# Service difficulty reports: N33284

A list on [N33284](https://openairdocs.org/aircraft/N33284.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 · 85 reports

- [SDR CALA2026033014886](https://openairdocs.org/sdr/CALA2026033014886.md): Unknown · odor · Mar 27, 2026 · N33284 · Boeing 737824 · Passenger Compartment Equipment
  > STRONG CHEMICAL ODOR IN AFT GALLEY. OPENED REAR DOORS TO VENTILATE AREA BELIEVE IT WAS CLEANING SOLUTION FROM AC CLEANERS ON BATHROOM FLOORS AREA ODOR DISAPATED
- [SDR CALA2025101309926](https://openairdocs.org/sdr/CALA2025101309926.md): Oven · odor · Oct 11, 2025 · N33284 · Boeing 737824 · Buffet/Galleys
  > BURNT SMELL IN FWD GALLEY UPON ENTERING A/C. FLIGHT CREW BRIEFED ODOR/SMELL NEAR DOOR 1R. NO APU IN OPERATION. FAINT SMELL EXISTED, BUT NOT HEAVY. RECIRC FANS WERE ON. OPENED EE COMPARTMENT, SAME ODOR EXISTED, COULDNT FIND ANYTHING NOTICEABLE. CREW STARTED APU
- [SDR CALA2025100909823](https://openairdocs.org/sdr/CALA2025100909823.md): Door · out of rig · Oct 7, 2025 · N33284 · Boeing 737824 · Passenger/Crew Doors
  > TEST FLIGHT REFLY REQUIRED REFLY REQUIRED FOR L2 DOOR LATCH MOVING ON TAKEOFF LOCKED BY SYSTEM. RE-RIGGING COMPLETED AND TEST HOP READY ACCOMPLISHED AFT ENTRY DOOR (SOFT UNLATCHING) CHECK AND ADJUSTED ALL LATCH ROLLERS WITHIN LIMITS IAW AMM 52-13-00-820-802. A
- [SDR CALA2025101309986](https://openairdocs.org/sdr/CALA2025101309986.md): Skin · damaged · Oct 5, 2025 · N33284 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT BS 177 - 196.50, STR 17R -24R DAMAGED. INTERIM REPAIR PERFORMED AT FUSELAGE SKIN STA 177 - 196.50, STR 17R - 24R IAW ECRA 5310-08695.
- [SDR CALA2025100709742](https://openairdocs.org/sdr/CALA2025100709742.md): Floorbeam · corroded · Oct 5, 2025 · N33284 · Boeing 737824 · Fuselage Main, Floor Beam
  > FORWARD PASSENGER CABIN FLOORBEAM UPPER SURFACE HAS CORROSION SPOT B.S. 380 LBL. 56". REMOVED CORROSION ON CABIN FLOORBEAM UPPER SURFACE B.S. 380 LBL 56", AND ACCOMPLISHED REPAIR IAW REF. AAR-MIA ESR-WI#13-12756 REV. ORIGINAL.
- [SDR CALA2025101309987](https://openairdocs.org/sdr/CALA2025101309987.md): Skin · corroded · Oct 1, 2025 · N33284 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LAVATORY TOILET SERVICE AT LWR EXTERNAL FUSELAGE SURFACE STRUCTURE WITH BULDGING SKIN AROUND FASTENERS. INSTALLED REPAIR AT FUSELAGE LOWER SKIN STA 827 - 887, STR 22L - 26L IN ACCORDANCE WITH AAR-MIA ESR-WI 2023803-19-12777 REV. IR,
- [SDR CALA2025100109510](https://openairdocs.org/sdr/CALA2025100109510.md): Rib · gouged · Sep 30, 2025 · N33284 · Boeing 737824 · Wing, Rib/Bulkhead
  > LEFT DEFLECTION CONTROL RIB GOUGED AT SERRATED PLATE ATTACHING TAB. INSTALLED REPAIR PARTS AT LT DEFLECTION CONTROL RIB IAW SRM 57-51-02-2R-4 AND SRM 57-51-02-2R-1.
- [SDR CALA2025100109508](https://openairdocs.org/sdr/CALA2025100109508.md): Strut · cracked · Sep 30, 2025 · N33284 · Boeing 737824 · Landing Gear Doors
  > LMLG STRUT DOOR CRACK AT FWD LWR AREA. 8-3 (REF AAR N/R 99950447) ESFR ENTRY INSTALLED REPAIR PARTS FITTING AND FILLER AT LMLG STRUT DOOR FWD LWR IAW SRM 51-40-02-0G-0 AND SRM 52-80-02-2R-3.
- [SDR CALA2025093009433](https://openairdocs.org/sdr/CALA2025093009433.md): Channel · punctured · Sep 29, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY ZEE ANGLE LH LOCATED BETWEEN STA. 727H AND 727I HAS BEEN PUNCTURED (REF AAR N/R 99951087) REMOVED AND REPLACED AFT CARGO BAY ZEE ANGLE LH BETWEEN STA. 727H AND 727I PER SRM 51-40-02-0G-0 AND DWG#146A7500.
- [SDR CALA2025100609637](https://openairdocs.org/sdr/CALA2025100609637.md): Web · corroded · Sep 27, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT SURROUND STRUCTURE, NEXT TO THE FORWARD EDGE, FOUND CORROSION ON UPPER SURFACE. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SURROUND SILL(WEB) STA 807 TO 847 RBL 22 PER SRM 51-40-02-0G-0 AND DWG#146A8120.
- [SDR CALA2025092909386](https://openairdocs.org/sdr/CALA2025092909386.md): Angle · corroded · Sep 27, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY. CORROSION AROUND HOLES AT ZEE ANGLE RT, BETWEEN BS 727J AND 747. REMOVED AND REPLACED ZEE ANGLE RH BETWEEN STA. 727J AND 767 RBL 21 IAW SRM 51-40-02-0G-0 AND DWG#146A7500.
- [SDR CALA2025092909384](https://openairdocs.org/sdr/CALA2025092909384.md): Support Angle · cracked · Sep 27, 2025 · N33284 · Boeing 737824 · Aerodynamic Fairings
  > FOUND CRACK RT FWD BODY FAIRING SUPPORT ANGLE INBD END OF FRONT SPAR FIXED LEADING EDGE. REMOVED AND REPLACED ZEE ANGLE RH BETWEEN STA. 727J AND 767 RBL 21 PER SRM 51-40-02-0G-0 AND DWG 146A7500.
- [SDR CALA2025092909381](https://openairdocs.org/sdr/CALA2025092909381.md): Support Angle · cracked · Sep 26, 2025 · N33284 · Boeing 737824 · Wing Miscellaneous Structure
  > RIGHT WING FIXED LEADING EDGE FOUND SUPPORT ANGLE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING FIXED LEADING EDGE IAW SRM 51-40-02-0G-0 AND DWG 116A4008.
- [SDR CALA2025092509260](https://openairdocs.org/sdr/CALA2025092509260.md): Door Frame · worn · Sep 24, 2025 · N33284 · Boeing 737824 · Fuselage Main, Structure
  > WORN AFT E/E DOOR LATCH FITTING AT E/E BAY DOOR CUT OUT. REMOVED AND REPLACED LATCH FITTING AT AFT E/E DOOR CUT OUT IAW SRM 51-40-02-0G-0 AND DWG 141A8505.
- [SDR CALA2025092609293](https://openairdocs.org/sdr/CALA2025092609293.md): Bracket · cracked · Sep 23, 2025 · N33284 · Boeing 7378 · Fuselage Miscellaneous Structure
  > RIGHT FWD CARGO COMPARTMENT AT AFT AIR CONDITIONING DISTRIBUTION BAY AT BS 500I, STR 19R HAS BRACKET CRACKED. REMOVED AND REPLACED RIGHT FWD CARGO COMPARTMENT GUSSET AT AFT AIR CONDITIONING DISTRIBUTION BAY AT BS 500I, STR 19-R IAW SRM 51-40-02-0G-0 AND DWG
- [SDR CALA2025092309167](https://openairdocs.org/sdr/CALA2025092309167.md): Skin · cracked · Sep 21, 2025 · N33284 · Boeing 737824 · Fuselage Main, Plate/Skin
  > EXTERNAL POWER DOOR CUTOUT CRACKED AT LOWER SIDE. INSTALLED DOUBLER AND FILLER TO REPAIR AREA AS PER REFERENCE SRM 53-10-15-2R-4 REPAIR 4 FIGURE 204 SHEET 1 AND SRM SRM 514002-0G-0
- [SDR CALA2025100609635](https://openairdocs.org/sdr/CALA2025100609635.md): Spar · corroded · Sep 19, 2025 · N33284 · Boeing 737824 · Wing Spar
  > FOUND CORROSION ON RIGHT WING INBD OF REAR SPAR SKIN NEXT TO FUEL BOOST PUMP LOWER BONDONG CABLE. ACCOMPLISHED REPAIR ON RIGHT WING REAR SPAR WEB IN ACCORDANCE WITH AAR-MIA ESR-WI #2023803-44-12877 REV IR, AND UNITED EC/RA 5720-03566 REV.
- [SDR CALA2025092209108](https://openairdocs.org/sdr/CALA2025092209108.md): Rib · worn · Sep 19, 2025 · N33284 · Boeing 737824 · Fuselage Main, Structure
  > L1 DOOR INTERNAL SKIN UPPER HINGE RIB GOUDGED. REMOVED AND REPLACED RIB (INTERCOSTAL) ON L1 DOOR UPPER HINGE IN REF TO SRM 51-40-02-0G-0 AND DWG 141A6190. VERIFIED ESFR HAS BEEN CREATED. NO DIPS REQUIRED.
- [SDR CALA2025092209106](https://openairdocs.org/sdr/CALA2025092209106.md): Support Angle · gouged · Sep 19, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND GOUGES AT LOWER FUSELAGE SUPPORT ANGLE O/B OF R/H RAM AIR EXIT EXHAUST FWD OF MAIN W/W. REMOVED AND REPLACED SUPPORT ANGLE AT LOWER FUSELAGE O/B R/H RAM AIR EXHAUST, FWD OF MAIN W/W REF SRM 51-40-0G-0 AND DWG # 149A7216.
- [SDR CALA2025092209105](https://openairdocs.org/sdr/CALA2025092209105.md): Support Angle · gouged · Sep 19, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND. GOUGES AT LOWER FUS. SUPPORT ANGLE O/B OF L/H RAM AIR EXIT EXHAUST. REMOVED AND REPLACED SUPPORT ANGLE AT LOWER FUSELAGE O/B L/H RAM AIR EXHAUST, FWD OF MAIN W/W REF. SRM 51-40-0G-0 AND DWG # 149A7216.
- [SDR CALA2025101309983](https://openairdocs.org/sdr/CALA2025101309983.md): Skin · dented · Sep 17, 2025 · N33284 · Boeing 737824 · Fuselage Main, Plate/Skin
  > DENT AT BS 188 BETWEEN STR 21 & 24 RT & CARD LP# 4423742 REF.AAR N/E:99950967. REMOVED DAMAGED AREA ON FUSELAGE SKIN AND INSTALLED REPAIR AT BS 177 TO 196.5, S17R-24R, REF AAR-MIA ESR-WI #2023803-17-12771 AND UNITED EC/RA 5310-08695. PERFORM AN INSPECTION O
- [SDR CALA2025101309981](https://openairdocs.org/sdr/CALA2025101309981.md): Door Frame · cracked · Sep 16, 2025 · N33284 · Boeing 737824 · Fuselage Main, Structure
  > CRACK AT CIRCUNFERENTIAL FRAME FITTING AT L1 DOOR CUT OUT INTERNAL STA 312 AND S8L. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR AT CIRCUMFERENTIAL FRAME L1 DOOR CUTOUT AREA, STA.312 AND STR.5L - STR.6L, IAW SRM 53-10-07-2R-1.
- [SDR CALA2025100609632](https://openairdocs.org/sdr/CALA2025100609632.md): Floorbeam · dented · Sep 16, 2025 · N33284 · Boeing 737824 · Fuselage Main, Floor Beam
  > FLIGHT DECK FLOOR HAS DENT AT STA 246 LBL 14. INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB STA 246 LBL10 TO RBL 8, REF. SRM 51-40-02-0G-0 AND SRM 53-10-51-2R-2.
- [SDR CALA2025092209084](https://openairdocs.org/sdr/CALA2025092209084.md): Angle · cracked · Sep 14, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LEFT AIR CONDITIONER BAY AFT UPPER ANGLE CRACKED ON IB SIDE. REMOVED FASTENERS AT STA 663 LT VAPOR BARRIER ANGLE FROM LBL 5 TO LBL 30 FOR ACCESS TO REPAIR PER SRM 51-40-02-0G-0.CUT AND REMOVED BARRIER ANGLE FROM LBL 5 TO LBL 20 FOR ACCESS TO REPAIR PER SRM 5
- [SDR CALA2025091608952](https://openairdocs.org/sdr/CALA2025091608952.md): Attach Angle · cracked · Sep 14, 2025 · N33284 · Boeing 737824 · Fuselage Main, Attach Fittings
  > RT AIR CONDITIONER BAY AFT UPPER ANGLE CRACKED ON IB SIDE. REF. AAR N/R:99950870 ESFR TRANSACTION COMPLETE REMOVED DAMAGED SECTION AND INSTALLED REPAIR AT STA 663 RH VAPOR BARRIER UPPER ATTACH ANGLE AND SPLICE FROM RBL5 TO RBL30 PER PER SRM 57-10-10-2R-5.
- [SDR CALA2025100609630](https://openairdocs.org/sdr/CALA2025100609630.md): Seal Depressor · cracked · Sep 13, 2025 · N33284 · Boeing 737824 · Fuselage Main, Structure
  > CRACK FOUND AT SEAL DEPRESSOR MAIN CABIN STA 294.5 BETWEEN STR 8R AND 9R R1 DOOR CUT OUT FWD UPPER CORNER. (REF AAR N/R 99950891) CREATED ESFR FOR LOG PAGE 6255534 NON-ROUTINE 99950891 REMOVED AND REPLACED SEAL DEPPRESOR AT FWD GALLEY DOOR STA.294.5 BET. STR8R
- [SDR CALA2025100609629](https://openairdocs.org/sdr/CALA2025100609629.md): Stringer · corroded · Sep 12, 2025 · N33284 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > CORROSION AT FWD CARGO AFT (AIR CONDITIONING DISTRIBUTION BAY) STR 28 LEFT STA 530.DOT251-083. (REF AAR N/R 99951024) ESFR TRANSACTION COMPLETED PERFORMED REPAIR TO THE LEFT-HAND KEEL BEAM UPPER INNER CHORD IN ACCORDANCE WITH AAR-MIA ESR-WI NO.: 2023803-27-12
- [SDR CALA2025100609628](https://openairdocs.org/sdr/CALA2025100609628.md): Stringer · corroded · Sep 12, 2025 · N33284 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > CORROSION AT FWD CARGO AFT (AIR CONDITIONING DISTRIBUTION BAY) STR 28 RIGHT STA 537.DOT251-084. (REF AAR N/R 99951025) ESFR TRANSACTION COMPLETE PERFORMED REPAIR TO THE RIGHT-HAND KEEL BEAM UPPER INNER CHORD IN ACCORDANCE WITH AAR-MIA ESR-WI NO.: 2023803-28-1
- [SDR CALA2025092209083](https://openairdocs.org/sdr/CALA2025092209083.md): Door Frame · cracked · Sep 12, 2025 · N33284 · Boeing 737824 · Fuselage Main, Structure
  > TYPICAL CRACK FOUND AT FWD GALLEY DOOR INTERNAL AFT AREA ABOVE AND ADJACENT TO SEAL DEPRESSOR. REMOVED AND REPLACED FRAME AT FWD GALLEY DOOR IAW B737 SRM 51-40-02-0G-0, AND DWG 141A8370.
- [SDR CALA2025091208828](https://openairdocs.org/sdr/CALA2025091208828.md): Floor Support · cracked · Sep 11, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CAB. STA.344-360 LBL 11" INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA.344-360 LBL 11" REF SRM 51-40-02-0G-0, AND DWG 141A5400.
- [SDR CALA2025101309982](https://openairdocs.org/sdr/CALA2025101309982.md): Skin · cracked · Sep 9, 2025 · N33284 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 120.30, 19" FROM REAR SPAR, I/B ROW. CRACK LENGTH: 0.343". REPAIRED AREA AND FABRICATED REPAIR PARTS LOWER INSPAR SKIN AT STAB. STA 120.30 AND 129 AND 138 RIGHT HORIZONTAL STABILIZER IN REF T
- [SDR CALA2025091008732](https://openairdocs.org/sdr/CALA2025091008732.md): Floorbeam · corroded · Sep 8, 2025 · N33284 · Boeing 737824 · Fuselage Main, Floor Beam
  > CORROSION FWD WET AREA AT FLOORBEAM STA 344 LBL 57. REMOVED CORROSION AT FWD WET AREA FLOORBEAM STA 344 LBL 57" IAW SRM 51-10-02-0G-0-.MEASURED THE AREA,ORIGINAL MATERIAL 0.175, MATERIAL LOSS 0.112", MATERIAL REMAINING 0.063", FOUND TO BE OUT OF LIMITS IAW
- [SDR CALA2025092209082](https://openairdocs.org/sdr/CALA2025092209082.md): Floorbeam · cracked · Sep 6, 2025 · N33284 · Boeing 737824 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOORBEAM CRACKED AT STA 540 BETWEEN BL0 TO RBL 24. INSTALLED FLOORBEAM AT PASSENGER CABIN STA 540 BETWEEN BL 0 TO RBL 24 IAW SRM 51-40-02-0G-0 AND IPC 53-42-11-66. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02-0G-0 AND DWG 143A0060.
- [SDR CALA2025091008721](https://openairdocs.org/sdr/CALA2025091008721.md): Floorbeam · corroded · Sep 6, 2025 · N33284 · Boeing 737824 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM 947.5 IS CORRODED RBL 50 AT AREA THAT LAV MOUNT IS ATTACHED. REMOVED DAMAGED AREA & INSTALLED FLOORBEAM REPAIR AT BS 947.5, IAW SRM 53-70-51-2R-5 REPAIR 5, DWGS 147A5760, 147A5504, AAR-MIA ESR-WI #14-12758 REV IR, & EC/RA #5370-01195, REV ORIG
- [SDR CALA2025101309985](https://openairdocs.org/sdr/CALA2025101309985.md): Skin · cracked · Sep 4, 2025 · N33284 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB. STA 175.50, 10" FROM REAR SPAR,I/B ROW. CRACK LENGTH: 0.281" ESFR SUBMITTED ACCOMPLISHED REPAIR ON LOWER INSPAR SKIN STA175.50 AT LH HORIZ. STAB. REF SRM 55-10-01-2R-11 & DWG 182A4001 AND REQUIRES
- [SDR CALA2025101309984](https://openairdocs.org/sdr/CALA2025101309984.md): Bulkhead Web · cracked · Sep 4, 2025 · N33284 · Boeing 737824 · Fuselage Main, Bulkhead
  > CRACK FOUND AT VERTICAL PRESSURE WEB BETWEEN RBL40 AND RBL45.64. CRACK LENGTH: 0.656". REF. AAR N/R:99950519. REMOVED DAMAGE SECTION AND INSTALLED VERTICAL PRESSURE WEB WEB REPAIR AT BS 663 BETWEEN RBL 25 TO RBL 47 IAW SRM 57 10-10-2R-3, REPAIR 3. PERFORM
- [SDR CALA2025090808579](https://openairdocs.org/sdr/CALA2025090808579.md): Bracket · corroded · Sep 4, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR L1 DOOR AFT GIRT BAR FITTING HAS CORROSION SPOTS. REMOVED AND REPLACED AFT GIRT BAR FITTING AT FORWARD PASSENGER CABIN FLOOR STRUCTURE L1 DOOR IAW SRM 51-40-02-0G-0 AND DWG # 141A5220.
- [SDR CALA2025090808576](https://openairdocs.org/sdr/CALA2025090808576.md): Floor Support · cracked · Sep 4, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR SUPPORT CHORD APPEARS CRACKED AT FRAME B.S. 303.9 LBL. 54". REMOVED AND REPLACED INNER CHORD AT MAIN CABIN FWD WET AREA FLOOR SUPPORT BETWEEN STA 270 TO STA 360 LBL 59" IAW SRM 51-40-02-0G-0 AND DWG #141A8110.
- [SDR CALA2025090808575](https://openairdocs.org/sdr/CALA2025090808575.md): Floor Support · cracked · Sep 4, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR SUPPORT CRACKED AT FASTENER HOLES BS 380 - 400, LBL 14. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG # 141A5400.
- [SDR CALA2025100609625](https://openairdocs.org/sdr/CALA2025100609625.md): Floor Support · corroded · Sep 2, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR SUPPORT HAS CORROSION SPOTS ON UPPER SURFACE B.S.312+5" LBL. 12". REMOVED AND REPLACED FLOOR SUPPORT AT FORWARD PASSENGER CABIN B.S. 312 TO 328, LBL. 12" REF SRM 51-40-02-0G-0. AND DWG: 141A5400.
- [SDR CALA2025100609624](https://openairdocs.org/sdr/CALA2025100609624.md): Floor Support · cracked · Aug 30, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR INTERCOSTAL CRACKED AT FASTENER HOLES B.S. 380 - B.S.400 RBL. 10". (51-023) ESFR ENTERED REMOVED AND REPLACED INTERCOSTAL AT PASSENGER CABIN FLOOR STA 380 TO STA 400 RBL 10" IAW SRM 51-40-02-0G-0 AND DWG # 143A5400.
- [SDR CALA2025100609623](https://openairdocs.org/sdr/CALA2025100609623.md): Floor Support · cracked · Aug 30, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR INTERCOSTAL CRACKED AT FASTENER HOLES B.S. 380 - B.S. 400 BL. 0 (51-022) ESFR ENTERED REMOVED AND REPLACED INTERCOSTAL AT FORWARD PASSENGER CABIN FLOOR STA 380 TO 400 LB 0 IAW SRM 51-40-02-0G-0 AND DWG # 143A5400 WORK ACCOMPLISHED
- [SDR CALA2025090408471](https://openairdocs.org/sdr/CALA2025090408471.md): Floor Support · cracked · Aug 30, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CAB. STA.344-360 BL-0, INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA.344-360-BL0, PER B737 SRM 51-40-02-0G-0 AND DWG 141A5400.
- [SDR CALA2025090208372](https://openairdocs.org/sdr/CALA2025090208372.md): Support Angle · corroded · Aug 30, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > REMOVED AND REPLACED SUPPORT ANGLE ATTACHED TO INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 141A8312. REMOVED AND REPLACED SUPPORT ANGLE ATTACHED TO INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 141A8312.
- [SDR CALA2025090208371](https://openairdocs.org/sdr/CALA2025090208371.md): Floorbeam · cracked · Aug 30, 2025 · N33284 · Boeing 737824 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOORBEAM AT STA 540 BETWEEN BL0 TO LBL 24 LOOSE. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02-0G-0,AND AMM 51-21-72-370-804.
- [SDR CALA2025090108311](https://openairdocs.org/sdr/CALA2025090108311.md): Floor Support · cracked · Aug 29, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR SUPPORT CRACKED AT NUTPLATE, BS 277-294.5, RBL 1. REMOVED AND REPLACED INTERCOSTAL AT FORWARD PASSENGER CABIN FLOOR SUPPORT BS 277 TO 294.5, RBL 1 IAW SRM 51-40-02-0G-0 AND DWG 141A5400.
- [SDR CALA2025090508499](https://openairdocs.org/sdr/CALA2025090508499.md): Floor Support · cracked · Aug 26, 2025 · N33284 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FORWARD PASSENGER CABIN FLOOR SUPPORT CRACKED AT FASTENER HOLES, BS 312 - 328, RBL 31. REMOVED AND REPLACED FORWARD CABIN FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5400.
- [SDR CALA2025061905718](https://openairdocs.org/sdr/CALA2025061905718.md): Sliding Window · failed · Jun 18, 2025 · N33284 · Boeing 737824 · Flight Compartment Windows
  > CAPTAIN`S L2 WINDOW SHATTER ON TAXI IN TALKED TO CREW WINDOW SHATTERED ON TAXI IN. WINDOW HEAT WAS ON WHEN WINDOW SHATTERED IT GAVE A WINDOW OVER HEAT CAUTION. CAPTAIN SAID IN FLIGHT WINDOW STARTED TO DELAMINATION IN MIDDLE. CAPTAIN DID STATE THERE WAS NO AR
- [SDR CALA2025051204617](https://openairdocs.org/sdr/CALA2025051204617.md): Fuse · blown · May 10, 2025 · N33284 · Boeing 737824 · Emergency Lighting
  > FLOOR PROXIMITY EMERGENCY LIGHTS INOP ROWS 22-31. REPLACED BATTERY M1670 & M1672. POWER SUPPLY M1672 FUSES CHECK OK. REPLACED BATTERY M1672 POWER SUPPLY. NO HELP. REINSTALLED EQUIPMENT IN ORIGINAL LOCATIONS. REF WDM 33-51-22-3.1 REF SSM 33-51-21-104.1 & WDM 3
- [SDR CALA2025022602475](https://openairdocs.org/sdr/CALA2025022602475.md): Light · broken · Feb 25, 2025 · N33284 · Boeing 737824 · Emergency Lighting
  > AISLE EMERGENCY LIGHT AT SEAT 37C IS BROKEN. REPLACED LIGHT ASSEMBLY REF MM 33-51-11. OPS CHECK OK.

Next page: https://openairdocs.org/aircraft/N33284/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 = 'N33284' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N33284/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.