N12125

Service difficulty reports · 122

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N12125' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026100520111Light · damagedEMERGENCY EXIT LIGHTS-FLOOR LIGHT DAMAGED SEAT 21 B EMERGENCY EXIT LIGHTS DAMAGED RESECURED EMERGENCY LIGHT REF AMM 33-51-11. OPS CHECKED GOOD.Oct 2, 2026 · N12125 · Boeing 757224 · Emergency LightingSDR CALA2026091719520Lamp · faultyL1 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-06.Sep 16, 2026 · N12125 · Boeing 757224 · Emergency LightingSDR CALA2026090119180Control Panel · faultedBACKLIGHTING INOP FOR OVERHD PANEL EMERLTS EMERGENCY LIGHT SWITCH PANEL BACKGROUND LIGHT INOPREF IMAGE TOMC APPROVED PLACED ON MEL REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PANEL DUE TO BACKGROUND LIGHTS INOP PANEL OPS CHECKS GOOD.Aug 31, 2026 · N12125 · Boeing 757224 · Emergency LightingSDR CALA2026082518902Frame · damagedAFT CARGO RH FREE FLANGE AT STA 1500 B/W STR 26 AND 27 HAS OPEN HOLE NEXT TO PLUG FASTENER. ACCOMPLISHED REPAIR PER VT MAE EA 757-5360-13-A4581 WITH NO DEVIATIONS. REF ECRA 5360-02196 PART 1- INTERIM REPAIR. ADD EMP:V944084 ACCOMPLISH A PERMANENT REPAIR AT FUSAug 20, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026082518896Frame · damagedAFT FARGO COMPARTMENT RH SIDE FR 1520 B/W STGR 23 - 26 FREE FLANGE HAS 2EA HOLES PLUGGED. FOR THE REPAIR AT FUSELAGE SECTION 46, AFT CARGO COMPARTMENT RH STA 1520 FRAME STGR 23R-24R AND STGR 25R-26R, PLANNING TO CONTACT ENGINEERING AFTER 18-JAN-2028 BUT BEFORAug 20, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026082518894Frame · damagedAFT CARGO RH FREE FLANGE AT STA 1500 B/W STR 26 AND 27 HAS OPEN HOLE NEXT TO PLUG FASTENER. FOR THE REPAIR AT FUSELAGE SECTION 46, AFT CARGO COMPARTMENT RH STA 1500 STGR 26R-27R, PLANNING TO CONTACT ENGINEERING AFTER 18-JAN-2028 BUT BEFORE 04-FEB-2028 FOR THE Aug 20, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026082518892Frame · damagedAFT FARGO COMPARTMENT RH SIDE FR 1520 B/W STGR 23 - 26 FREE FLANGE HAS 2EA HOLES PLUGGED. ACCOMPLISHED REPAIR PER VT MAE EA 757-5360-13-A4585 WITH NO DEVIATIONS.REF EC/RA 5360-02197 PART 1 INTERIM REPAIR FIGURES 1-13.. ACCOMPLISH A PERMANENT REPAIR AT FUSELAGEAug 20, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026082518890Access Panel · crackedCRACK INDICATION FOUND ON LEFT WING ACCESS PANEL 543BB HOLE #6 AT 12 O' CLOCK POSITION LOOKING. PERMANENT REPAIR FOR L/HWING INTERSPAR LOWER SKIN (P/N 757-3401-1) OUTBOARD OF THE SPLICE AT WSTA 711.50 PER THE LATEST REVISION OFEC/RA 5720-03672.Aug 20, 2026 · N12125 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026082518878Access Panel · crackedCRACK INDICATION FOUND ON LT WING ACCESS PANEL 543BB HOLE #6 AT 12 O' CLOCK POSITION LOOKING. ACCOMPLISHED REPAIR INSTRUCTIONS PER VT MAE EA 757-5720-13-A4564 REV. ORIGINAL WITH NO DEVIATIONS. PER ECRA 5720-03672 FIG. 1-29 FOR REFERENCE. LT WING INTER SPAR LOAug 20, 2026 · N12125 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026082118798Access Panel · cracked)EA5720-03647 PER FIGURE 1, CRACK INICATION FOUND ON LT WING ACCESS PANEL 543BB, HOLE NR 6 AT THE 12 O'CLOCK POSTION LOOKING FORWARD. A REPAIR WAS PERFORMED ON LT WING SKIN IAW EC/RA 5720 -03672, & EA 757-5720-13-A4564 REV-.Aug 20, 2026 · N12125 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026082118794Frame · damagedAFT CARGO, RT FREE FLANGE AT BS 1500 BTWN STRINGERS 26 - 27 HAS AN OPEN HOLE NEXT TO PLUG FASTENER. REPAIRED PERFORMED ON AFT CARGO, RT FREE FILANGE AT BS A500 BTWN S26 - 27 IAW EC/RA #5360-02196, & EA757-5360-13-A4581 REV-.Aug 20, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026082118792Frame · gougedMAIN CABIN LT FRAME AT BS 1100 BTW STRINGERS 16L-17L GOUGED. ACCOMPLISHED REPAIR IAW ECRA 5340-02283, AND EA 757-53 40-13-A4586 REV-.Aug 20, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026082118786Frame · dentedAFT CARGO, FRAME DENTED AT LT BS 1320, BTWN STR 25- 26. REPAIRED THE FRAME BS 1320, STR 25 - 26 IAW UAL ECRA 5360-02198 AND VT MAE EA 757-5360-13-A4576 REV-.Aug 19, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026081918723Skin · dentedFUS. EXT SKIN WITH DENTS (4EA) STA 310-327 BTW STRGR 2L-4L. DENT 1.) A=1.187" Y=.019" A/Y=62.4 DENT 2) A=.720" Y =.008 A/Y=90 DENT 3) A=795 Y=.012 A/Y=66.25 DENT 4) A=.850 Y=.01 0" A/Y=85. IN LIMITS IAW 53-00-01-1A-1 DENTIII. DENTS HAVE INSUFFICIENT DISTANCEAug 17, 2026 · N12125 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2026082018742Frame · damagedAFT CARGO, RT SIDE FRAME BS 1520 BTWN STR 23 - 26R, FREE FLANGE HAS 2EA HOLES PLUGGED. ACCOMPLISHED REPAIR IAW ECRA 5360-0 2197 AND EA 757-5310-13-A4585 REV-.Aug 16, 2026 · N12125 · Boeing 757224 · Fuselage Main, FrameSDR CALA2026081818711Angle · crackedRT MLG WHEEL WELL AT BS 1094.2 RBL 64 .5, SEAL RETAINER ANGLE IS CRACKED. REMOVED, FABRICATED, LOCATED, DRILLED, RESTORED SURFACE PROTECTI ON AND INSTALLED SEAL RETAINER ANGLE IAW REF DRAWING 149N7550 AN D B757 SRM 51-40-02-0G-0, SRM 51-40-04.Aug 16, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026082018740Beam · crackedVERTICAL STAB. FIXED T/E LT LOWER SEAL TO FUSELATE OUT OF THE RIGHT PLACE. REMOVED, FABRICATED AND INSTALLED BEAM COMMON TO LT VERTICAL LOWER FUSELAGE, FABRICATED & ATTACHED IAW DWG 173N1300, & SRM 51-40-02-0G.Aug 14, 2026 · N12125 · Boeing 757224 · Vertical Stabilizer Miscellaneous StructureSDR CALA2026081718658Angle · crackedLEFT MLG WHEEL WELL, FWD SEAL RETAINER AT BS 1060, BRACKET ANGLE IS CRACKED AT LBL 10. R & R ONE EACH 654N0243-13 BATCH 0004481466 LT WHEEL WELL SEAL RETAINER CORNER BRACKET IAW SRM 51-40-02-0G-0.Aug 14, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026081718656Support Bracket · crackedLEFT MLG WHEEL WELL, A.C.M.P. CD/PRESSURE FILTER HYD. MODULE, SUPPORT BRACKET IS CRACKED. REMOVED AND REINSTALLED RETURN FILTER MODULE ON LT MLG WW IAW AMM 29-11-15-004-001 AND AMM 29-11-15-404-014, REPAIR CONTROLLED IN T2611873551, NO LEAK DETECTED. R & R A Aug 14, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026081718650Torque Box · dentedRT VERTICAL STAB EXTERNAL SURFACE OF LWR TORQUE BOX SKIN FROM FSS 92.250-FSS 270.784 HAS NUMEROUS DENTS (APPROX 100+). VERTICAL STAB RH VERTICAL TORQUE BOX PANEL. REMOVED AND REPLACED 175N2001U4 TORQUE BOX PANEL COMMON TO NETIO RT STAB IAW SRM 51-40-02-OG.Aug 13, 2026 · N12125 · Boeing 757224 · Vertical Stabilizer Miscellaneous StructureSDR CALA2026081718648Plate · crackedLOWER LT WING FASTENER HOLE NR 370 HAS A CRACK INDICATION (1E A) INSIDE THE 1ST LAYER OF THE HOLE AT THE 6 O'CLOCK POSITION, REMOVED AND REPLACED PLATE ASSY AF LWR LT WING SKIN IAW SRM 51-40-02-0G-0 AND DWG 757-3400.Aug 13, 2026 · N12125 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026081418587Strap · crackedAFTER REMOVAL OF SHROUD PANEL AT AFT CARGO, FOUND A CEILING STRAP CRACKED AT BS 1460, RT SIDE. REPAIRED IAW SRM 53-00-51-2R-12, NOTE A, DET 1 IAW SRM 51-40-02-0G.Aug 12, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026081418585Angle · crackedCARGO COMPT CEILING STRAP AT BS 1580-1600 BL0 CRACKED. R & R 146N5180U59, BATCH 0004502013 CEILING ANGLE COMMON TO BS 1580 - 1600, BL 0 IAW SRM 51-40-02.Aug 11, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026081218512Support Bracket · crackedLEFT MLG WHEEL WELL, AFT BULKHEAD BS 1180 LOWER SECTION LBL12, SUPPORT BRACKET CRACKED. REMOVED AND REPLACED CHANNEL ON LT MLG WHEEL WELL AFT BULKHEAD IAW SRM 51-90-02-0G-0 AND DWG 199N2503.Aug 11, 2026 · N12125 · Boeing 757200 · Fuselage Miscellaneous StructureSDR CALA2026081218510Support Bracket · crackedRIGHT MLG WHEEL WELL, AFT BULKHEAD BS 1180 LOWER SECTION, RBL 12, SUPPORT BRACKET CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-40-02-OG-0, AND DWG 144N 2503.Aug 11, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026081718646Skin · crackedLEFT WING LEADING EDGE SLAT NR 2, LOWER SKIN HAS A CRACK, AT 31 INCH. FROM THE INBD EDGE. REMOVED, FABRICATED, AND INSTALLED COVE SKIN ON LT WING L/E SLAT NR 2 IAW SRM 51-40-05-06-0, SRM 51-9 0-02-0G-0, AND DWG 114N4076. REF: 17347.Aug 9, 2026 · N12125 · Boeing 757224 · Leading Edge DevicesSDR CALA2026080918408Skin · corrodedEXTERNAL FUSELAGE, APU INLET CUTOUT EXTERNAL, HAS EVIDENCE OS CORROSION AT BS 1825, S6R AND BY BS 1787, S3R. PERFORMED REPAIR AT APU INLET CUTOUT STA 1825 IAW SRM 5 3-80-15-2R-1, REPLACED FWD STRAP AT BS 1787 BTW S3-6R, 2 EA SUPPORT ANGLES BTW BS 1825 - 1787Aug 9, 2026 · N12125 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2026080718351Retainer · crackedRIGHT MLG WHEEL WELL AT BS 1094.2, RBL 72.5, SEAL RETAINER BRACKET CRACKED. DRAWING 149N7552 WAS REF, REMOVED SEAL RETAINER BRACKET & SEAL RETAINER ANGLE AT RT MLG WHEEL WELL BS 1094.2 RBL 72.5 IAW SRM 51-40-02-0G-0, RECEIVED NEW PART BRACKET. LOCATED & Aug 6, 2026 · N12125 · Boeing 757224 · Fuselage Main, StructureSDR CALA2026080518319Intercostal · corrodedAFT CARGO COMPARTMENT RT SIDE BTWN BS 1540 - 1560, STRG 27 - 28 UNDER SIDE PANEL INTERCOSTAL CHORD IS CORRODED. REMOVED AND REPLACED INTERCOSTAL CHORD AT AFT CARGO BAY RT SIDE BTWN BS 1540 - 1560, STR 27 - 26 UNDER SIDE PANEL IAW SRM 51-40-02-0G-0, SRM 51-40Aug 5, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026080418268Bracket · crackedRIGHT MLG WW DOOR CLOSE SENSOR BRACKET CRACKED, BS 1040. REMOVED AND INSTALLED A NEW SENSOR BRACKET IAW SRM 51-40-02 & DWG 284N1643-24.Aug 3, 2026 · N12125 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2026080318221Bracket · crackedLEFT WHEEL WELL, MLG DOOR CLOSED SENSOR BRACKET IS CRACKED. REMOVED & REPLACED 284N1643-23 LT WHEEL WELL MLG DOOR CLOSED SENSOR BRACKET IAW SRM 51-40-02-0G.Aug 2, 2026 · N12125 · Boeing 757224 · Fuselage Main, Attach FittingsSDR CALA2026080218182Skin · crackedAFT CARGO DOOR SKIN: LWR FWD DOOR SKIN CRACKED, MEASURES .125" LONG EXTENDS .050" INTO PANEL FROM EDGE. REMOVED THE CRACK DAMAGE ON LWR FWD CORNER AFT CARGO DOOR SKIN MATERIAL REMOVED .800 X .050 O/T EDGE OF PART IN LIMITS IAW SRM 51 -30-01-1A-1 DET VIII T9Jul 31, 2026 · N12125 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA2026080218180Skin · damagedAFT CARGO DOOR FWD LWR EDGE OF EXTERNAL SKIN DAMAGED. PERFORMED PERMANENT REPAIR ON AFT CARGO DOOR FWD LWER EDGE. REMOVED DAMAGE 1 EACH LOCATIONS. 1) L= .400 D= .090" (WIDTH) IAW SRM 52-30-01-A-1.Jul 31, 2026 · N12125 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA2026031714610Charger · inoperativeEMERGENCY LIGHTS OPS TEST WITH THE TEST SWITCH PROCEDURE, FOUND EMERGENCY LIGHT INOP AT SEAT 27ABC OVERHEAD BIN, RELAMPED, NO HELP IAW AMM 33-51-00 NO. TWO ADJACENT (OPPOSITE SIDE) LIGHT ASSEMBLIES ARE INOPERATIVE ONLY SEAT 27ABC. APPLYING MEL 3351A APPROMar 10, 2026 · N12125 · Boeing 757224 · Emergency LightingSDR CALA2025082508088Oven · dirtyODOR ONLY HAPPENED IN COCKPIT, NO ODOR IN CABIN. ONCE IN CRUISE FOR 15-20 MINS & ONCE ON DESCENT FOR 15-20 MINUTES..ODOR WENT AWAY BOTH TIMES SDR REPORTABLE DISCREPANCY TROUBLESHOOTED AIR CONDITIONING SYSTEM IN REF WITH FIM TASK 21-00-01/301 STEP 3 PROCEDURE 1Aug 23, 2025 · N12125 · Boeing 757224 · Buffet/GalleysSDR CALA2025040303497Skin · gougedFOR THE INTERIM REPAIR AT RH WING LOWER SKIN EDGE GOUGE DAMAGE AT WSTA 585, ACCOMPLISH PERMANENT REPAIR PER PART 3 OF THE LATEST REVISION OF ECRA #: 5720-03512 ON OR BEFORE 30-SEPT-2026. FOR THE INTERIM REPAIR AT RH WING LOWER SKIN EDGE GOUGE DAMAGE AT WSTA 58Mar 31, 2025 · N12125 · Boeing 757224 · Wing, Plate/SkinSDR CALA2025032703253Skin · damagedL1 DOOR CUTOUT MOD. THERE ARE DISCREPANCIES BETWEEN THE INSTALLATION DRAWING AND ACTUAL FASTENER LOCATIONS FOUND DURING LAYOUT OF DOUBLER AND TRIPLER. L1 DOOR SURROUND - REPAIR / PREVENTATIVE MODIFICATION PER EA 5330-04213 AND ECRA 5330-07490 VERIFIED L1 DOOR Mar 25, 2025 · N12125 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2025013002133Door · fod1R DOOR WILL NOT ARM REMOVED FOD, DOOR ARMS AND DISARMS NORMAL.Jan 27, 2025 · N12125 · Boeing 757224 · Service DoorsSDR CALA2025010601785Line · crackedENG OIL PRESS RIGHT ECIAS MESSAGE AT CRUISE PER QRH THE RIGHT E NGINE WAS SHUTDOWN ADDED 21 QTS OF ENGINE OIL TO THE #2 ENGINE. CLEANED AREA AND DRY MOTORED THE #2 ENGINE TO VERIFY OIL LEAK. FOUND THE #2 ENGINE OIL PRESSURE TRANSMITTER BRAIDED OIL LINE STREAMJan 5, 2025 · N12125 · Boeing 757224 · Turbine Engine Oil SystemSDR CALA2024121901584Girt Bar · fodDOOR 4L TOMC REQUEST TO REMOVE DOOR SLIDE BUSSEL AND INSPECT ALL MECHANISMS AND INSTALLATIONS FOR DEFECTS. REF FUP 3198159 GAINED ACCESS TO ARMING/DISARMING LEVER & ITS ASSOCITED LINKAGES FOR DETAILED INSP REF AMM 25-66-10. FOUND NO LOOSE HARDWARE, BENT/BINDINDec 16, 2024 · N12125 · Boeing 757224 · Emergency EquipmentSDR CALA2024121701550Slider · icedDOOR 4R DOES NOT APPEAR TO FULLY SEAT IN DISARM POSITION REMOVED BUSSEL. ICE BUILDUP ON GIRT BAR SLIDERS MELTED IN A FEW MINUTES. DOOR DISARMED FULLY.OPENED DOOR. CLEANED DOOR SILL AREA. CLOSED DOOR. VARIFIED GIRT BAR SLIDERS FULLY ENGAGE IN ARMED. INSTALLED BDec 15, 2024 · N12125 · Boeing 757224 · Service DoorsSDR CALA2024100402557Circuit Breaker · inoperativeEICAS CONT PNL CAUTION ON TO PAST 100KTS. REF FOUND C/B POPPED 115 VAC BUS R SECT 2 ON P32 PANEL. PERFORMED BPCU BITE PROCEDURE IN REFERENCE TO B757 FIM 24-20 FAULT TREE 801 BPCU BITE SHOWED NO EXISTING FAULTS OR FAULTS FOR THE INBOUND LEG REST BREAKER WITH EXOct 2, 2024 · N12125 · Boeing 757224 · Electrical Power SystemSDR CALA2024072400277Light · intermittentAUTO LIGHT IN LAV 1L INTERMITENT REQUIRES TOO MUCH FORCE WHEN LOCKING DOOR TO TURN ON SUSPECT DOOR SWITCH, AUX AND DOME LIGHT OPERABLE. APPROVED NEF 3320AS COMPLY WITH DDP. FOUND LIGHT IN LAV 1L AND LOCKING MECHANISM TO BE OPERATING NORMALLY.Jul 21, 2024 · N12125 · Boeing 757224 · Passenger Compartment LightingSDR CALA2023100302933Tank · fullFWD LAV NOT ENOUGH WATER SWIRAL IN FLUSH TO EMPTY WASTE LAVS SERVICED, OPS CHECKS GOOD. ALL SERVICEABLE LAVS DUMPED AND SERVICED. OPERATIONAL CHECK OK. VERIFIED MID LAV TANKS IS EMPTY PER MEL.Sep 29, 2023 · N12125 · Boeing 757200 · Waste Disposal SystemSDR CALA2023070502165Fastener · missingRIGHT WING LANDING LIGHT PANEL 611AB HAS 1 EA FASTENER MISSING. QC COMPLETING MATERIALS NEEDED FOR EPLACE.RECORDS UPDATE -- DC SPEED TAPE APPLIED, COMPLIED WITH EC/RA:#:3340-01562. ON WALK AROUND FOUND R WING LANDING LIGHT ACCESS PANEL 611AB MISSING 1 EA FASTEJul 4, 2023 · N12125 · Boeing 757224 · Wing StructureSDR CALA2022072501871None · missingTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/25/22.PANEL BELOW OVERHEAD BIN BY SEAT 2E FELL DOWN FILLER PANEL MISSING TABS. R/R 12 CLIPS, ALL OPS CHK OK.Jul 24, 2022 · N12125 · Boeing 757 · Cabin Equipment/FurnishingsSDR CALA2022051101198None · corrodedFWD CARGO LT TUNNEL LAV SERVICE PANEL HOUSING CORRODED AT DUCT A TTACH FLANGE. BS 700-720. TRANSCRIBED FROM HAECO NR 9284657. REMOVED AND REPLACED DOUBLER ONLAV SERVICE PAN BS700-720 PER B DWG 143N3412 REV G AND B757-200 SR, 51-40-02. HAECO GSO MECH V9 3500May 9, 2022 · N12125 · Boeing 737 · Fuselage Structure (General)SDR CALA2022051101197None · corroded(SUPPORT TASK) AFT PIT AFT ACCESSORY AREA, WASTE SERVICE PAN COR RODED AT UPPER SURFACE BETWEEN BS 1680 AND 1700 AND BETWEEN STRI NGER S-26R AND STRINGER S-29R. TRANSCRIBED FROM HAECO NR 928591 0. REMOVED AND REPLACE DOUBLERON WASTE SERVICE PAN BS1680-1700 S2May 9, 2022 · N12125 · Boeing 737 · Fuselage Main, StructureSDR CALA2022050901176Pressure Switch · unserviceable(B757-35-3-0009) PASSENGER OXYGEN SYSTEM, ALTITUDE PRESSURE SWIT CH FAILS OPS CHECK. TRANSCRIBED FROM HAECO GSO NRC 9285968May 7, 2022 · N12125 · Boeing 757200 · Oxygen SystemSDR CALA2022042501059Frame · misrepairedSUPPORT TASK, MAIN CABIN STA 760 L/H FUSELAGE FRAME AT FLOORBEAM HAS A DRILL START, TRANSCRIBED FROM HAECO GSO NRC 9285440 REPAIRED DRILL START ON MAIN CABIN STA 760 L/H FUSELAGE FRAME AT FLOORBEAM IAW UAL ECRA 5332-01026 AND HAECO REO-G23725, HAECO G SO MECH Apr 23, 2022 · N12125 · Boeing 757224 · Fuselage Main, Floor Beam
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