N69833
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES INC | Operator | 2022-07-07 – 2022-07-07 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2022-07-07 – 2022-07-07 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
ECONOMY PASSENGER SEAT EPL - DETAIL VISUAL INSPECTION (PINNACLE COACH SEATS ONLY) (ADDED BY EC2500-16019) PROCEDURE - SEAT 24C EPL HOUSING MOUNTING TAB IS BROKEN. REMOVED AND REPLACED EPL HOUSING FOR SEAT 24C REF. IFM 25-23-55. EPL LIGHT OPS CHECKED GOOD IAW AMM 33-51-11.
ABOVE 120 KNOTS ON TAKEOFF ROLL AFT CARGO DOOR LIGHT ILLUMINATED. PRESSURIZATION NORMAL. AFT CARGO DOOR LIGHT ILLUMINATED DURING FLIGHT. CHECKED AFT CARGO DOOR, LOCKS AND LATCHES NORMAL. APPLIED MEL. CHECKED DOOR BEING LOCKED AND LATCHED BEFORE DISPATCH. T/S USING FIM 52-30 TASK 803. R/R AFT CARGO DOOR WARNING SWITCH (S961) IAW AMM 52-71-31-000-802. AFT CRAGO DOOR INDICATION SWITCH TEST PASSED. DURING PSEU SELF TEST ORIGINAL FAULT CLEARED BUT TWO NEW FAULTS APPEAR.. REQUIRES FURTHER T/S.. CYCLED POWER, TROUBLESHOT SYS PER FIM 52-10-802, PSEU SELF TEST PASS WITH NO EXISTING FAULTS.
NUMBER 1 ENG OIL FILTER BYPASS OCCURED ATFL270 300KIAS, DELCARED EMERGENCY LANDING. DURING INSPECTION, FOUND DEBRIS ON AGB/TGB SCAVENGE MCD. EXAMINED STARTER MAGNETIC PLUG CONTAMINATION REF AMM TASK 79-00-00-200-804-F00. NO PARTICLES FOUND.
RH WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD AT RBL 40.875, FOUND LATCH STOP WEARING STRIKER PLATE AND STRUCTURE. REMOVED SEAL AND SEAL RETAINER TRIM FROM ALONG THE RH LOWER CHORD TO FOM IAW SRM 51-40-02. CUTOUT DAMAGE AS PER REF STEP 4.E OF SRM 57-10-13-2R-3. INSPECTION REQUIRED REFER TO NDT PART 6, 51-00-00, PROCEDURE 4 OR 737 NDT PART 6, 51-00-00, PROCEDURE 23. ACCOMPLISED HFEC OF CUTOUT. REF NDT P6-51-00-00 23. NO DEFECTS NOTED SHOT PEENED CUTOUT AREA PER REF SRM 51-21-99-300-802 STEP H VERIFIED REPAIR CUTOUT AREA WAS FLAP PEENED, IAW SRM 51-21-99-300-802 STEP H. FABRICATED ITEM 1 & 4 (STRAP AND FILLLER) LOCATED & DRILLED IAW SRM 57-10 -13-2R-3 REPAIR INSTRUCTIONS 4(I) THRU (M) OK TO ALODINE & PRIME MATERIAL ID .125 7075 T6 FOR STRAP AND FILLER ITEMS 1 AND 4 TABLE 201 SRM 57-10-13-2R-3. UPDATED TO RII STATUS. ALODINED AND PRIMED OK TO INSTALL INSTALLED REPAIR PARTS AS PER SRM 57-1013-2R-3. INSTALLED REPAIR AS PER SRM 57-10-13-2R-3 VERIFIED INSTALLATION OF REPAIR IAW SRM 57-10-13-2R-3. IAW GMM 09-25-05. OK TO CONTINUE. INSTALLED PNEUMATIC DOOR 192DR ADJUSTED LATCHED SECURED PROPERLY AMM 52-48-42-820-004.
DIFFICULTY CONTROLLING FLIGHT DECK TEMP. SUPPLY DUCT OVER 40 DEG REES WHILE REQUESTING COLD CREW DEBRIEF: NO PROBLEMS TAXIING SINGLE ENGINE ON GROUND. IN FLIGHT, COCKPIT WAS WARM AND SUPPLY DUCT TEMP NEVER GOT BELOW 40*C UNTIL DESCENT DESPITE TURNING KNOB TO FULL COLD. FLIGHT ATTENDANTS REPORTED CABIN TEMPERATURE WAS COMFORTABLE AND ADJUSTABLE. DUCT PRESSURE WAS 44PSI THROUGHOUT FLIGHT. AIR COMING THROUGH THE VENTS IN THE COCKPIT WAS WEAK AND WARM. BITE BOTH PZTC'S NOTE FAULTS THEN DO APPLICABLE FIM. RUN BOTH PA CKS MONITOR TEMP FOR L&R PACKS RECOMMENDED IS 30DEG CELSIUS OR L ESS. ALSO DO FIM 21-62T905 FAULT ISOLATION PROCEDURE FOR CONTROL CABIN FAULT. NOTE FAULTS. ALSO CHECK FLOW FROM RECIRC FANS AND PACK DUCTING TO CONTROL CAB IN FOR BLOCKAGE. PERFORMED BITE ON BOTH PZTC. NO FAULTS NOTED. REF TSM 21-62 TASK 801. PER FIM 21-62 TASK 905 REPLACED CABIN TEMP SENSOR REF AMM 21-61-14. OPS CHECK PASSED. OPERATED BOTH PACKS SIMULTANEOUSLY AND INDIVIDUALLY, ADJUSTING ZONE TRIM AIR IN MANUAL AND AUTO SETTING. DUCT SUPPLY TEMP REMAINED AT 20C IN ALL CONDITIONS, HAD A CONSISTENT AIRFLOW, AND ADJUSTED ITS ZONE TEMPERATURE ACCORDINGLY.
FLOOR PROXIMITY EMERGENCY LIGHT INOP AT SEAT 38CBA REPLACED LIGHT ASSEMBLY. NO FIX. LIGHT STILL INOP. FURTHER T/S REQUIRED.PARTS USED: 76-2525-3-0269, QTY :1 REQUEST MEL 3319E FOR INOP FLOOR PROXIMITY LIGHT AT SEAT 38CBA. ALL OTHER EMERGENCY LIGHTS IN OPERATION. MEL 3319E MX WORKING ITEM CHECKED FOR GROUND ON EMERGENCY LIGHT SEAT CONNECTOR AT SEAT 38C AND FOUND NO CONNECTION. JUMPED LIGHT ASSEMBLY GROUND TO SEAT RAILS AND LIGHT OPERATED NORMALLY. TRACED WIRING TO SEAT 38A AND FOUND BROKEN GROUND WIRE ON CONNECTION NEAR FLOOR. WIRE REQUIRES RE-TERMINATION. EPL ILLUMINATES AS INTENDED. CABLE RACEWAY NEEDS TO BE ACCESSED UNDER SEAT BOTTOMS TO ROUTE REPLACEMEMT HARNESS. SEAT BOTTOM CUSHIONS REMOVED AND PLACED IN ROW 39. SEAT PARTS, NEW EPL HARNESS, AND SEAT TRACK COVER PLACED IN SEATS 38 DEF. REF CMM 25-23-55 REMOVED AND REPLACED EMERGENCY HARNESS REF AMM 25-22-00. OPS GEST GOOD REF AMM 33-51-00 INSPECTED PER IDT
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - WHITE EMERGENCY EXIT FLOOR LIGHT ROW 14ABC BROKEN. R&R ROW 14ABC EMERGENCY EXIT FLOOR LIGHT REF AMM 33-51-11. OPS CHECK GOOD.
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - DOOR 2R LOWER EMERGENCY EXIT SIGN CRACKED AND HALF BULBS INOP IDT C/W PROPER INSTALL AND OPS OF DOOR 2R LOWER EMERGENCY LIGHT REF GMM 09-10-05 UPON REMOVAL OF LENSE, FOUND COFFEE AND COFFEE GROUNDS REMOVED AND REPLACED DOOR 2R LOWER EMERGENCY EXIT SIGN ASSEMBLY WITH REFERENCE TO AMM 33-51-01. OPS CK GOOD.PARTS USED: 29-3351-3-0011,QTY :1 VERIFIED AREA IS CLEAN, ALL TOOLING REMOVED.
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - ROW 30ABC AISLE EPL INOP IDT C/W 30A EPL LIGHT OPC NORMAL REF GMM 09-10-05 BENEATH SEAT 30A, FOUND SEAT SIDE BLACK WIRE BROKEN FROM CRIMPED NEW MATE-N-LOK PIN CONNECTOR IAW BOEING SWPM 20-42-01, CONNECTOR AISLE EPL LIGHT OPS CHECK OKAY / PARTS USED: 00-0366-3-2289,QTY :1 REINSTALLED TRIM BENEATH SEAT 30A, ALL TOOLING REMOVED AND GARBAGE DISPOSED
ENG 2 OVERHEAT DURING DEPARTURE. LIGHT EXT AFTER REDUCING POWER OPENED #2 ENGINE COWLING AND INSPECTED BLEED AIR DUCTING. FOUND THE STAGE 9 INLET TUBE [23] TO THE HPTACC VALVE LOOSE AND COMBUSTION CASE FLANG AND SEAL BLOWN OUT. REPLACED SEAL ON STAGE 9 DUCT AND SECURED, REF AMM TASK 75-21-01-400-801-F00. ACTUATORS TEST AND IDLE TEST NORMAL.
SEVERAL EMERGENCY LIGHTS INOP. REF. AAR N/R:9208905. REMOVED AND REPLACED BATTERY PACK POSITION M1675 PER REF B737 AMM 33-51-06. PERFORMED EMERGENCY LIGHY OPERATIONAL TEST PER REF. B737 AMM 33-51-00, TEST FOUND NORMAL REF. AAR N/R:9208905
SEVERAL EMERGENCY LIGHTS INOP REF. AAR N/R:9208905 REMOVED AND REPLACED BATTERY PACK POSITION:M1670 PER REF. B737 A MM 33-51-06-. PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER REF B737AMM 33-51-00.TEST FOUND NORMAL. REF. AAR N/R:9208905
SEVERAL EMERGENCY LIGHTS INOP REF. AAR N/R:9208905 REMOVED AND REPLACED BATTERY PACK POSITION M2503 PER REF B737 AMM 33-51-06. PERFORMED EMERGENCY LIGHY OPERATIONAL TEST PER REF. B737 AMM 33-51-00, TEST FOUND NORMAL.
REMOVED AND REPLACED BATTERY PACK POSITION M1694 PER REF B737 AMM 33-51-06. PERFORMED EMERGENCY LIGHY OPERATIONAL TEST PER REF. B737 AMM 33-51-00, TEST FOUND NORMAL REF. AAR N/R:9208905
SEVERAL EMERGENCY LIGHTS INOP REF. AAR N/R:9208905 REMOVED AND REPLACED BATTERY PACK POSITION:M2627PER REF. B737 A M 33-51-06-. PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER REF B737AMM 33-51-00.TEST FOUND NORMAL. REF. AAR N/R:9208905
SEVERAL EMERGENCY LIGHTS INOP. REF. AAR N/R:9208905 REMOVED AND REPLACED BATTERY PACK M2626 PER REF. B737 AMM 33-51-06. PERFORMED EMERGENCY LIGHT OPERRATIONAL TEST PER REF. B737 AMM 33-51-00, TEST FOUND NORMAL REF. AAR N/R:9208905
SEVERAL EMERGENCY LIGHTS INOP. REF. AAR N/R:9208905 REMOVED AND REPLACED BATTERY PACK POSITION:M1671PER REF. B737 AM M 33-51-06-. PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER REF. B737AMM 33-51-00.TEST FOUND NORMAL. REF. AAR N/R:9208905
SEVERAL EMERGENCY LIGHTS INOP REF. AAR N/R:9208905 REMOVED AND REPLACED BATTERY PACK POSITION M1676 PER REF B737 AMM 33-51-06. PERFORMED EMERGENCY LIGHY OPERATIONAL TEST PER REF. B737 AMM 33-51-00, TEST FOUND NORMAL REF. AAR N/R:9208905
CORROSION AT AFT WET AREA AROUND R/H SIDE LAV I/B AFT HARD POINT FITTING STA 947 RLB 24 REF AAR N/R 9208678 ACCOMPLISHED INSTALLATION OF "T" CHORD, REPAIR SPLICES PARTS AND ALL PARTS REMOVED FOR ACCESS PER REF B737 SRM 53-70-51-2R-5, REPAIR 5 FIG 205. ACCOMPLISHED BY V940460.
LOWER FUS CENTER WING BOX R/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED AT STA 663.75 RBL 7. REF AAR N/R 9208547. REPAIRED ATTACH ANGLE AT R/H WING CENTER SECTION REAR SPAR VAPOR BARRIER STA 663.75 RBL 7 IN REF B737-900 SRM 57-10-10-2R-5. WORK ACCOMPLISHED BY V9208547.
ENG FIRE DETECT FAULT BOTH CHANELS NO 1 ENGINE INOP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. LP 9006579 ALSO ENCOUNTERED BIRD STRIKE THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/11/22.ENG FIRE DETECT FAULT BOTH CHANELS NO 1 ENGINE INOP.FOUND LOOP A AND B DAMAGED AT UPPER FAN LOOP. NEW ENGINE CAME WITH LOOPS INSTALLED OPS CHECKED SYS A AND B. OPS CHK GOOD.
LOUD BANGING NOISE RIGHT SIDE OF A/C ROW 31 ON CLIMBOUT. DTV SEAL FAILED THE BULBSEAL ORDERED COULD NOT BE INSTALLED DUE TO REMOVAL OF ECRA BY ENGINEERING FOR IT, SO CALLED LIVE TV AND THEY GAVE ME AN UPDATED FOR FAIRING WITH SEAL ALREADY INSTALLED P/N 73SK2102-101. NO REMOVAL POSSIBLE BECAUSE OF TOOLING, WEATHER, RADOME AND FAIRING PER AMM 44-20-15-350-803. NO DEFERRAL OR AND NO HANGAR. SLING NEEDED ARE K51101-107 AND K51101-105. ,51101-105 IS AVAILABLE IN MCO. TECHS CLEANED OLD SELANT AND INSPECTED FOR DAMAGE, NONE AT TIME. REMOVED RADOME AND FAIRING ASSY AS PER AMM 44-20-15-020-801 REPLACE BULB SEAL K23102-101 AS PER AMM 44-20-15-350-803 INSTALLED LIVE TV FARING AS PER AAM 44-20-15-420-801 AND ACCOMPLISHED ELICTRICAL CHECK AS PER AMM 44-20-15-760-801 ACCOMPLISHED ELICTRICAL CHECK AS PER AMM 44-20-15-760-801 INSTALLED LIVE TV FARING AS PER AAM 44-20-15-420-801 AND ACP RII INSPECTION REF GMM 09-25-05 ATA 44 INSTALLED RADOME AS PER AMM 44-20-16-420--801 SEE ALL UPDATED FOR WORK ACCOMPLISHED.
EMERGENCY FLOOR PROXIMITY LIGHT DOES NOT TURN ON 01B COVER OVER LIGHT MISSING. LIGHT OPS CHECK, REPLACED MISSING LENS
LE FLAP TRANSIT ON WHEN FLAP 1 SELECTED IN FLT. PERFORMED FSEU BITE CHECK, NO EXITSTING FAULT. NO LE FLAP FAULT HISTORY, BUT TE FLAP SNSR L 27-52259 ON LEG 0 ONLY. PERFORMED FIM TASK 27-51 TASK 813. OPS CHECKED LE & TE FLAPS FOR 3 CYCLES, CHECKED NORMAL, AND NO FAULT. RETURNED ACFT BACK TO NORMAL.