CORROSION ON LOWER FUSELAGE SKIN FROM STATIONS 888 TO 1016 & STRINGERS 21 TO 25 LT. CORROSION R & R ACCOMPLISHED IAW EA B737-53-036943.
MIA CREW REPORTED LG WOULD NOT RETRACT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LG SELECTOR VLV. SYS GND CHECKED NORMAL, OPERATION CLOSED.
SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 8 TO 12 INOPERATIVE. FOUND ROW 8 HAD ONE WIRE FOR LIGHT GOUNDING OUT ON SEAT FRAME. REPLACED BATTERY PACK AND ROW 8 LIGHT SOCKET ASSEMBLY. OPS CHECK NORMAL.