N67827
Registered owner: UNITED AIRLINES INC, IL (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.
56 reports on file, 2016-01-18 – 2026-08-18.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN BTW STA 269 AND 1.5" ABOVE OF S-19R. APPLIED PRIMER ON NEW RIVET ON FUSELAGE EXTERNAL SKIN AND SPOTFACE ON INTERNAL SKIN IAW B737-900ER IAW SRM 53-00-01-2R-38 STEP 4 E (6) SOPM 20-44-04. PERFORMED REPAIR ON FUSELAGE SKIN BTW STA 269 AND 1.150" ABOVE OF S-19R ALL WORKS WERE ACOMPLISHED IAW EO 260425 REV. P1, EO 260425 REV. IR AND EC/RA 5310-09013 REV. ORG. ECRA TRANSACTION COMPLETE PERFORMED REPAIR ON FUSELAGE SKIN BTW STA 269 AND 1.150" ABOVE O F S-19R ALL WORKS WERE ACOMPLISHED IAW EO 260425 REV. P1, EO 260 425 REV. P1, EO 260425 REV. IR AND EC/RA 5310-09013 REV. ORG. ES FR NO. 4198.
Part: WINGLET — DAMAGED (ZONE 600) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND POSSIBLE LIGHTNING STRIKE ON RT WINGLET UPPER TIP. PERFORMED A REPAIR ON THE RT WINGLET UPPER TIP IAW SRM 57-30-01-2R-6APB, 51-10-04-0G-0, 51-20-01-0G-0, SOPM 20-44-04, AMM 51-21-99-300-801 AND 51-21-99-300-802. THIS IS A CATEGORY A REPAIR NO FURTHER ACTION.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 727E - 727F, STR 24R - 25R. PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN BS 727E & 727F, STR 24R - STR 25R, ORIGINAL THICNESS: 0.090" MATERIAL LOSS: 0.005" REMAINING THICKNESS 0.085" FOUND TO BE WITHIN LIMITS, PERFORMED NDT NO CRACKS FOUND, WORK DONE IAW SRM 53-00-01-2R-38, 53-00-01-1A-5, 51-20-01-0G-0, AMM 51-21-11-150-801, 51-21-72-370-804, 51-21-99-300-802, & NDTM PART 6 51-00-00 PROCEDURE 23.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN BTW STA 322 AND 1 INCH ABOVE OF STRINGER 18R. PERFORMED A REPAIR OF LIGHTNING STRIKE ON FASTENER BTW BTW BS 322 AND 1 INCH ABOVE OF S18R, IAW SRM 53-00-01-2R-38. THIS REPAIR IS A CATEGORY A REPAIR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER BTW BS 328 & STRINGER 19R. PERFORMED REPAIR OF THE LIGHTNING STRIKE ON FASTENER IAW SRM 53-00-01-2R-40 THIS REPAIR IS A CATEGORY A REPAIR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER BTWN BS 294 & STRINGER 19R. PERFORMED REPAIR OF THE DAMAGE ON FASTENER. THIS REPAIR IS A CATEGORY A REPAIR AND NOT REQUIRE REPETITIVE INSPECTIONS IAW STEP 2.A.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FASTENER BTWN BS 236 AND 10" ABOVE OF EXTERNAL POWER. PERFORMED REPAIR IAW SRM 53-00-01-2R-40 THIS REPAIR IS A CATEGORY A REPAIR STEP 2.A.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 500A TO 500B, STR 19R. PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN BS 500A - 500B, STR 19R, IAW SRM 53-00-01-2R-41.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSP, FOUND LIGHTNING STRIKE ON SKIN BTWN BS 187 AND 8.5 INCHES BELOW OF STRINGER 17R. .REMOVED PAINT FROM SKIN IAW AMM 51-21-11-150-810. PERFORMED VISUAL INSP OF THE DAMAGE LOCATION, DAMAGE IS NO MORE THAN 0.5 INCH OF LEGHT AND BLEND OUT IAW SRM 51-00-01-2R-38 PAR 4 AND SRM 53 -00-01-2R-38 STEP 4.D(2) NDT INSPECTION PERFORMED IAW NDTM PART 6 51-00-00 PROCEDURE 23, & SRM 53-00-01-2R-38, STEP 4. D(3), NO CRACK SIGNAL NOTED. NDT INSPECTION WAS PERFORMED IAW NDTM PART 4, 51-00-00 PRO CEDURE 2, REMAINING THICKNESS 0.042", FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01-1A-1, STEP 4.( 2) (D), FIGURE 103, DETAIL C, FIG 104, SHT 3, AND SRM 53-00-01- 2R-38, STEP 4.D(2) APPLIED ALODINE, PRIMER, & PAINT IAW AMM 51-21-41-370-802, AMM 51-21-72-370-804, & AMM 51-21-99-300-802.
Part: SKIN — DAMAGED (ZONE 200) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER BTWN BS 360 AND 2 INCHES ABOVE OF STRINGER 14R. PERFORMED A REPAIR ON SKIN, PERFORMED NDT, NO CRACKS FOUND, THIS REPAIR IS CATEGORY A AND NOT REQUIRE REPETITIVE INSPECTIONS, ALL WORK PERFORMED IAW SRM 53-00-01-2R-40, 51-40-02-0G-0, 51-2 0-01-0G-0, AMM 51-21-11-150-80, 51-21-72-370-804, 51-21-73-370-8 01, NDTM PART 6 51-00-00 PROCEDURE 16.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BTWN BS 500C - 500D, STRINGER 18R. PERFORMED A REPAIR TO THE SKIN IAW SRM 53-00-01-2R-41 THIS REPAIR IS A CATEGORY A REPAIR AND NOT REQUIRE REPETITIVE INSPECTIONS STEP 2.A.
Part: FASTENER — DAMAGED (ZONE 200) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER AT BS 293, S18R. PERFORMED REPAIR OF THE LIGHTNING STRIKE ON FASTENER IAW SRM 53-00-01-2R-40, THIS REPAIR IS A CATEGORY A REPAIR STEP 2.A.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND A LIGHTNING STRIKE ON FUSELAGE SKIN BTWN BS 221 & 7.7 INCHES BELOW S17R. PERFORMED A REPAIR ON FUSELAGE SKIN IAW SRM 53-00-01-2R-38, THIS REPAIR IS A CATEGORY A REPAIR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FASTENER BTW STA 197 AND 8.3 INCHES BELOW OF STRINGER 17R. PERFORMED REPAIR IAW SRM 53-00-01-2R-41 THIS REPAIR IS A CATEGORY A REPAIR AND NOT REQUIRE REPETITIVE INSPECTIONS STEP 2.A.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION, FOUND A LIGHTNING STRIKE ON FUSELAGE SKIN BTWN BS 199 AND 7.5 INCHES BELOW OF S-17R. PERFORMED A REPAIR ON FUSELAGE SKIN IAW SRM 53-00-01-2R-38, THIS REPAIR IS A CATEGORY A REPAIR.
Part: SKIN — DAMAGED (ZONE 100) · airframe 37,064 hrs · 13,735 cycles
AFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN BTW BS 213.8 AND 8 INCHES BELOW OF S17R. PERFORMED REPAIR LIGHTNING STRIKE ON SKIN BTW BS 213.8 AND 8 INCHES BELOW S17R, IAW SRM 53-00-01-2R-38 THIS REPAIR IS A CATEGORY A REPAIR.
Part: SKIN — SCRATCHED (ZONE 200) · airframe 37,064 hrs · 13,735 cycles
LEFT PRIMARY STATIC PORT WAS SCRATCHED. BLENDED & EVALUATED SCRATCH ON LT PRIMARY STATIC PORT, LOCATED BTW BS 411.3 AND 2.5" BELOW OF S15L, FOUND WITHIN LIMITS, PERFORMED NDT INSPECTION, NO CRACKS SIGNAL NOTED, APPLIED ALODINE, REVIEWED THE AERODYNAMIC SMOOTHNESS, THE SMOOTHNESS WAS SATISFACTORY AND NOT DECREASE IN THE PERFORMANCE, MEASURED THE SKIN WAVINESS FOUND TO BE WITHIN LIMITS IAW SRM 53-30-01-1A-2, SRM 51-20-13-0G-0, SRM 51-20-01-0G-0, SRM 51-10-01-0G-0, AMM 34-11-02-200-802.
Part: LENS — MISSING (ZONE 200) · airframe 36,361 hrs · 13,425 cycles
EMERG PATH LIGHT MISSING SEATS 1ABC REPLACED LENS. OPS CHECK AMM 33-51-00
Part: OVEN — CONTAMINATED (ZONE 900) · airframe 36,241 hrs · 13,381 cycles
FRONT OVENS SMELLING OF CAMPFIRE. NO SMOKE NOR EVIDENCE OF FLAME . DISCONTINUED USE. PLACING BOTH FIRST CLASS GALLEY OVENS ON DEFERRAL IAW NEF 2510AU. FOUND FWD GALLEY OVEN 204 WITH BURNED PAPER DEBRIS. REMOVED DEBRIS AND CLEANED INSIDE OF OVEN PERFORMED OPS CHECKED, NO MORE CAMPFIRE ODOR NOTED. ADJACENT OVEN HAD NO ISSUES. REF AMM 25-34-00-400-801-C4 AND AMM 25-34-00-100-801-C1. OPS CHECKED GOOD. PLACARD REMOVED.
Part: SKIN — SCRATCHED (ZONE 100) · airframe 35,659 hrs · 13,142 cycles
RAMP DAMAGE. SCRATCH AT FWD CARGO DOOR THRESH HOLD CUTOUT APPROX. 10IN. ABOVE R/H LOWER CORNER. SCRATCH DAMAGE IS L=3. 968 W=1 AND 0.0073 IN DEPTH. ADDING PICTURES OF DAMAGED BEHIND PANEL. DENT AT THE THRESH HOLD MEASURES L= 0.6875" W= 0.212" DEPTH = 0.0937" MAJOR REPAIR. PERFORMED A REPAIR TO THE DAMAGED FUSELAGE SKIN & BEAR STRAP AT THE FWD EDGE OF THE FWD CARGO DOOR CUTOUT FROM BS 420 - 460 AND FROM S20 - 26R IAW ESR-WI 1-14461 REV IR AND ECRA 5330-07681.
Earlier reports · 2016–2025 · 36 reports
2025
Part: GIRT BAR — PULLED (ZONE 800) · airframe 35,423 hrs · 13,046 cycles
DOOR 1L SLIDE GIRT BAR PULLED OUT REPORTED BY MOVE TEAM. RECLIPPED BAR FOR MOVE. FOUND GIRT BAR REINSTALLED, HOWEVER THE "Z" FOLD NEEDS TO BE TUCKED IN. READJUSTED Z FOLD REF AMM TASK 25-66-01-400-803. OPS CHK GOOD.
Part: SPEED BRAKE — FAULTED · airframe 35,373 hrs · 13,022 cycles
SPEEDBRAKE DO NOT ARM LIGHT ILLUMINATED AT 70KTS DURING TAKEOFF. REQ MEL 2707F. VERIFIED MANUAL SPEEDBRAKE DEPLOYED AND STOWED. OPENED AND COLLARED C/B PER THE MEL. PLACARD APPLIED. PERFORMED FIM TASK 27-62 TASK 802 STEP E (2) . NO FURTHER ACTION REQUIRED . NO FAULTS , DO NOT ARM LIGHT NOT ILLUMINATED AT THIS TIME . OK TO CONTINUE
Part: BLEED VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 35,095 hrs · 12,895 cycles
LEFT ENGINE BLEED PRESSURE INDICATES 7PSI IN CLIMB & CRUISE, OPENED NR 1 ENGINE & TR FOUND NO OBVIOUS VISIAL DESCREPENCIES. OPENED & CLOSED NR 1 ENGINE. PERFORMED HIGH POWER RUN REF FIM 36-10 TASK 804. ZERO DUCT PRESSURE ON ENG NR 1 AT ALL POWER LEVELS. PERFORMED ENG BLEED AIR SYS HEALTH CHK IAW AMM 36-11-00-700-801 UP TO STEP G.5(D).2, PRSOV FAILED. R & R PRSOV REF AMM 36-11-04. CONTINUED ENG HEALTH CHK. R & R BLEED AIR REGULATOR REF AMM 36-11-03. NO FIX. CONTINUED HEALTH CHK AMM 36-11-00-700-801 UP TO BUT NOT INCLUDING STEP G.6(E)9. R & R THE BLEED AIR REGULATOR REF AMM:36-11-03, ATTEMPTED HEALTH CHK FROM PREVIOUS STEP, COULD NOT GET ANY SUPPLY AIR THROUGH BAR. BENCHED CHKD BAR, & FOUND OPEN NR 1 ENG, ACCOMPLISHED ENG BLEED AIR CROSSOVER OPS TEST PER MM 36-11-00-710-801. ALL DUCT PRESSURES WITHIN MM LIMITS.
Part: HANDLE — UNSECURE (ZONE 100) · airframe 34,968 hrs · 12,843 cycles
HYD SYS A QTY DROPPING IN LEVEL FLIGHT 75 TO 70 IN 30 MINUTES, PERFORMED AMM TASK 29-00-00-790-801, HYDRAULIC SYSTEM EXTERNAL LEAKAGE CHECK. NO LEAKS FOUND. FOUND HYD SERVICING LEVER IN WHEEL WELL NOT IN CLOSED POSITION. PERFORMED AMM TASK 29-11-00-200-801, HYD FLUID LEVEL CHECK AND BLED SYSTEM IAW AMM TASK 29-00-00-870-801. SYSTEM PRESSURE AND QTYS NORMAL. SUSPECT AIR MAY HAVE ENTERED SYSTEM DUE TO PUMP HANDLE NOT BEING CLOSED & SECURED.
Part: TIRE — WORN (ZONE 700) · airframe 34,146 hrs · 12,515 cycles
EXCESIVE NOSE WHEEL VIBRATIONS ON TAKEOFF TO THE POINT WE THOUGH T WE BLEW A TIRE INSPECTED TIRES ALL PRESSURES AND TREAD WEAR WITHIN LIMITS, NO TIRE TREAD LOSS FROM THIS AIRCRAFT. TOWER REPORTED AFTER TAKEOFF RUBBER TREAD FOUND ON RUNWAY, TIRE TREAD LOSS POSSIBLE FROM ANOTHER AIRCRAFT. ACCOMPLISHED GENERAL VISUAL INSPECTION FOR ADD EMP:U401069 IMPACT DAMAGE ON FUSELAGE AND FLIGHT CONTROLS SURFACES PER AMM TASK 05-51-54-210-801 AND AMM TASK 05-51-67-280-801. REPLACED LH AND RH NLG WHEEL ASSY AS PRECAUTION REF LOGPAGE #5027673 AND #5027679. RETORQUED SHIMMY DAMPER AS PRECAUTION REF LOGPAGE #5029568 .
Part: SLIDE — FAULTED (ZONE 800) · airframe 33,984 hrs · 12,451 cycles
REMOVED AND REPLACED ESCAPE SLIDE ON 1L PER NON-ROUTINE 002635416 REMOVED AND REPLACED 1L ESCAPE SLIDE PER NON-ROUTINE 002635416ROTABLE PARTS CHG:TT # 1452082 SN OFF 0439 PN OFF 29-2566-9-0007.SLIDE, FWD/AFT OFF 29-2566-9-0007 0439 ON 29-2566-9-0006 0507
Part: SLIDE — EXPIRED (ZONE 800) · airframe 33,713 hrs · 12,343 cycles
REMOVED & REPLACED LA DOOR-MOUNTED ESCAPE SLIDE REF JOB CARD 29-0525-8-0697. LP CREATED FOR ROTABLE PARTS TRANSACTION. REPLACED LA DOOR-MOUNTED ESCAPE SLIDE PER JOB CARD 29-0525-8-0697. PARTS USED: 29-2566-9-0007, QTY :1 ROTABLE PARTS CHG:TT # 1503111 SN OFF 1540 PN OFF 29-2566-9-0007.SLIDE, FWD/AFT OFF 29-2566-9-0007 1540 ON 29-2566-9-0007 2906
Part: LIGHT — FAILED (ZONE 200) · airframe 33,300 hrs · 12,175 cycles
EMER EXIT LIGHTS NOT ARMED LIGT FELL APART WHEN CHANGING THE BUL B REPLACED SWITCHED PER AMM 33-51-00 ,OPS CHECK GOOD
2023
Part: BATTERY PACK — DISCHARGED (M1676) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M1676 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288865. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND PERFORMED OPS CH ECK GOOD IAW B737 AMM 33-51-06. (M1676) HAECO GSO MECH V933790 INSP QC393
Part: BATTERY PACK — DISCHARGED (M1673) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M1673 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288870. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND PERFORMED OPS CH ECK GOOD IAW B737 AMM 33-51-06. (M1673) HAECO GSO MECH V933790 INSP QC393
Part: BATTERY PACK — DISCHARGED (M1671) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M1671 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288867. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1671 AND OPS CHECK GOOD IAW AMM 33-51-06. HAECO GSO MECH V941318 INSP QC393
Part: BATTERY PACK — DISCHARGED (M1670) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M1670 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288868. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1670 IAW B737NG AMM 33-51-06. OPS CHECK GOOD IAW B737NG AMM 33-51-06. HAECO GSO ME CH V902280 INSP QC393
Part: BATTERY PACK — DISCHARGED (UNKNOWN) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M1675 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288044. REMOVED AND REPLACED EMERGENCY PACK M1675 IAW B737NG AMM 33-51-0 6. OPS CHECK GOOD IAW B737NG AMM 33-51-06.
Part: BATTERY PACK — DISCHARGED (M2816) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M2816 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288045. REMOVED AND REPLACED EMERGENCY BATTERY PACK M2816 IAW B737NG AMM 33-51-06. OPS CHECK GOOD IAW B737NG AMM 33-51-06. HAECO GSO ME CH V902280 INSP QC393
Part: BATTERY PACK — DISCHARGED (M1672) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M1672 EMERGENCY BATTERY PACK NEEDS REPLACED. TRANSCRIBED FROM HAECO GSO NRC# 9288869. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1672 AND OPS CHECK GOOD IAW AMM 33-51-06. HAECO GSO MECH V941318 INSP QC393
Part: BATTERY PACK — DISCHARGED (M2503) · airframe 28,735 hrs · 10,393 cycles
(SUPPORT TASK) M2503 EMERGENCY BATTERY PACK NEEDS REPLACED. TRAN SCRIBED FROM HAECO GSO NRC# 9288866. REMOVED AND REPLACED EMERGENCY BATTERY PACK M2503 IAW B737NG AMM 33-51-06. OPS CHECK GOOD IAW B737NG AMM 33-51-06. HAECO GSO ME CH V902280 INSP QC393
Part: DOOR FRAME — GOUGED (L-1 DOOR) · airframe 28,735 hrs · 10,393 cycles
L-1 DOOR AFTER REMOVING LOWER SEAL LOCATOR FOUND FWD FRAME DEEP GOUGED AT LOWER END NEAR LOWER GATE. TRANSCRIBED FROM HAECO GSO NRC# 9288712. REMOVED DAMAGED FRAME REF B737-900ER SRM 51-40-02 AND INSTALLED COMPOUND REF B737-900ER AMM 51-41-11. HAECO GSO MECH V901058 IN NEW FRAME REF B737-900ER SRM 51-40-02, BAC DWG 141A6101 REV D, B SP QC002 AC DWG 141A6185 REV F AND BAC DWG 141A6260 REV C. RESTORED FINIS H TO AREA REF B737-900ER AMM 51-21-99. RE-APPLIED LEVELING
Part: CREASE BEAM — CORRODED (STA 946) · airframe 28,735 hrs · 10,393 cycles
(B737-53-3-0711) **CORROSION** FOUND AT STA 946 RIGHT CREASE BEAM INNER CHORD/UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NRC# 9 288445
Part: FLOOR PANEL — DAMAGED (PANEL 231DF) · airframe 28,735 hrs · 10,393 cycles
SUPPORT TASK: MAIN CABIN FLOOR PANEL 231DF HAS SURFACE DAMAGE. TRANSCRIBED FROM HAECO GSO NRC# 9288652. EVALUATED FLOOR PANEL 231DF AND FOUND MISSING/PEELING FIBERS THR OUGHOUT UPPER SURFACE AND 1EG DELAM IAW UAL B737-900ER SRM 53-30 -50-1A-0 AND SRM 53-00-50-1A. REPAIR IAW UAL B737-900ER SRM 53-0 0-50-2R HAECO GSO MECH V936283 INSP QC357
Part: FLOOR PANEL — DELAMINATED (PANEL 231UF) · airframe 28,735 hrs · 10,393 cycles
SUPPORT TASK: MAIN CABIN FLOOR PANEL 231UF HAS SURFACE DELAMINATION. TRANSCRIBED FROM HAECO GSO NRC# 9288657. COMPLETED WET LAY UP REPAIR ON MAIN CABIN FLOOR PANEL 231UF IAW B737-900ER SRM 53-00-50-2R-0 HAECO GSO MECH V902229 INSP QC357
Part: FLOORBEAM — CORRODED (STA 328) · airframe 28,735 hrs · 10,393 cycles
B757-53-3-0711 MAIN CABIN FLOORBEAM UPPER SURFACE HAS CORROSION AT STA 328, FROM RBL 44 - RB; 54 - MARKED REF HAECO GSO NR 9288578 REMOVED CORROSION IN AREA, ORIG MAT .125, REMOVED .025, REMAININ G IS .100, OUT OF LIMITS IAW B737-900 SRM 53-10-51-1A-1. INSTALL ED REPAIR STRAP AND TAPERED FILLER TO AREA IAW B737-900 SRM 53-1 0-51-2R-8. SFR# 1033135. HAECO GSO MECH V899687,INSP QC031
Part: SEAT TRACK — CORRODED (STA 500C-500F) · airframe 28,735 hrs · 10,393 cycles
MAIN CABIN SEAT TRACK UPPER SURFACE IS CORRODED FROM APPROX STA 500C-500F, LBL 24(MARKED). TRANSCRIBED FROM HAEC O GSO NR 9288474. ZR-4 REPAIR 4. HAECO GSO MECH V899687 REMOVED CORROSION ON SEAT TRACK MAT LOST EXCEEDS MAT LIMITS ALLO WED IN AREA OF 20% AT FS500C+0 TO F500F+10 LBL 24 IAW B737-900ER SRM 53-00-52, FIG 103, REMOVED AND REPLACED SEAT TRACK FROM 500 C+10 TO F500+100 WOTJ 2A SPLICES IAW B737-900ER SRM 53-00-52
Part: INSERT — DAMAGED (PANEL 242ZCF) · airframe 28,735 hrs · 10,393 cycles
SUPPORT TASK: MAIN CABIN FLOOR PANEL 242ZCF HAS 2 DAMAGED INSERTS. TRANSCRIBED FROM HAECO GSO NRC# 9288649 REMOVED AND REPLACED DAMAGED INSERTS IAW B737-900ER SRM 53-00-50 -1A-1 AND SRM 53-00-50-2R-0 ON MAIN CABIN FLOOR PANEL 242ZCF. H AECO GSO MECH V901642 INSP QC357
Part: FLOOR PANEL — DAMAGED (PANEL 232RF) · airframe 28,735 hrs · 10,393 cycles
SUPPORT TASK: MAIN CABIN FLOOR PANEL 232RF HAS SURFACE DAMAGE. TRANSCRIBED FROM HAECO GSO NRC# 9288656. EVALUATED PANEL 232RF P/N 144A5810-124 AND FOUND MULTIPLE AREAS OF MISSING/PEELING FIBERS IAW B737-900ER SRM 53-00-50-1A-1. REPA IRED DAMAGED AREAS IAW B737-900ER SRM 53-00-50-2R-0. HAECO GSO MECH V936283 INSP QC357
Part: INSERT — DAMAGED (PANEL 241ZFF) · airframe 28,735 hrs · 10,393 cycles
SUPPORT TASK: MAIN CABIN FLOOR PANEL 241ZFF HAS 2 DAMAGED INSERTS. TRANSCRIBED FROM HAECO GSO NRC# 9288662. REMOVED AND REPLACED DAMAGED INSERTS IAW B737-900ER SRM 53-00-50 -1A-1 AND SRM 53-00-50-2R-0 ON MAIN CABIN FLOOR PANEL 241ZFF. H AECO GSO MECH V901642 INSP QC357
Part: FLOOR PANEL — DAMAGED (PANEL 241GF) · airframe 28,735 hrs · 10,393 cycles
SUPPORT TASK: MAIN CABIN FLOOR PANEL 241GF HAS SURFACE DAMAGE. TRANSCRIBED FROM HAECO GSO NRC# 9288660 EVALUATED PANEL 241GF P/N 146A5810-455 AND FOUND MULTIPLE AREAS OF SURFACE DAMAGE ON UPPER SURFACE IAW B737-900ER SRM 53-00-50-1 A-1. REPAIRED DAMAGED AREAS IAW B737-900ER SRM 53-00-50-2R-0. H AECO GSO MECH V936283 INSP QC357
2021
Part: INDICATOR — MALFUNCTIONED (FLAP SYSTEM) · airframe 22,020 hrs · 7,919 cycles
*EMERGNCY DECLARED ON LANDING* NO FLAP LANDING NEEDLE NOTICABLE SPLIT WHEN UP LOCKED PER TOMC SM LOCKED FOR SIGNOFFS. T/S REF FIM 27-59-00-810-809 NO ACTIVE FAULTS NOTED R&R FLAP POSTION INDICTOR REF MM 27-58-02 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1004083 SN OFF 2916 INDICATOR, POSI OFF 29-2758-9-0001 2916 ON 29-2758-9-0001 5116
Part: CONNECTOR — LOOSE (FLAP TRANSMITTER) · airframe 21,994 hrs · 7,911 cycles
REF. L/P 6406582, PERFORMED FSEU BITE REF. FIM 27-51 TASK 801. N O EXISTING FAULTS NOTED. WHILE T/S , FOUND RIGHT FLAP POSITION T RANSMITTER CONNECTOR LOOSE. AS PRECAUTIONARY, REMOVED RIGHT FLAP POSITION TRANSMITTER REF. AMM 27-58-01-000-801. NEW TRANSMITTER CURRENTLY NIS AND ON AOG. INSTALLED NEW RT FLAP POSITION TRANSMITTER AS PER AMM 27-58-01-400-801, ALL INDICATIONS NOW NORMAL, OPS CHECKS GOOD AS PER AMM. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1966724 SN OFF 2272 TRANSMITTER, FL OFF 59-2758-9-0002 2272 ON 59-2758-9-0002 2094
2020
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 20,861 hrs · 7,527 cycles
RT LOWER EXTERNAL FUS-WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE IS CRACKED, REF NR 9473300. REMOVED DAMAGED SECTION OF ATTACH ANGLE AT RT LOWER EXTERNAL FUS-WING CENTER, REAR SPAR VAPOR BARRIER. FABRICATED ANGLE & SPLICE, TREATED & PRIMED AND INSTALLED, REF B737-900ER SRM 57-10-10 FIG 202 & 51-20-01.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 20,861 hrs · 7,527 cycles
SUSPECTED CRACK AROUND FASTENER AT WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BETWEEN LBL 5-10, REF NR 9473544. REMOVED DAMAGED SECTION OF ATTACH ANGLE AT LBL 5-10 WING CENTER REAR SPAR VAPOR BARRIER. FABRICATED ANGLE & SPLICE. TREATED AND PRIMED AND INSTALLED, REF B737-900ER SRM 57-10-10 FIG 202 & 51-20-01.
Part: SKIN — CRACKED (GROUND POWER BOX) · airframe 20,861 hrs · 7,527 cycles
FOUND CRACK AT ELECTRICAL GROUND POWER RECEPTACLE SURROUNDING DOUBLER LOWER FLANGE, REF AAR N/R 9473376. ACCOMPLISHED REPAIR AT ELECTRICAL GROUND POWER RECEPTACLE SURROUNDING DOUBLER LT WING FLANGE, AS PER REF B737-900ER SRM 53-10-15 REPAIR 4 FIG 204.
Part: SWITCH — INOPERATIVE (CABIN PRESSURE) · airframe 20,858 hrs · 7,526 cycles
CABIN ALTITUDE AUTO DROP TEST FAILED. REMOVED AND REPLACED ALTITUDE PRESSURE SWITCH, IAW AMM 35-22-41. OPERATIONS CHECK GOOD, IAW AMM 35-22-41. WORK ACCOMPLISHED BY AAR ROCKFORD MECHANIC V931575. THIS TEST WAS PERFORMED AS PART OF THE RETURN TO SERVICE PROCESS.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,858 hrs · 7,526 cycles
EMERGENCY LIGHTS FOR L1, L2 AND ROWS 28-34 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, IAW AMM33-51-06. OPERATIONS CHECK GOOD. WORK ACCOMPLISHED BY AAR ROCKFORD MECHANIC V931575.
2017
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,543 hrs · 4,470 cycles
EMERGENCY LIGHT LENS MISSING NEAR CLOSET 712. REPLACED THE LENS.
Part: SKIN — DAMAGED (BS 755-888) · airframe 10,026 hrs · 3,576 cycles
THE FUSELAGE SKIN DAMAGED LT SIDE FWD OF THE L2 DOOR, EXTENDING FROM BS 755 TO 888, BETWEEN STRINGERS 18 AND 19L. REPAIRED IAW ECRA 5300-02417, REV A,
2016
Part: GALLEY — POWER LOSS (CABIN) · airframe 5,636 hrs · 1,996 cycles
LOST ALL GALLEY & LAVATORY POWER, AIRBORNE. NOTICED BURNING SMELL IN AFT GALLEY. FLIGHT DECK INDICATIONS NORMAL. ACCOMPLISHED FIM TASK 25-31-00-810-801 BPCU BITE, NO FAULTS, OPERATIONS TEST MM TASK 24-21-00-700-803, NO FAULTS. IAW MFG FLEET TEAM DIGEST ARTICLE 737NG-FT-24-12003, REPLACED BPCU PRECAUTIONARY, MM TASK S 24-41-21-000-801, 24-41-21-400-801. TESTED IN AIR MODE OK, 32 -09-00-860-80.