# Service difficulty reports: N33103

A list on [N33103](https://openairdocs.org/aircraft/N33103.md).

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

Page 1 of 2 · 99 reports

- [SDR CALA2026102120481](https://openairdocs.org/sdr/CALA2026102120481.md): Smoke Detector · false activation · Oct 19, 2026 · N33103 · Boeing 757224 · Smoke Detection
  > LAV SMOKE CAUTION MSG DURING DESCENT, PASSING 16000. NO SMOKE OBSERVED. AFT LT LAV. DEBRIEF CREW & THEY STATED DIDN'T SMELL OR SAW SMOKE IN CABIN OR LAV. AMBER CAUTION EICAS MSG & SMOKE DETECTOR CHIME CAME ON INFLIGHT & ON GROUND. VISUALLY INSPECTED SMOKE DE
- [SDR CALA2026102120486](https://openairdocs.org/sdr/CALA2026102120486.md): Access Door · missing · Oct 17, 2026 · N33103 · Boeing 757224 · Nacelle/Pylon, Main Frame
  > NR 1 ENG OIL FILLER ACCESS DOOR FOUND MISSING DURING WALK AROUND. THE OIL FILLER ACCESS DOOR WAS REPLACED IAW AMM 72-00-00, REV 141.
- [SDR CALA2026092119600](https://openairdocs.org/sdr/CALA2026092119600.md): Bleed Valve · faulted · Sep 18, 2026 · N33103 · Boeing 757224 · Compressor Bleed Valve
  > ENGINE EXCEED ON TAKE OFF N2 INDICATE 103. MAX THRUST TAKE OF EPR 1.75. EXCEEDANCE HAPPENED IN LOW SPEED ON TAKE OFF. BELOW 80 KTS. NO HOT BRAKES. ADD EMP:U374916 EXCEED RECORDED ON #1 ENG N2 103% FOR 8 SECONDS. RR ENGINEERING REQUESTED BVCU TEST FOR #1 ENG EX
- [SDR CALA2026072317959](https://openairdocs.org/sdr/CALA2026072317959.md): Wire Harness · faulted · Jul 20, 2026 · N33103 · Boeing 757224 · Turbine Engine System Wiring
  > RIGHT ENG STARTER CUTOFF MSG, RT ENG VALVE LIGHT FLASHING. RAN CHCKLST SPOKE TO FLIGHT CREW, AFTER TAKE OFF STARTER CUTOFF MSG AND VALVE LIGHT WAS FLASHING THE WENT AWAY. DURING CRUISE MSG AND LIGHT CAME BACK & STAYED FLASHING UNTIL CREW RAN CHECKLIST LIGHT
- [SDR CALA2026063017491](https://openairdocs.org/sdr/CALA2026063017491.md): Elec Connector · broken · Jun 30, 2026 · N33103 · Boeing 757224 · Light System Wiring
  > FOUND BROKEN CONNECTOR UNDER SEAT 2B ESCAPE PATH LIGHTING. FOUND CONNECTOR BROKEN UNDER SEAT 2B FOR THE ESCAPE PATH LIGHTING. REPLACED CONNECTOR IAW BRUCE WIRING DIAGRAM BR2013-P-757200-5 + SWPM 20-60-00 REPLACED CONNECTOR UNDER SEAT 2B FOR ESCAPE PATH LIGHT
- [SDR CALA2026063017472](https://openairdocs.org/sdr/CALA2026063017472.md): Skin · cracked · Jun 29, 2026 · N33103 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING FIX LE BETWEEN SLATS NR 1 & 2, THERE IS A 6" CRACKED. REPAIRED LT WING LE. SKIN BETWEEN SLATS NR 1 AND NR 2 IAW SRM 57-41-01-2R-1 AND SRM 51-70-04.
- [SDR CALA2026062217271](https://openairdocs.org/sdr/CALA2026062217271.md): Angle · corroded · Jun 22, 2026 · N33103 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFTER APU AIR INTAKE DOOR REMOVED. FOUND CORROSION AT LOWE R ANGLE. REMOVED AND REPLACED LOWER ANGLE AT APU AIR INLET DOOR CUTOUT IAW SRM 51-40-02.
- [SDR CALA2026062917403](https://openairdocs.org/sdr/CALA2026062917403.md): Strap · corroded · Jun 20, 2026 · N33103 · Boeing 757224 · Fuselage Main, Structure
  > EXTERNAL FUSELAGE RT SIDE CORROSION AROUND OF THE FWD FRAM E IN THE APU INLET DOOR. REMOVED STRAP AT STA 787.45 APU INLET CUTOUT AFTER BEEN FOUND OU T OF LIMITS AND REPLACED WITH NEW STRAP IAW SRM 51-40-02 AND SRM 53-80-02-1A-0 REMOVED AND REINSTALLED APU AI
- [SDR CALA2026061817173](https://openairdocs.org/sdr/CALA2026061817173.md): Strap · cracked · Jun 17, 2026 · N33103 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FUSELAGE INTERNAL STRAP ATTACHED TO FLOOR BEAM AT STA 377 LBL25 WITH CRACKS. NR#15759 ESFR ENTRY ONLY FOR REPLACED PART REPAIRED FLOOR BEAM STABILIZATION STRP STA 377.7 LBL 24.75 IAW B 757-200 SRM 53-00-51-2R-123 REPAIR 12 NR:9278890
- [SDR CALA2026042415704](https://openairdocs.org/sdr/CALA2026042415704.md): Girt Bar · fod · Apr 21, 2026 · N33103 · Boeing 757224 · Emergency Equipment
  > 4R DIFFICULTIES DISARMIN G REMOVED DEBRIS FROM GIRT BAR RECEPTACLE AT 4R DOOR, REF AMM 25-66-10. OPS SATIS. ADD EMP:U247336
- [SDR CALA2026012613246](https://openairdocs.org/sdr/CALA2026012613246.md): Toilet · odor · Jan 26, 2026 · N33103 · Boeing 757224 · Waste Disposal System
  > LAVATORY TOILET BOWL HAD A BAD ODOR AT L4 DOOR. AFT CABIN LAV K SERVICED. AFT LAV WITH FRESH DEGERM FLUID. NO LEAKS NOTED. ODOR ELIMINATED.
- [SDR CALA2025110410867](https://openairdocs.org/sdr/CALA2025110410867.md): Sensor · out of adjust · Nov 2, 2025 · N33103 · Boeing 757224 · Fixed Inner Doors
  > SENSOR ON TOP OF FLIGHT DECK DOOR NEEDS ADJUSTMENT. CAUSES DIFFICULTY OPE NING AND CLOSING. ADJUSTED MAGNETIC SENSOR TRAGET AND VERIFIED FWD ENTRY LIGHT CHECK GOOD, REF AMM 52-52-01-800-801-C10.
- [SDR CALA2025091608982](https://openairdocs.org/sdr/CALA2025091608982.md): Lamp · inoperative · Sep 15, 2025 · N33103 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - L4 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT AND OPS CHECK GOOD W/REF AMM 33-51-00.
- [SDR CALA2025070106124](https://openairdocs.org/sdr/CALA2025070106124.md): Fmc · faulted · Jun 29, 2025 · N33103 · Boeing 757224 · Flight Management Computing Hardware System
  > NO VERTICAL PATH OR FUEL OR TIME INFO AVAILABLE UPON DEPARTURE. AIRCRAFT 103 RETURNED TO SHANNON AFTER APPROX 1 HOUR OF FLIGHT. CAPTAIN REPORTED THAT ONCE THEY REACHED THEIR REQUIRED FLIGHT L EVEL HE NOTICED THAT THE VNAV WAS INOP (VERTICAL PATH). THE FUEL FLO
- [SDR CALA2025052704978](https://openairdocs.org/sdr/CALA2025052704978.md): Light · broken · May 26, 2025 · N33103 · Boeing 757224 · Emergency Lighting
  > DOOR 1R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, NO HELP. R/R LT ASSY REF AMM 33-51-06. OPC GOOD. NO FURTHER DEFECTS NOTED.
- [SDR CALA2025030502599](https://openairdocs.org/sdr/CALA2025030502599.md): Charger · inoperative · Mar 3, 2025 · N33103 · Boeing 757224 · Emergency Lighting
  > FORWARD RIGHT EMERGENCY SLIDE LIGHT INOP. RELAMPED AND STILL INOP, T/S TO FUSE BAD ON M730 BATTERY CHARGER BAD, REMOVED AND REPLACED SAME, P/N 2012-1, OPS CHKS GOOD.PARTS USED: 19-3351-3-0097, QTY:1
- [SDR CALA2025021402326](https://openairdocs.org/sdr/CALA2025021402326.md): Guide Arm · out of adjust · Feb 12, 2025 · N33103 · Boeing 757224 · Passenger/Crew Doors
  > L AFT ENTRY DOOR EICAS MSG AFTER TAKEOFF. HANDLE COULD NOT BE SE CURED. ADJUSTED GUIDE ARM REF.AMM 52-11-04-822-056 UP TO 6 E B5. VERIFIED ADJUSTMENT OF GUIDE ARM FROM STEPS 6.A THROUGH 6.E.B.5 REFERANCE AMM 52-11-04-822-056. OK TO CONTINUE. COMPLETED GUIDE AR
- [SDR CALA2025021102292](https://openairdocs.org/sdr/CALA2025021102292.md): Warning Message · false activation · Feb 9, 2025 · N33103 · Boeing 757224 · Door Warning System
  > L AFT ENT DOOR EICAS INFLIGHT. DOOR CLOSED AND LOCKED FROM INSIDE TESTED INTEGRITY OF L AFT ENTRY DOOR IAW AMM 52-11-00/501 NO DEFECTS NOTED, DOOR OP AS IT SHOULD.
- [SDR CALA2025020200263](https://openairdocs.org/sdr/CALA2025020200263.md): Pan · gouged · Feb 2, 2025 · N33103 · Boeing 757224 · Passenger/Crew Doors
  > GOUGE ON EXTERIOR DOOR 1L PAN STRUCTURE. REMOVED AND REPLACED PAN STRUCTURE ON EXTERIOR DOOR 1L IAW B757-200 SRM 51-40-02 AND DWG 141N6100.
- [SDR CALA2025013000243](https://openairdocs.org/sdr/CALA2025013000243.md): Pan · gouged · Jan 30, 2025 · N33103 · Boeing 757224 · Passenger/Crew Doors
  > GOUGE ON EXTERIOR DOOR 2L HANDLE PAN STRUCTURE. REMOVED AND REPLACED PAN HANDLE P/N 654N0243-44 ON L2 DOOR IAW B757-200 SRM 51-21-01 AND DWG 143N6100.
- [SDR CALA2025013000241](https://openairdocs.org/sdr/CALA2025013000241.md): Skin · cracked · Jan 30, 2025 · N33103 · Boeing 757224 · Leading Edge Devices
  > ON THE SLAT 1, NEXT TO THE AUXILARY TRACK HAS A CRACK. REMOVED AND REPLACED COVER SKIN AT LH WING SLAT #1 IAW B757-200 SRM 51-40-02.
- [SDR CALA2025012900232](https://openairdocs.org/sdr/CALA2025012900232.md): Pan · gouged · Jan 26, 2025 · N33103 · Boeing 757224 · Service Doors
  > EA 5210-03219- GOUGE ON EXTERIOR DOOR 4R HANDLE PAN STRUCTURE. N O DOT.
- [SDR CALA2025012700219](https://openairdocs.org/sdr/CALA2025012700219.md): Bracket · cracked · Jan 18, 2025 · N33103 · Boeing 757224 · Fuselage Main, Attach Fittings
  > B757-06-3-0238- RH, WW MLG, HYD PRESS FILTER MODULE BRACKET HAS A CRACK. REMOVED AND REPLACED BRACET AT RH WW MLG HYD PRESS FILTER MODULE IAW SRM 51-10-02 PARAGAPH 9 AND SRM 51-40-02 AND REMOVED AND RE PLACED RETURNED FILTER MODULE IAW B757 AMM 29-11-15-004-00
- [SDR CALA2025011700139](https://openairdocs.org/sdr/CALA2025011700139.md): Support Bracket · cracked · Jan 16, 2025 · N33103 · Boeing 757224 · Fuselage Miscellaneous Structure
  > B757-06-3-0238-RH WW MLG DOOR CUT-OUT FWD SIDE BULB SEAL BRACKET SUPPORT IS CRACKED AND DEFORMED.
- [SDR CALA2024102900947](https://openairdocs.org/sdr/CALA2024102900947.md): Pcb · faulted · Oct 27, 2024 · N33103 · Boeing 757224 · Flight Control System Wiring
  > REJECTED TAKE OFF DUE TO UNSCHED STAB TRIM EICAS MSG.AIRSPEED APROX 50 KTS RIGHT SAM MODULE HAS A SPM YELLOW BALL SHOWN, REPLACED RIGHT SPM CARD ASSY, GND TEST PASSED BUT YELLOW BALL DOES NOT DISAPPEAR. GND TEST OF RIGHT GPM WAS DONE PER AMM 27-48-03-424-009.
- [SDR CALA2024090502391](https://openairdocs.org/sdr/CALA2024090502391.md): Pin · pulled · Sep 4, 2024 · N33103 · Boeing 757200 · Life Raft
  > LIFE RAFT AT 7E ACTIVATION PIN PULLED. R & R LIFE RAFT AS REQUIRED.
- [SDR CALA2024080100344](https://openairdocs.org/sdr/CALA2024080100344.md): Idg · faulty · Jul 30, 2024 · N33103 · Boeing 757224 · AC Generator-Alternator
  > LEFT GEN OFF. RESET PER CHECKLIST AND GEN CAME BACK OFF AFTER RESETMX ENGINE IDLE RUN, FOUND L GENERATOR UNABLE TO ENGAGE, ATTEMPTS TO SWITCH TO L GEN POWER BUT KICKS BACK TO APU POWER AFTER A FEW SECONDS. PERFORMED BPCU BITE REF. FIM 24-20 FAULT TREE 801. M
- [SDR CALA2024071600202](https://openairdocs.org/sdr/CALA2024071600202.md): Wire · unsecure · Jul 14, 2024 · N33103 · Boeing 757224 · Light System Wiring
  > COACH CABIN, ALL FLOOR EMERGENCY PATH LIGHTS INOP. FOUND POWER SUPPLY M10919 SUPPLYING POWER TO ALL ROWS. FOUND WIRE L9043A18 FROM BATTERY M10699 STOWED BEHIND 12 ABC DADO PANEL. RE ROUTED TO 32ABC TO CONFORM TO DRAWING BR2013-P-7572C0-5 AND DRAWING BR2013-P
- [SDR CALA2024021600443](https://openairdocs.org/sdr/CALA2024021600443.md): Retainer · missing · Feb 14, 2024 · N33103 · Boeing 757224 · Passenger/Crew Doors
  > EXTREMLY LOUD SQUEAL / NOISE AT 2L DURING CLIMB. AT FL350 NOISE NOT AS LOUD BUT NON. DR #2LH, 3 FEET OF THE FWD LOWER DOOR LINER SEAL AND RETAINER ARE MISSING.REPLACED DOOR 2L LOWER DOOR LINER SEAL RETAINER AND LINER SEAL REF CMM52-11-15. CLOSED DOOR, PRESSUR
- [SDR CALA2023081102490](https://openairdocs.org/sdr/CALA2023081102490.md): Skin · unknown · Aug 9, 2023 · N33103 · Boeing 757224 · Trailing Edge Flaps
  > GENERATING ITEM EA5100-0234 REV E: REENFORCEMENT REPAIR FOUND ON LEFT WING OUTBOARD MAIN FLAP BOTTOM SIDE SKIN OUTBOARD AFT LOWER CORNER MEASURING APPROX. 10 INCHES BY 5 INCHES. FOUND REPAIR NOT MATCHING THE CURRENT SRM. B757 SRM-57-53-01-2R-4 AND PER PAGE 2 O
- [SDR CALA2022122303477](https://openairdocs.org/sdr/CALA2022122303477.md): Idg · faulted · Dec 23, 2022 · N33103 · Boeing 757224 · AC Generator-Alternator
  > RIGHT AC BUSS OFF EICAS, RIGHT AC MAIN BUSS IS NOT ENERGIZED RT AC BUSS OFF, RESET ONCE. AC BUSS OFF AGAIN 5 MIN LATER. RELATED NOTED FAULTS. PERFORMED BITE CHECK ON BPCU IAW FIM 24-20 TREE 801, FAULT NOTED ON RIGHT GEN POWER SYSTEM DP TRIP AND MAIN BUS/
- [SDR CALA2022062701594](https://openairdocs.org/sdr/CALA2022062701594.md): Cabin Air Sys · warning message · Jun 27, 2022 · N33103 · Boeing 757200 · Cabin Pressure Control System
  > AS SOON AS WE LEVELED OFF AT FL 350/ WE GOT CABIN ALT ALERT AND WARNING BELL. OBSERVED. EXCESSIVE CABIN PRESSURE LEAKAGE TEST CARRIED OUT, CABIN DIFFERENTIAL PRESSURE REACHED AND MAINTAINED 4.0PSI, NO LEAKS NOTED THROUGHOUT THE CABIN, ALL SYSTEMS FUNCTIONED AS
- [SDR CALA2022011700166](https://openairdocs.org/sdr/CALA2022011700166.md): Support · damaged · Jan 16, 2022 · N33103 · Boeing 757224 · Fuselage Structure (General)
  > SDR REQUIRED, FOR REPAIR AT STATION 1380 FRAME INNER CHROD AT S-27R REQUIRES REPAIR. SDR REQUIRED, REF LOG PAGE 7591125. TRANSCRIBED FROM HAECO LP 9287333. AT STA 1320 S-27R, REMOVED SUPPORT STRUCTURE FOR INNER CHORD AND RESTORED PROTECTIVE FINISH SUPPORT STRU
- [SDR CALA2022011700155](https://openairdocs.org/sdr/CALA2022011700155.md): Support · damaged · Jan 14, 2022 · N33103 · Boeing 757224 · Fuselage Main, Frame
  > TRANSCRIBED FROM HAECO GSO NR LP 9287333 B757-06-3-0244 STATION 1380 FRAME INNER CHROD AT S-27R REQUIRES REPAIR PER ECRA 5360-01624: "PERFORM AN INSPECTION PER THE LATEST REVIS ION OF ECRA 5360-01624 PART 2 ON OR BEFORE 22-MAY-2023" DIP INITIATED, PERFORM INSP
- [SDR CALA2022010500029](https://openairdocs.org/sdr/CALA2022010500029.md): Flap · chafed · Jan 4, 2022 · N33103 · Boeing 757200 · Trailing Edge Flaps
  > TRANSCRIBED FROM HAECO GSO TASK CARD 9286940: (SUPPORT TASK) RIG HT WING T/E I/B FWD FLAP L/E AREA HAS CHAFFING MARKS AS MARKED. MEASURED DAMAGE AREA ON THE I/B T/E FLAP L/E, ORIGINAL THICKNESS INSP QC418.055", LOWEST DEPTH.022", REMAINING.033" FOUND TO BE
- [SDR CALA2021121002316](https://openairdocs.org/sdr/CALA2021121002316.md): Floorbeam · corroded · Dec 10, 2021 · N33103 · Boeing 757200 · Fuselage Main, Floor Beam
  > TRANSCRIBED FROM HAECO GSO TASK CARD 9287218: (B757-53-3-0480) M AIN CABIN FLOOR STRUCTURE (AFT WET AREA), FWD FLANGE OF THE FLOO R BEAM CORRODED AT LOWER SURFACE AT BS 1681.8 APPROX LBL-11. ALL WORK COMPLETED ON NRC 9286698, SEE ATTACHED COPY. ALL CORROS ION
- [SDR CALA2021121002314](https://openairdocs.org/sdr/CALA2021121002314.md): Beam · corroded · Dec 8, 2021 · N33103 · Boeing 757200 · Fuselage Main, Floor Beam
  > TRANSCRIBED FROM HAECO GSO TASK CARD 9287219: (B757-53-3-0480) M AIN CABIN FLOOR STRUCTURE (AFT WET AREA), FWD FLANGE OF THE FLOO R BEAM HAS CORROSION BETWEEN THE FLOORBEAM AND THE WEB AT BS 168 1.8 APPROX LBL 52.5. ALL WORK COMPLETED ON NRC 9286698, SEE ATTAC
- [SDR CALA2021120602267](https://openairdocs.org/sdr/CALA2021120602267.md): None · corroded · Dec 6, 2021 · N33103 · Boeing 757200 · Fuselage Main, Plate/Skin
  > TRANSCRIBED FROM HAECO NR 9286539. B757-06-3-0244: AFT CARGO INT ERCOSTAL BETWEEN STA.1360-1380, STRINGER S26R-S27R CORRODED. TRANSCRIBED FROM HAECO NR 9286539.REMOVED CORRODED INTERCOSTAL IAW B757-200 SRM51-40-02. FABRICATED NEW INTERCOSTAL PER BAC DWG 146N32
- [SDR CALA2021120602265](https://openairdocs.org/sdr/CALA2021120602265.md): Fitting · corroded · Dec 6, 2021 · N33103 · Boeing 757200 · Fuselage Structure (General)
  > TRANSCRIBED FROM HAECO GSO NRC# 9286540--B757-06-3-0244: AFT CAR GO NET TIE DOWN FITTING JUST FWD OF STA 1380 ON R/H SIDE CORRODED. TRANSCRIBED FROM HAECO GSO NRC# 9286540. REMOVED CORRODED TIE SRM 51-40-02 AND BAC DWG 146N5390. DOWN FITTING IAW B757-2 SRM 51-
- [SDR CALA2021120602264](https://openairdocs.org/sdr/CALA2021120602264.md): Door · corroded · Dec 6, 2021 · N33103 · Boeing 757200 · Fuselage Main, Plate/Skin
  > TRANSCRIBED FROM HAECO NR 9286297. (B757-53-3-0526) AFT CARGO COMPARTMENT DOOR SURROUNDING SUPPORT STRUCTURE - INTERCOST AL TO FORWARD FRAME 1380 ATTACH BRACKET EXFOLIATED. STREAMER FS 1360- FS 1380, STR S25R STR S26R. TRANSCRIBED FROM HAECO NR 9286297. REMOVE
- [SDR CALA2021120602260](https://openairdocs.org/sdr/CALA2021120602260.md): Floor Mat · corroded · Dec 6, 2021 · N33103 · Boeing 757200 · Fuselage Main, Plate/Skin
  > TRANSCRIBED FROM HAECO GSO TASK CARD 9286698--SUPPORT TASK CBN F LOOR SHEAR WEB CORRODED BS 1681 BL LBL-0 REMOVED CORROSION IAW B757-2 SRM 53-60-51 AT STA 1681 LBL 10-55 REPAIR III. REF HAECO GSO MECH V933620 INSP QC418 ORIGINAL MATERIAL THICKNESS.156, REMOV
- [SDR CALA2021120602259](https://openairdocs.org/sdr/CALA2021120602259.md): Angle · elongated · Dec 6, 2021 · N33103 · Boeing 757200 · Fuselage Main, Structure
  > TRANSCRIBED FROM HAECO GSO NRC# 9287273: SUPPORT TASK- MAIN CABI N STA 295-430 LBL65 CREASE BEAM ANGLE HAS ELONGATED AND OVERSIZE D ATTACHMENT HOLES. REMOVED AND REPLACED CREASE BEAM ANGLE FROM STA 295 TO 430 LBL-6 5 IAW B757-2 SRM 51-40-02 AND DWG# 141N8322 R
- [SDR CALA2021120202237](https://openairdocs.org/sdr/CALA2021120202237.md): Intercostal · corroded · Dec 1, 2021 · N33103 · Boeing 757200 · Fuselage Main, Plate/Skin
  > TRANSCRIBED FROM HAECO NR 9286539. B757-06-3-0244: AFT CARGO INT ERCOSTAL BETWEEN STA.1360-1380, STRINGER S26R-S27R CORRODED. TRANSCRIBED FROM HAECO NR 9286539.REMOVED CORRODED INTERCOSTAL IAW B757-200 SRM51-40-02. FABRICATED NEW INTERCOSTAL PER BAC DWG 146N32
- [SDR CALA2021120202236](https://openairdocs.org/sdr/CALA2021120202236.md): Bracket · none · Dec 1, 2021 · N33103 · Boeing 757200 · Fuselage Main, Plate/Skin
  > TRANSCRIBED FROM HAECO NR 9286297. (B757-53-3-0526) AFT CARGO COMPARTMENT DOOR SURROUNDING SUPPORT STRUCTURE - INTERCOST AL TO FORWARD FRAME 1380 ATTACH BRACKET EXFOLIATED. STREAMER FS 1360- FS 1380, STR S25R STR S26R. TRANSCRIBED FROM HAECO NR 9286297. REMOVE
- [SDR CALA2021120102203](https://openairdocs.org/sdr/CALA2021120102203.md): Web · none · Nov 29, 2021 · N33103 · Boeing 757200 · Fuselage Miscellaneous Structure
  > TRANSCRIBED FROM HAECO GSO NRC# 9287422: SUPPORT TASK- L-1 DOOR THRESHOLD WEB STA 345-365 HAS EXISTING DOUBLE DRILLED HOLES. REMOVED AND REPLACED L-1 DOOR THRESHOLD WEB IAW B757-200 SRM 51-40-02 AND DWG #141N8422-50 REV-R.
- [SDR CALA2021120102202](https://openairdocs.org/sdr/CALA2021120102202.md): Channel · corroded · Nov 29, 2021 · N33103 · Boeing 757200 · Passenger/Crew Doors
  > TRANSCRIBED FROM HAECO GSO NRC 9287089: B757-53-3-0550- L1 DOOR SILL INBOARD ATTACH POINT UNDER SIDE HAS CORROSION. REMOVED CORROSION IAW B757-2 SRM 51-10-02. ORIG MAT.050 PER BAC V901427, INSP QC418 DWG 141N8322. MAT REMOVED.028, MAT REMAINING.022 IS OUT O
- [SDR CALA2021120102200](https://openairdocs.org/sdr/CALA2021120102200.md): Web · corroded · Nov 29, 2021 · N33103 · Boeing 757200 · Fuselage Miscellaneous Structure
  > TRANSCRIBED FROM HAECO GSO NRC# 9287336: SUPPORT TASK- MAIN CABI N STA 377-395 LBL60 AT CUSP WEB HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW B757-2 SRM 51-10-02. ORIG MAT.040 PER BAC REV F. REF HAECO GSO MECH V901427 INSP QC418 DWG 141N8322 REV F.
- [SDR CALA2021120102199](https://openairdocs.org/sdr/CALA2021120102199.md): Angle · none · Nov 29, 2021 · N33103 · Boeing 757200 · Fuselage Main, Structure
  > TRANSCRIBED FROM HAECO GSO NRC# 9287273: SUPPORT TASK- MAIN CABI N STA 295-430 LBL65 CREASE BEAM ANGLE HAS ELONGATED AND OVERSIZE D ATTACHMENT HOLES.
- [SDR CALA2021120102198](https://openairdocs.org/sdr/CALA2021120102198.md): Web · none · Nov 29, 2021 · N33103 · Boeing 757200 · Fuselage Main, Structure
  > TRANSCRIBED FROM HAECO GSO NRC# 9287537: SUPPORT TASK- THE CREAS E WEB BETWEEN STA 395 AND 410 LBL65 HAS ELONGATED AND OVERSIZED HOLES. REMOVED AND REPLACED CREASE WEB FROM STA 395 TO STA 410 LBL-65 I AW B757-2 SRM 51-40-02 AND DWG 141N8322 REV F. REF HAECO G
- [SDR CALA2021111702119](https://openairdocs.org/sdr/CALA2021111702119.md): Skin · dented · Nov 16, 2021 · N33103 · Boeing 757200 · Fuselage Main, Structure
  > TRANSCRIBED FROM HAECO GSO NR 9287125 B757-06-3-0253: DENT AT LH STA 640 STR 14L REQ EVAL REPAIR AREA PER EC/RA # 5331-02779. PLANNING TO CONTACT EG AFTER FLIGHT CYCLES. HAECO GSO MECH V932840 47,000 BUT BEFORE 48,000 AIRCRAFT TOTAL FLIGHT CYCLES AND REUES T T

Next page: https://openairdocs.org/aircraft/N33103/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N33103' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N33103/reports

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