# Service difficulty reports: N41135

A list on [N41135](https://openairdocs.org/aircraft/N41135.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 · 89 reports

- [SDR CALA2026102120503](https://openairdocs.org/sdr/CALA2026102120503.md): Support · cracked · Oct 18, 2026 · N41135 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LEFT MLG WW, FWD SEAL RETAINER, SUPPORT FRAME OTBD END CRACKED. REMOVED AND REPLACED THE SEAL RETAINER SUPPORT IAW SRM 51-40-02-OG-0. REMOVED AND REINSTALL FOR ACCESS FOR ACCESS PANEL 197BL AND PANEL IAW AMM 53-66-01-404-005.
- [SDR CALA2026102120501](https://openairdocs.org/sdr/CALA2026102120501.md): Guide Arm · cracked · Oct 18, 2026 · N41135 · Boeing 757224 · Service Doors
  > INSPECT ALL MAIN CABIN ENTRY DOORS FOR GUIDE ARM SECURITY. PERFORMED INSPECTION ON ALL MAIN CABIN ENTRY DOORS (L1, R1,L2, L4, & R4) GUIDE ARMS BRACKET BOLTS IAW AMM 52-11-04-402- 037 AND AMM 20-11-00-912-001 T97605, T97654. WC: 20026.
- [SDR CALA2026101920437](https://openairdocs.org/sdr/CALA2026101920437.md): Oven · dirty · Sep 22, 2026 · N41135 · Boeing 757224 · Buffet/Galleys
  > GALLEY WARMING OVEN SMOKING OR SPARKING IN THE AFT GALLEY. SMOKE AFTER APPROX 5 MIN DEBRIEFED CREW AND CREW STATED WHILE COOKING MEALS AT NR 3 OVEN OF AFT GALLEY, OVEN STARTED SMOKING. DID NOT SMELL LIKE ELECTRICAL SMOKE. SUSPECT FOOD BURNING CAUSED SMOKE. OV
- [SDR CALA2025120711821](https://openairdocs.org/sdr/CALA2025120711821.md): Oven · dirty · Dec 6, 2025 · N41135 · Boeing 757224 · Buffet/Galleys
  > AFT OVENS 411 AND 412 PRODUCED EXCESSIVE SMOKE OR STEAM MID COOK ING CYCLE CONFIRMED WITH CREW, VERIFIED AFT GLLY OVENS SMOKED DUE EXCESS WATER AND PLASTIC. CLEANED 412 OK, 411 SMOKES, MEL L/P 7197105 CHECKED COFFEEMAKERS, CB'S, GLLY EQUIP ALL OK. AIRED OUT GA
- [SDR CALA2025070806343](https://openairdocs.org/sdr/CALA2025070806343.md): Battery Pack · no test · Jul 7, 2025 · N41135 · Boeing 757224 · Emergency Lighting
  > SEAT ENDCAP EMERGENCY LIGHTS INOP, FROM SEAT 32BC THRU 41ABC. REMOVED AND REPLACED (FUSE) ON BATTERY PACK (M737) IAW BOEING 75 7-200 AMM 33-51-07-962-071. TEST IS GOOD.
- [SDR CALA2025070806342](https://openairdocs.org/sdr/CALA2025070806342.md): Battery Pack · inoperative · Jul 7, 2025 · N41135 · Boeing 757224 · Emergency Lighting
  > MAIN CABIN EMERGENCY EXIT SIGN BTW L4 AND R4 DOOR ARE NOT WORKING. REMOVED AND REPLACED ON (FUSS) MAIN CABIN EMERGENCY BATTERY PAC K (M736) IAW BOEING 757-200 AMM 33-51-07-962-071 TEST IS GOOD.
- [SDR CALA2025070706278](https://openairdocs.org/sdr/CALA2025070706278.md): Bulb · burned out · Jul 6, 2025 · N41135 · Boeing 757224 · Emergency Lighting
  > L-2 DOOR EMERGENCY LIGHTS INOP L-2 DOOR LIGHT INOP.
- [SDR CALA2025070706277](https://openairdocs.org/sdr/CALA2025070706277.md): Elec Connector · unsecure · Jul 6, 2025 · N41135 · Boeing 757224 · Emergency Lighting
  > OVERHEAD BINS 7 DEF, 34 DEF, 1 FE EMERGENCY LIGHTS INOP STE N/R 129622. TIGHTEN CONNECTION AND OPS CHECKS WERE GOOD PER 33-51-07-862-004
- [SDR CALA2025070706276](https://openairdocs.org/sdr/CALA2025070706276.md): Elec Connector · unsecure · Jul 6, 2025 · N41135 · Boeing 757224 · Light System Wiring
  > R-2 DOOR EMERGENCY LIGHTS INOP CONNECTION WAS SECURED AND OPS CHECKS OF LIGHTS WERE GOOD PER 33-57-07-862-034. R-2 DOOR EMERGENCY LIGHTS INOP CONNECTION WAS SECURED AND OPS CHECKS OF LIGHTS WERE GOOD PER 33-57-07-862-034 REF STE N/R 129621.
- [SDR CALA2025070706275](https://openairdocs.org/sdr/CALA2025070706275.md): Bulb · burned out · Jul 6, 2025 · N41135 · Boeing 757224 · Emergency Lighting
  > AISLE PATH LIGHTS FROM SEAT 31 AFT ARE INOP. REPLACED BULB PER 33-51-03-002-001 OPS CHECKS GOOD.
- [SDR CALA2025070706274](https://openairdocs.org/sdr/CALA2025070706274.md): Bulb · burned out · Jul 6, 2025 · N41135 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 3 AB END CAP IS INOP SDR REPORTING REPLACED LIGHT AT SEAT 3AB PER 33-51-11-403-036, OP CHECKS GOOD.
- [SDR CALA2025070706269](https://openairdocs.org/sdr/CALA2025070706269.md): Light · damaged · Jul 3, 2025 · N41135 · Boeing 757224 · Door Warning System
  > DURING REMOVAL OF L-1 DOOR FRAME LINER WAS FOUND INDICATOR LIGHT L00403 WITH CONTACT DAMAGED. FOUND PER EA 5330-04213. LIGHT WAS REPLACED ON STE 128718.
- [SDR CALA2025070706268](https://openairdocs.org/sdr/CALA2025070706268.md): Mount · corroded · Jul 3, 2025 · N41135 · Boeing 757224 · Wing, Control Surface Attach Fittings
  > ROB #6 TE FLAP TRANSMISSION MOUNTING PLATE TO BE INSTALLED TO AC 0124 (PN 113N1249-10). DURING ROB REMOVAL OF #6 TE FLAP TRANSMISSION MOUNTING PLATE, CORROSION FOUND ON #6 TE FLAP TRANSMISSION MOUNTING PLATE. ROB CANCELLED. ADD EMP:V940938 (SDR) REMOVED AND RE
- [SDR CALA2025070706267](https://openairdocs.org/sdr/CALA2025070706267.md): Bracket · corroded · Jul 3, 2025 · N41135 · Boeing 757224 · Aerodynamic Fairings
  > FUSELAGE UPPER AREA IN AREA OF LIVETV FARING/RADOME HAVE S ERVERAL SPOTS OF EVIDENCE OF CORROSION. REPAIR WAS PERFORMED ON FUSELAGE UPPER AREA OF LIVETV FARING RAD OME IAW WORK PER EC/RA #5330-07557 AND EA 757-4434-13- A3968 REV-.
- [SDR CALA2025070706265](https://openairdocs.org/sdr/CALA2025070706265.md): Skin · cracked · Jul 3, 2025 · N41135 · Boeing 757224 · Leading Edge Devices
  > LH WING #2 SLAT OUTBD INNER WALL S KIN CRACK. 16-23 (NRC:128561) ESFR COMPLETED. REMOVED AND REINSTALLED SLAT #2 AS PER B757 AMM 27-81-02-424-021, TEST SATISFACTORY, REMOVED AND REPLACED NEW COVER SKIN IAW SRM 51-40-02-0G-0. REF: NR 128561.
- [SDR CALA2025070706262](https://openairdocs.org/sdr/CALA2025070706262.md): Stringer · damaged · Jul 3, 2025 · N41135 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT. FR 1520 S27R HAS FREE FLANGE AREA WITH DRILLED HOLE. REPAIR WAS PERFORMED ON AFT CARGO COMP FR 1520 R/SIDE STR 27 IAW WORK PER UAL EC/RA:5360-01977 AND VT MAE EA 757-5360-13-A3993 R EV-
- [SDR CALA2025070706261](https://openairdocs.org/sdr/CALA2025070706261.md): Stringer · damaged · Jul 2, 2025 · N41135 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT. FR 1500 R/SID E STRG 27 HAS FREE FLANGE AREA WITH DRILLED HOLE. REPAIR WAS PERFORMED ON AFT CARGO COMP FR 1500 R/SIDE STR 27 IAW WORK PER UAL EC/RA:5360-01976 AND VT MAE EA 757-5360-13-A3989 RE V-. REF: NR 128606.
- [SDR CALA2025070706260](https://openairdocs.org/sdr/CALA2025070706260.md): Panel · worn · Jul 2, 2025 · N41135 · Boeing 757224 · Wing, Plate/Skin
  > L/H WING PANEL S521UBX. PANEL CUT OUT AT INBD LA TCH AREA LAND STRUCTURE WORN. REPAIR WAS PERFORMED ON LH WING L/E PANEL 521UBX, PANEL CUTOUT A T INB IAW WORK PER UAL EC/RA#:5740-03399 AND VT MAE EA 757-5740- 13-A3987 REV- AND SRM 51-40-02-0G-0.
- [SDR CALA2025070206140](https://openairdocs.org/sdr/CALA2025070206140.md): Skin · cracked · Jul 1, 2025 · N41135 · Boeing 757224 · Leading Edge Devices
  > CRACK ON AFT INNER SKIN SLAT 10 NEAR ACCESS 625 CB RIGHT WING. REMOVED AND REINSTALLED LE SLAT #10 AS PER AMM TASK 27-81-0 2-424-021, TEST SATISFACTORY, REPLACED 2 E/A COVERED SKIN IAW B757 SRM 51-40-02-0G, ADJUSTED SLAT NR 10 PER B757 AMM TASK 27-81-02 -424-
- [SDR CALA2025070206139](https://openairdocs.org/sdr/CALA2025070206139.md): Skin · cracked · Jul 1, 2025 · N41135 · Boeing 757224 · Leading Edge Devices
  > CRACK ON AFT SKIN SLAT #9 NEAR ACCESS 624CB. REMOVED AND REINSTALLED LE SLAT #9 AS PER B757 AMM TASK 27-81-02 -424-021, TEST SATISFACTORY, SKIN OF SLAT #9 WAS REPLACED IAW B7 57 SRM 51-40-02.
- [SDR CALA2025063006073](https://openairdocs.org/sdr/CALA2025063006073.md): Access Door · corroded · Jun 28, 2025 · N41135 · Boeing 757224 · Fuselage Main, Plate/Skin
  > (SDR) EXFOLIATION CORROSION ON PANEL 121AL (LAVATORY SERVICE) LW R NEAR LATCHES. REMOVED AND REPLACED PANEL ASSY DOOR 121AL P/N 143N3411U126 ON L AVATORY SERVICE IAW B757-200 SRM 51-40-02-06-0 AND DWG 143N3411 CLEANED AREA PAN IAW SOPM 20-30-03 AND RESTORED
- [SDR CALA2025063006064](https://openairdocs.org/sdr/CALA2025063006064.md): Bracket · cracked · Jun 27, 2025 · N41135 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FWD CARGO, BETWEEN STA.845 TO STA.879, RH SIDE AIR FILTER, STRUCTURE, FWD/LOWER BRACKET SUPPORT IS DEFORMED. SDR REPROTING PURPOSE ONLY STRAIGHTENED RH SIDE AIR FILTER STRUCTURE IAW BAC 5300-2 AND PERF ORMED HFEC ON AREA, CRACK FOUND, CRACKED BRACKET WAS REMOV
- [SDR CALA2025070706256](https://openairdocs.org/sdr/CALA2025070706256.md): Frame · dented · Jun 26, 2025 · N41135 · Boeing 757224 · Fuselage Main, Frame
  > AFT CARGO COMPT. FR1280 L/SIDE BTWN STRG 26/27 FREE FLANGE HAS DENT. REPAIR WAS PERFORMED ON AFT CARGO COMP FR 1280 LH SIDE BETWEEN STA 26LH TO STA 27LH IAW WORK PER UAL EC/RA# 5360-01981 AND VTMA E EA 757-5360 13-A3960 REV - LP:5266904 RII VERIFIED PERFORME
- [SDR CALA2025063006060](https://openairdocs.org/sdr/CALA2025063006060.md): Web · cracked · Jun 26, 2025 · N41135 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FWD CARGO, BETWEEN STA.84 5 TO STR. 879, RH SIDE, AIR FILTER, BASE OF THE STRUCTURE, AFT E DGE HAS CRACK. REMOVEFD AND REPLCED NEW WEB P/N 214N5020-26 ON SUPPORT ISNT MIX BAY RECIRCULATE, FWD CARGO COMP BETWEEN STA 845 TO STA 878 SIDE RH SRM 51-40-02-06-0 AN
- [SDR CALA2025063006059](https://openairdocs.org/sdr/CALA2025063006059.md): Web · cracked · Jun 26, 2025 · N41135 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FWD CARGO, BETWEEN STA. 845 TO STA 879, RH SIDE, AIR FILTER, TOP STRUCTURE IS DEFORMED. REMOVED AND REPLACED NEW WEB P/N 214N5020-26 ON FWD CARGO COMP B ETW STA 845 TO STA 879, RH SIDE, AIR FILTER, TOP STRUCTURE IAW SRM 51-40-02-0G-0 AND DWG 214N5020 AND RES
- [SDR CALA2025063006058](https://openairdocs.org/sdr/CALA2025063006058.md): Seat Track · corroded · Jun 26, 2025 · N41135 · Boeing 757224 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED OUT OF LIMIT SET TRACK LBL 24.75 FROM STATION 1080 TO 1200. SEAT TRACK LBL 24.75 FROM STA 1080 TO STA 1200 WAS REMOVED AND R EPLACED IAW B757-200 SRM 51-40-02-0G, SRM 53-40-52-01-1 AND AMM 20-11-00.
- [SDR CALA2025063006057](https://openairdocs.org/sdr/CALA2025063006057.md): Seat Track · corroded · Jun 26, 2025 · N41135 · Boeing 757224 · Fuselage, Seat/Cargo Attach Fittings
  > OUT OF LIMIT SEAT TRACK LBL 45.5 FROM STATION 900 TO 1200. SEAT TRACK LBL 45.5 FROM STA 900 TO STA 1200 WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G, SRM 53-40-52-01-1, 53-00-52-2 R AND AMM 20-11-00. TR:T87303.
- [SDR CALA2025062605903](https://openairdocs.org/sdr/CALA2025062605903.md): Skin · cracked · Jun 23, 2025 · N41135 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING, LE I/B-LOWER SIDE OF THE GAP PANEL HAS A CRACK. REMOVED SKIN IAW B757-200 SRM 51-40-02, FABRICATED NEW PART GAP PANEL IA SRM 57-41-01-01-01, LOCATED AND DRILLED IAW SRM 51-40-0 2-0G-, REMOVED FASTENERS FOR ACCESS IAW SRM 51-40-02-0G-0, INSTA LLED
- [SDR CALA2025062605901](https://openairdocs.org/sdr/CALA2025062605901.md): Floor Support · cracked · Jun 23, 2025 · N41135 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT. BTWN STA 1580-1600 BL 0 CEILING AREA HAS FLOOR SUPPORT ANGLE WITH CRACK. REMOVE SUPPORT ANGLE PER SRM 51-40-02-0G. FAB AND HEAT TREAT ANG LE ON VT MAE TRAVELER T2511816123 INSTALL NEW ANGLE PER SRM 51-4 0-02 LP#: 5291831
- [SDR CALA2025062605897](https://openairdocs.org/sdr/CALA2025062605897.md): Skin · cracked · Jun 23, 2025 · N41135 · Boeing 757224 · Wing, Plate/Skin
  > LEFT WING, LE, GAP PANEL, I/B SIDE HAS A CRACK. REMOVED SKIN IAW B757-200 SRM 51-40-02-OG-0,FABRICATED NEW PART GAP PANEL IAW SRM 57-41-01-02-01,LOCATED AND DRILLED IAW SRM 51- 40-02-OG-0, REMOVED FASTENERS FOR ACCESS IAW SRM 51-40-02-OG-0, INSTALLED NEW PART
- [SDR CALA2025062605896](https://openairdocs.org/sdr/CALA2025062605896.md): Tee Angle · corroded · Jun 23, 2025 · N41135 · Boeing 757224 · Aerodynamic Fairings
  > WING TO BODY AREA, T-CHORD STA900 BTW RBL45 TO LBL45 HAS CORROSION NOTED AND WEAR MARK*91195281-03((EVALUAT ION)) REF:NR128387. REMOVED AND EVALUATED CORROSION ON T-CHORD STA 900 BTW RBL45 TO LBL45 FOUND TO BE OUT OF LIMITS MATERIAL LOSS 50% WAS REPAIRED I A
- [SDR CALA2025062305807](https://openairdocs.org/sdr/CALA2025062305807.md): Retainer · cracked · Jun 19, 2025 · N41135 · Boeing 757224 · Fuselage Main, Structure
  > RH MLG CUT-OUT FWD SEAL RETAINER AT TACHMENT FRAME CRACHED AT THE O/B END. REMOVED AND REPLACED SUPPORT CHANNEL AT RH MLG W/W CUT OUT FRAME 1060 I.A.W B757-200 SRM 51-40-02-0G-0 AND DWG 149N7550 REV H. L P#5250684
- [SDR CALA2025060905381](https://openairdocs.org/sdr/CALA2025060905381.md): Wire Harness · inoperative · Jun 6, 2025 · N41135 · Boeing 757224 · Light System Wiring
  > FWD CABIN, EMERGENCY LIGHTS BETWEEN SEAT ROW 3LH AND FWD CABIN AFT CLOSET ARE INOP. CW HARNESS SEAT TO SEAT WAS REPLACED IAW B757-200 SWPM 20-10-11 AND SWPM 20-61-28. OP CHECK WILL BE PERFORMED ON JOB CARD 53-3350-1 -0007 (IDT).
- [SDR CALA2025060905380](https://openairdocs.org/sdr/CALA2025060905380.md): Elec Connector · broken · Jun 6, 2025 · N41135 · Boeing 757224 · Light System Wiring
  > FWD CABIN, DURING BUSINESS FIRST SEATS RST, FOUND EMERGENCY LIGHT CONNECTOR BROKEN AND PINS BENT AT SEAT 4B. R&R CONNECTOR AND HARNESS. CONNECTOR AND HARNESS WERE REPLACED IAW B757-200 SWPM 20-10-11 A ND SWPM 20-61-28. OP CHECK WILL BE PERFORMED ON JOB CARD 5
- [SDR CALA2025020202162](https://openairdocs.org/sdr/CALA2025020202162.md): Smoke Detector · false activation · Jan 31, 2025 · N41135 · Boeing 757224 · Smoke Detection
  > LAVATORY SMOKE EICAS MSG FOR LEFT AND RIGHT AFT LAVS..STAYED ON FOR 2 MINS CREW REPORTED A "HOT, BURNED FOOD, HOT METAL" SMELL. TURNED ON ALL G4 GALLEY COFFEE MAKERS, WARMERS, OVENS FOR 30 MIN. BURNED FOOD SMELL WAS PRESENT AFTER 6-7MIN, DISIPATED ABOUT 15MIN
- [SDR CALA2024112601291](https://openairdocs.org/sdr/CALA2024112601291.md): Oven · smoke · Nov 24, 2024 · N41135 · Boeing 757224 · Buffet/Galleys
  > AFT LEFT OVEN SET OFF 4R LAV SMOKE ALARM WHEN USED. FA REPORTED ELEC SMELL FA REPORTS WHEN THE DOOR ON AFT OVEN #3 WAS OPENED SOMETHING ACTIVATED THE LAV SMOKE DETECTOR LAV DOOR WAS OPEN AND STOPPED WHEN OVEN DOOR WAS SHUT NO TIME TO TS REQUEST NEF NOCDESK: 75
- [SDR CALA2023091102760](https://openairdocs.org/sdr/CALA2023091102760.md): Governor · faulty · Sep 7, 2023 · N41135 · Boeing 757200 · Fuel Controlling System
  > RIGHT ENG DID NOT SPOOL UPON T/O RTO GOVERNOR PART NUMERS IS 8062-551, FFG022AC S/N 9758 PHASE 2 ENG GOVERNOR. VERIFIED P/N''S AND EFFECTIVITY ON FFG & POSITION 38 & 39 OK TO INSTALL FFG ON #2 ENGINE O-RINGS. RAN RIGHT ENG, WITH THROTTLES AT IDLE, N3 WAS H
- [SDR CALA2023012700229](https://openairdocs.org/sdr/CALA2023012700229.md): Fuse · inoperative · Jan 27, 2023 · N41135 · Boeing 757224 · Emergency Lighting
  > CABIN CEILING EMERGENCY LIGHT BETWEEN THE TWO OVER WING DOORS IS INOP. SUPPORT TASK NSA EMX N/R 00257. 33-51-07-962-071. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00257. TROUBLE SHOT SYSTEM CHECKED POWER AND GND AT L48 DISCONNECT IAW B757-ALL SCM 33-51-01 DETECTED
- [SDR CALA2023010400030](https://openairdocs.org/sdr/CALA2023010400030.md): Seat Track · not reported · Jan 2, 2023 · N41135 · Boeing 757224 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK REPLACEMENT AT BS 1320 - 1540, LBL 45.50. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-00-52, REPAIR 3.
- [SDR CALA2022051601265](https://openairdocs.org/sdr/CALA2022051601265.md): None · none · May 16, 2022 · N41135 · Boeing 757200 · Fuselage Structure (General)
  > IN REFERENCE TO DIP#8578540 PLANNING TO CONTACT ENGINEERING AFTER AUGUST 20,2023 BUT BEFORE SEPTEMBER 20,2023 FOR THE INSPECTION REQUIREMENTS AND PERMANENT REPAIR ON ECRA 5362-01035 LATEST REVISION. INSPECTION REQUIREMENTS AND PERMANENT REPAIR ON ECRA 5362-010
- [SDR CALA2022051601264](https://openairdocs.org/sdr/CALA2022051601264.md): None · none · May 16, 2022 · N41135 · Boeing 757200 · Fuselage Structure (General)
  > THE REPAIR INCORPORATED VIA ECRA 5362-01035 AT STA 1640 S5R-S6R IS APPROVED AS TIME LIMITED FOR 18 MONTHS PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE ACFT FROM SERVICE ON OCTOBER 20, 2023 UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING
- [SDR CALA2022051301221](https://openairdocs.org/sdr/CALA2022051301221.md): Fitting · corroded · May 12, 2022 · N41135 · Boeing 757200 · Fuselage Structure (General)
  > (SUPPORT TASK) MAIN CABIN STA 395-418 RBL 10.40 FITTING IS CORRODED. TRANSCRIBED FROM HAECO GSO NR 9287543.
- [SDR CALA2022051101203](https://openairdocs.org/sdr/CALA2022051101203.md): Intercostal · corroded · May 10, 2022 · N41135 · Boeing 737 · Fuselage Main, Floor Beam
  > (B757-53-3-0479) GALLEY 1B FLOOR STRUCTURE INTERCOSTAL STATION 400 INBOARD HAS CORROSION. DOT: F542. TRANSCRIBED FROM HAECO GSO NR 9286842.
- [SDR CALA2022051101202](https://openairdocs.org/sdr/CALA2022051101202.md): Floor Support · corroded · May 10, 2022 · N41135 · Boeing 737 · Fuselage Main, Floor Beam
  > (B757-53-3-0479) GALLEY 1B FLOOR STRUCTURE INTERCOSTAL BETWEEN STATION 377- 400 HAS CORROSION. DOT:F541. TRANSCRIBED FROM HAECO GSO NR 9286841.
- [SDR CALA2022050901178](https://openairdocs.org/sdr/CALA2022050901178.md): Skin · worn · May 7, 2022 · N41135 · Boeing 757200 · Trailing Edge Flaps
  > B757-06-3-0302 LEFT WING O/B MAIN FLAP O/B SIDE L/E AREA WORN, T RANSCRIBED FROM HAECO GSO NR 9286982 V901426 INSP QC418 REPAIR 3. THIS REPAIR REQUIRES THAT THE BLIND RIVETS INSTALLED IN REPAIR TO BE EXAMINED EVERY 2500 FLIGHT CYCLES. ACCOMPLISHED NOSE SKIN RE
- [SDR CALA2022050901177](https://openairdocs.org/sdr/CALA2022050901177.md): Deck Plate · corroded · May 7, 2022 · N41135 · Boeing 757200 · Fuselage Main, Structure
  > B757-53-3-0479 MAIN CABIN AFT DECK PLATE UPPER SURFACE IS CORROD ED FROM APPROX STA 1708 - 1720, BL 0 - LBL 21 (MARKED), TRANSCRI BED FROM HAECO GSO NR 9286867 REMOVED AND REPLACED AFT DECK PLATE FROM STA 1681 TO 1720 IAW BA C DWG 146N5300 REV A AND B757-200 S
- [SDR CALA2022050901175](https://openairdocs.org/sdr/CALA2022050901175.md): Frame · gouged · May 7, 2022 · N41135 · Boeing 757200 · Fuselage Main, Frame
  > B757-53-3-0582 MAIN CABIN RH FRAME UPPER FLANGE IS GOUGED AT STA 1640 BETWEEN S5R AND S6R (MARKED), TRANSCRIBED FROM HAECO GSO N R 9287062 REPAIRED RH FRAME GOUGE IAW HAECO REO G23780 STAGE 2 AND RECEIVE D FINAL UAL EC/RA 5302-01035. HAECO GSO MECH V900838 INS
- [SDR CALA2022050401126](https://openairdocs.org/sdr/CALA2022050401126.md): Frame · gouged · May 3, 2022 · N41135 · Boeing 757200 · Fuselage Main, Frame
  > B757-53-3-0580 MAIN CABIN LH FRAME UPPER FLANGE IS GOUGED AT STA 1640 BETWEEN S5L AND S6L (MARKED), TRANSCRIBED FROM HAECO GSO N R 9287063 REPAIRED DAMAGE AREA IAW REO G23479 APPLIED CIC TO AREA IAW AMM 51-24-03-377-008 AND FINAL UAL EC/RA 5362-01036. HAECO GS
- [SDR CALA2022050201111](https://openairdocs.org/sdr/CALA2022050201111.md): None · corroded · Apr 30, 2022 · N41135 · Boeing 757 · Fuselage Structure (General)
  > SUPPORT TASK MAIN CABIN R2 DOOR LOWER SILL HAS CORRODED CHORD ST A 680 RBL 65, TRANSCRIBED FROM HAECO GSO NR 9287526 REMOVED CORROSION IAW B757-200 SRM 51-40-02 ORIGINAL MATERIAL.1 PN 143N8328U53 PO 1028565.1 IAW B757-200 SRM 51-40-05, 51-40-08 00, REMOVED.0
- [SDR CALA2022042901098](https://openairdocs.org/sdr/CALA2022042901098.md): Beam · corroded · Apr 27, 2022 · N41135 · Boeing 757200 · Fuselage Main, Floor Beam
  > B757-53-3-0479 GALLEY 1B FLOOR STRUCTURE T-CAP STATION 365 INBOA RD HAS APPROX 2O" CORROSION, TRANSCRIBED FROM HAECO GSO NR 92868 39 REMOVED CORROSION ON T-CAP AT STA 365. ORIGINAL MAT THICKNESS IS 53-00-51-2R-10 REPAIR 10 FIG 201 DETAIL I AND II. RESTORED FIN

Next page: https://openairdocs.org/aircraft/N41135/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 = 'N41135' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N41135/reports

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