# Service difficulty reports: N33289

A list on [N33289](https://openairdocs.org/aircraft/N33289.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 · 61 reports

- [SDR CALA2026092919959](https://openairdocs.org/sdr/CALA2026092919959.md): Wire Harness · faulted · Sep 28, 2026 · N33289 · Boeing 737824 · Engine Fuel System Wiring
  > REPLACE NR 2 ENG MW0311 HARNESS IAW AMM 73-21-06-400-802-F00, BEFORE DEPARTING SFO DUE HISTORY OF NO BLEED ON NR 2 ENGINE. STARTED REMOVAL OF MW0311 HARNESS FROM FIREWALL DOWN TO STRUT FAIRING. REMOVED AND INSTALLED MW0311 IAW AMM 73-21-06-400-802-F00. REF
- [SDR CALA2026091019346](https://openairdocs.org/sdr/CALA2026091019346.md): Battery Pack · no test · Sep 9, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > SEAT-MOUNTED FLOOR PROXIMITY LIGHTS ON ROWS 7-14 DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY BATTERY PACK AT M1676 PER AMM 33-51-06.
- [SDR CALA2026081418639](https://openairdocs.org/sdr/CALA2026081418639.md): Slide · faulted · Aug 12, 2026 · N33289 · Boeing 737824 · Escape Slide
  > CREW REPORTED, L1 DOOR GIRT BAR SLIDE HAS EXCESS GIRT MATERIAL. MX ACCOMPLISHED INSPECTION OF ESCAPE SLIDE GIRT BAR & FOUND EXCESSIVE GIRT MEASUREMENTS OUT OF LIMITS IAW AMM 25-66-01. REPACK, REPLACEMENT OF DOOR 1L. R & R L1 ESCAPE SLIDE IAW AMM 25-66-01-0
- [SDR CALA2026031614581](https://openairdocs.org/sdr/CALA2026031614581.md): Unknown · odor · Mar 14, 2026 · N33289 · Boeing 737824 · Air Distribution System
  > UNUSUAL ODOR THROUGHOUT PLANE ESPECIALLY NEAR FRONT. NOTED VERY STRONG ELECTRICAL BURNING ODOR COMING FROM FLIGHTDECK AND FWD E & E AREA REPLACED LT & RT RECIRCULATION AIR FILTERS IAW TASK 21-25-01-400-801. INSPECTED FWD GALLEY AREA LIGHTS. ENTRY LIGHTS, N
- [SDR CALA2026030514343](https://openairdocs.org/sdr/CALA2026030514343.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > BATTERY PACK M1695 FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERY PACK M1695 IAW AMM 33-51-06-960-805 TESTED GOOD.
- [SDR CALA2026030514341](https://openairdocs.org/sdr/CALA2026030514341.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > BATTERY PACK M1694 FAILED AN OPS CHECK. REMOVED AND REPLACED POWER SUPPLY M1694 & BATTERY PACK M1694 IAW AMM 33-51-06-960-806 & AMM 33-51-06-960-805 TESTED GOOD.
- [SDR CALA2026030514339](https://openairdocs.org/sdr/CALA2026030514339.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY PACK M1674 FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERY IN POWER SUPPLY M1674, INSTALLATION TESTED GOOD IAW AMM 33-51-06-960-806.
- [SDR CALA2026030314288](https://openairdocs.org/sdr/CALA2026030314288.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > PASSENGER CABIN, EMERGENCY LIGHT BATTERY PACK M1672 FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERY PACK M1672 IAW AMM 33-51-06-960-805, TESTED GOOD.
- [SDR CALA2026030314287](https://openairdocs.org/sdr/CALA2026030314287.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS, BATTERY PACK M1670 FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERY PACK M1670 IAW AMM 33-51-06-960-806 & AMM 33-51-06-960-805, TESTED GOOD.
- [SDR CALA2026030314286](https://openairdocs.org/sdr/CALA2026030314286.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS, BATTERY PACK M1676 FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERY PACK M1676 IAW AMM 33-51-06-960-806 & 33-51-06-960-805. TESTED GOOD.
- [SDR CALA2026030314285](https://openairdocs.org/sdr/CALA2026030314285.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS, BATTERY PACK M1675 FAILED AN OPS CHECK. REMOVED AND INSTALLED A NEW BATTERY PACK M1675, TESTED GOOD IAW AMM 33-51-960-806.
- [SDR CALA2026030314283](https://openairdocs.org/sdr/CALA2026030314283.md): Battery Pack · no test · Mar 2, 2026 · N33289 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS, BATTERY PACK M1671 FAILED AN OPS CHECK. REMOVED AND REPLACED THE BATTERY PACK M1694 IAW AMM 33-51-06-960-805 TESTED GOOD.
- [SDR CALA2026092319714](https://openairdocs.org/sdr/CALA2026092319714.md): Window Frame · cracked · Feb 26, 2026 · N33289 · Boeing 737824 · Fuselage Main, Structure
  > RIGHT NR 3 WINDOW FRAME FOUND CRACKED AT HOLE NR 3. PERFORMED A REPAIR TO THE RT NR 3 WINDOW FRAME E-F POST IAW EA5310-08195, REV C,
- [SDR CALA2026021813856](https://openairdocs.org/sdr/CALA2026021813856.md): Floorbeam · corroded · Feb 14, 2026 · N33289 · Boeing 737824 · Fuselage Main, Floor Beam
  > FOUND CORROSION OUT OF LIMITS AT FLOORBEAM, BS 312, LBL 57. REPAIRED THE DAMAGE CORROSION AT THE FWD WET AREA FLOORBEAM IAW ECRA 5310-0879.
- [SDR CALA2026021213718](https://openairdocs.org/sdr/CALA2026021213718.md): Structure · corroded · Feb 10, 2026 · N33289 · Boeing 737824 · Passenger/Crew Doors
  > FWD WET AREA L1 DOOR, INNER STRUCTURE, BS 344, LBL 60 POSSIBLE CORROSION. REMOVED AND REPLACED L1 DOOR INNER STRUCTURE IAW SRM 51-40-02-0G-0, & DWG 141A8110.
- [SDR CALA2026092319703](https://openairdocs.org/sdr/CALA2026092319703.md): Stiffener · cracked · Feb 8, 2026 · N33289 · Boeing 737824 · Horizontal Stabilizer Miscellaneous Structure
  > LT HORIZONTAL STAB. IN-STAB, RIB HSS 92.7, 3RD STIFFENER FROM FRONT CRACKED. REPAIRED THE 3RD STIFFENER IAW SRM 55-10-09-2R-5, SRM 55-10-01-2R-11.
- [SDR CALA2026092319701](https://openairdocs.org/sdr/CALA2026092319701.md): Stiffener · cracked · Feb 8, 2026 · N33289 · Boeing 737824 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB, IN-SPAR HSS 92.7, NR 3 & 4 STIFFENERS TRANSITION RADIUS & HSS 111.10, NR 3 STIFFENER, CRACKED. REPAIR OVER 5LBS. WEIGHT AND BALANCE CHANGE FORM WAS COMPLETED. WEIGHT CHANGE IS 8.763LBS.+/-. REPAIRED THE DAMAGE IAW 55-10-09-2R-4 AND SR
- [SDR CALA2026012713336](https://openairdocs.org/sdr/CALA2026012713336.md): Floorbeam · corroded · Jan 23, 2026 · N33289 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA, FLOORBEAM BS 986.5, LBL 43 CORRODED.. REPAIRED FLOORBEAM IAW SRM 53-70-51-2R-4,
- [SDR CALA2026012713334](https://openairdocs.org/sdr/CALA2026012713334.md): Channel · corroded · Jan 23, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY, LT ZEE CHANNEL BTW BS 500A & 500F SEVERAL SPOTS OF CORROSION. R & R THE ZEE CHANNEL IAW AMM 20-60-07-913-801, SRM 51-40-02-0G-0, SRM 53-00-53-2R-6, STEP 4 D, TABLE 201, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, AMM 51-21-72-370-802, AMM 51-21-72
- [SDR CALA2026021913903](https://openairdocs.org/sdr/CALA2026021913903.md): Frame · cracked · Jan 22, 2026 · N33289 · Boeing 737824 · Fuselage Main, Frame
  > VISUAL INDICATION OF CRACK IN CABIN FRAME AT BS 380 BTWN S8 - 9R, INBD OVERHEAD BIN ATTACH BRACKET FASTENER. REPAIRED THE DAMAGE IN THE FRAME IAW ECRA 5310-07665.
- [SDR CALA2026021813852](https://openairdocs.org/sdr/CALA2026021813852.md): Flap Track · worn · Jan 22, 2026 · N33289 · Boeing 737824 · Trailing Edge Flaps
  > FLAP TRACK NR 7 HAS WEAR ON THE UPPER RAIL. REPAIRED THE FLAP TRACK UPPER RAIL IAW SRM 57-53-02-2R-10, REP 10, (REPAIR IS A CATEGORY B) INSPECTION REQUIREMENTS IAW STEP 5 TABLE 202. ALL WORK CAPTURED ON AAR N/R 1000065135. REPLACED THE NR 7 FLAP TRACK AS
- [SDR CALA2026012713325](https://openairdocs.org/sdr/CALA2026012713325.md): Bracket · dented · Jan 22, 2026 · N33289 · Boeing 737824 · Fuselage Main, Structure
  > L2 DOOR EXTERNALM BRACKET ON FWD EDGE OF THE DOOR FRAME APPEARS TO HAVE A DENT. REPLACED THE BRACKET IAW 147A0010. REV.- AND SRM 51-40-02-0G-0.
- [SDR CALA2026021913902](https://openairdocs.org/sdr/CALA2026021913902.md): Web · corroded · Jan 21, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY MAIN SILL WEB POSSIBLE CORROSION BTWN BS 787 - 827. REMOVED AND REPLACED THE AFT CARGO MAIN SILL WEB IAW DWG 146A8123, REV C, SRM 51-40-02-0G-0.
- [SDR CALA2026021913901](https://openairdocs.org/sdr/CALA2026021913901.md): Web · corroded · Jan 21, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY MAIN SILL WEB BTWN BS 440 - 500 POSSIBLE CORROSION. REPLACED THE MAIN SILL WEB BTWN BS 440 - 500 IAW SRM 51-40-02--0G-0, 51-40-05-0G-0, 51-40-08-0G-0. AMM 51-21-91-620-802, 51-21-72-370 -804, AND DWG 143A8122, REV D, DWG 143A8120, REV T.
- [SDR CALA2026012313199](https://openairdocs.org/sdr/CALA2026012313199.md): Channel · corroded · Jan 21, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY, RT ZEE CHANNEL BTW BS 500 AND 500I HAD CORROSION. REPAIRED THE ZEE CHANNEL IAW SRM 53-00-53--2R-6, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, SRM 51-10-02-0G-0, AMM 20-60-07-913-801, & SOPM 20-41-02.
- [SDR CALA2026012313197](https://openairdocs.org/sdr/CALA2026012313197.md): Channel · cracked · Jan 21, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY, LT ZEE CHANNEL POSSIBLE COROSION AND CRACK BTW BS 727B AND 727J. R & R THE LT ZEE CHANNEL BTW BS 727B AND 727J IAW SRM 53-00-53-2R-6, AMM 20-60-07-9913-801, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, AMM 51-21-
- [SDR CALA2026012213170](https://openairdocs.org/sdr/CALA2026012213170.md): Channel · cracked · Jan 21, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY, RT ZEE CHANNEL HAD POSSIBLE CORROSION AND CRACKED BTW BS 727D & 727F. REPLACED THE ZEE CHANNEL BTW BS 727C - 727 G IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, & AMM 51-21-72-370-804.
- [SDR CALA2026012213168](https://openairdocs.org/sdr/CALA2026012213168.md): Structure · corroded · Jan 21, 2026 · N33289 · Boeing 737824 · Passenger/Crew Doors
  > AFT WET AREA, L2 DOOR INNER STRUCTURE HAD POSSIBLE CORROSION. REMOVED AND REPLACED L2 DOOR INNER STRUCTURE IAW SRM 51-40-02-0G-0, AND DWG 147A8501, REV B.
- [SDR CALA2026092319697](https://openairdocs.org/sdr/CALA2026092319697.md): Skin · cracked · Jan 20, 2026 · N33289 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > TWO CRACK SIGNALS NOTED AT HORIZONTAL STAB, LT SIDE HSS 157.10, INBD SIDE. FIRST CRACK L=0.375 INCH LOCATED TO 9.375 INCH FWD FROM AFT SPAR, SECOND CRACK L=0.250INCH LOCATED TO 16.500 INCH FWD FROM AFT SPAR. REPAIRED THE DAMAGE IAW SRM 55-10-01-2R -11,
- [SDR CALA2026022614064](https://openairdocs.org/sdr/CALA2026022614064.md): Structure · corroded · Jan 14, 2026 · N33289 · Boeing 737824 · Fuselage Main, Structure
  > AFT WET AREA, R2 DOOR INNER CHORD POSSIBLE CORROSION BETWEEN BS 947 & 986. REMOVED AND INSTALLED NEW INNER STRUCTURE AT THE R2 DOOR. BS 887 - 1006, RBL 55 IAW SRM 51-40-02-0G-0 AND DWG 147A8501, REV A.
- [SDR CALA2026011212879](https://openairdocs.org/sdr/CALA2026011212879.md): Sidewall Support · corroded · Jan 8, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT; LH SIDEWALL SUPPORT AT STA. 500D POSSIBLE CORROSION. REPLACED LH SIDEWALL SUPPORT AT STA 500D IAW B737-800 SRM 51-40- 02-0G-0, 51-40-05-0G-0 AND IPC 53-11-00-35A.
- [SDR CALA2026011212878](https://openairdocs.org/sdr/CALA2026011212878.md): Shield · corroded · Jan 8, 2026 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT; FLOOR STRUCTURE SHIELD BTW BS 500 AND 500A POSSIBLE CORROSION. REPLACED SHIELD ON FWD CARGO BTW STA 500 TO 500A R/H IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG: 143A8126 REV A.
- [SDR CALA2025111711255](https://openairdocs.org/sdr/CALA2025111711255.md): Gcu · faulted · Nov 15, 2025 · N33289 · Boeing 737824 · AC Generator-Alternator
  > GENERATOR SOURCE OFF LIGHT, LIGHT COMES ON BUT NO FAULT LIGHT ON GCU ON GEN 2, SOURCE OFF LIGHT. WHILE TESTING AC SYSTEM, GEN & APU MODULE GEN 2 SOURCE OFF LIGHT CAME ON. GEN 1 WAS ON LINE, RESET GEN 2 & SOURCE OFF LIGHT WENT OUT. GCU 2 NOW HAS AN IDG FAUL
- [SDR CALA2025100309580](https://openairdocs.org/sdr/CALA2025100309580.md): Slide · no discrepancy · Oct 3, 2025 · N33289 · Boeing 737824 · Escape Slide
  > DOOR 1R SLIDE FLAP DRAGGING FOUND GIRT MATERIAL TO BE WITHIN LIMITS CONTAINED WITH AMM 25-66-01-400-801.OPERATION FOUND NORMAL WHEN ENGAGING INTO FLOOR FITTINGS AND STOWING IN STOW BRACKETS.
- [SDR CALA2025081107551](https://openairdocs.org/sdr/CALA2025081107551.md): Fuel Sys · out of balance · Aug 11, 2025 · N33289 · Boeing 737824 · Aircraft Fuel System
  > AT FL320 NOTICED SIGIFICANT FUEL IMBALANCE RT TANK DROPPED 900LBS WITHIN 15 MINS TOTAL DROPED 1700LBS, CAPT REPORTED FUEL INDICATION ON RT SIDE DROPPED 900 LBS AND TOTALIZER DROPPED 1700 LBS IN FLT. CAPT CHECKED CROSS FEED VALVE IN FLT VERIFIED IT WAS CLOSED
- [SDR CALA2025071706672](https://openairdocs.org/sdr/CALA2025071706672.md): Slide · out of position · Jul 15, 2025 · N33289 · Boeing 737824 · Escape Slide
  > GIRT BAR SLIDE MATERIAL DRAGGING ON GROUND DOOR R1. RESECURED R1 DOOR SLIDE PACK MATERIAL IAW AMM 25-66-01. OK FOR SERVICE.
- [SDR CALA2025050904571](https://openairdocs.org/sdr/CALA2025050904571.md): Girt Bar · out of position · May 8, 2025 · N33289 · Boeing 737824 · Escape Slide
  > FA REPORTS FWD GALLEY DOOR GIRT BAR HAS EXCESIVE SLIDE MATERIAL COMING OUT TUCKED EXCESS MATERIAL BACK TO APPROX 11 INCHES REF AMM 25-66-01-400-803.
- [SDR CALA2025021702344](https://openairdocs.org/sdr/CALA2025021702344.md): Trim System · faulted · Feb 14, 2025 · N33289 · Boeing 737824 · Stabilizer Position Indicating
  > STAB TRIM FAIL IN FLIGHT UPON INITIAL INSPECTION, FOUND STAB TRIM WOULD NOT MOVE WHEN OPERATING STAB TRIM WITH BOTH CAPT AND FO TRIM SWITCHES PERFORMED STABILIZER TRIM MOTOR TEST REF AMM 27-41-71-700-801. WHEN ATTEMPTING TO MOVE STAB TRIM MANUALLY USING STAB T
- [SDR CALA2024082000456](https://openairdocs.org/sdr/CALA2024082000456.md): Web · damaged · Aug 18, 2024 · N33289 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN E&E DOOR ENTRYWAY WEBS AND FITTINGS HAVE DAMAGE FROM E&E DOOR LATCH PINS. VERIFIED NEW PART AND FASTENER, INSPECTED INTERFACE. OK TO INSTALL. BLENDED R/H WEB, MINIMAL MATERIAL LOSS NOTED, POLISHED FWD AND AFT ACCESS DOOR FITTINGS, MINIMAL MATERIAL LOSS,
- [SDR CALA2024013100272](https://openairdocs.org/sdr/CALA2024013100272.md): Windshield · cracked · Jan 28, 2024 · N33289 · Boeing 737824 · Flight Compartment Windows
  > TWO CRACKS ON INNER PANE OF CAPTAIN L1 WINDSHIELD. PICS LOG PAGE FLAGGED FOR SDR VERIFIED TAP ON TB5010 IS ON #1 FOR NEW WINDOW H13 IAW AMM 30-41-21-000-801 REMOVED WINDOW IN REFERENCE WITH AMM 56-11-11. CLEANED MATING SECTIONS IN PREPARATION FOR WINDOW INSTAL
- [SDR CALA2023112703480](https://openairdocs.org/sdr/CALA2023112703480.md): Lens · missing · Nov 26, 2023 · N33289 · Boeing 737824 · Exterior Lighting
  > LEFT RETRACTABLE LANDING LIGHT BULB AND LENS FOUND MISSING. SEE LP 6397094 FOR CDL PIC ADDED. LEFT RETRACTABLE LANDING LIGHT IS EXTENDED AND THE LENS IS MISSI NG UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDAT
- [SDR CALA2022080501977](https://openairdocs.org/sdr/CALA2022080501977.md): Door Knob · warning light · Aug 5, 2022 · N33289 · Boeing 737824 · Passenger/Crew Doors
  > REJECTED TAKEOFF FOR AFT DOOR LIGHT AT 60K DOOR HANDLE MOVED DOOR HANDLE RESET LGT OUT REF LP 9208377 AND LP 9206190 FOR ACCOMPLISHMENT
- [SDR CALA2021071201063](https://openairdocs.org/sdr/CALA2021071201063.md): Skin · damaged · Jul 9, 2021 · N33289 · Boeing 737824 · Fuselage Main, Plate/Skin
  > COMPLY WITH AVO 9046 FOR DAMAGE AT LOWER VHF ANTENNA. STEPS 1,2,3 AND STEP 6 PREVIOUSLY ACCOMPLISHED, REF L/P 6594015 AND L/P 6598025. HOLES, REMOVED MOUNT FITTING FASTENER HOLES, REMOVED FASTENER INCHES. NO DEFECTS FOUND. THIS COVERS AVO 9046 STEPS 5, 8, 12 A
- [SDR CALA2020032100669](https://openairdocs.org/sdr/CALA2020032100669.md): Bulkhead · canning · Mar 18, 2020 · N33289 · Boeing 737824 · Fuselage Main, Bulkhead
  > REF EA 5310-04639 REV F OP 002: STEP 1.2, APB 1016 WEB "OIL CANNING" BETWEEN STRINGERS 9R AND 11R APPRO 10" LONG, 4.5" WIDE AND.250" DEEP AND BETWEEN STRINGERS 11R AND 12R APPRO 4" LONG, 3.5" WIDE AND.125" DEEP. NO NDI CRACK INDICATIONS NOTED. MARKED A/C REP
- [SDR CALA2020032100668](https://openairdocs.org/sdr/CALA2020032100668.md): Bulkhead · canning · Mar 18, 2020 · N33289 · Boeing 737824 · Fuselage Main, Bulkhead
  > REF EA5310-04639 REV F. OP 002: STEP 1.4. APB 1016 WEB "OIL CANN ING" BETWEEN STR 23R AND 25R. APPROX 6" LONG, 4.5" WIDE AND.100 " DEEP. NO NDI CRACK INDICATIONS NOTED. A/C REPAIRED IN REF TO SRM53-80-08 REPAIR 2 AND ECRA 5311-02414 REV -,FASTENER SUBSTITUTIO
- [SDR CALA2020030700581](https://openairdocs.org/sdr/CALA2020030700581.md): Pressure Panel · cracked · Mar 4, 2020 · N33289 · Boeing 737824 · Fuselage Main, Bulkhead
  > LT WHEEL WELL, FWD CENTER WING BOX. REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL 45.64 AND 40.00, ABOVE WL 192.0, HAS AN INDICATION OF A CRACK USING HFEC. MARKED. REF FLEETCYCLE N/R 9727325. REPAIRED DAMAGE IN REF TO SRM 57-10-10 REPAIR 3 ALTERNATIVE 3...GENERA
- [SDR CALA2020030700580](https://openairdocs.org/sdr/CALA2020030700580.md): Vapor Barrier · cracked · Mar 4, 2020 · N33289 · Boeing 737824 · Fuselage Main, Bulkhead
  > R/H WHEEL WELL UPPER VAPOR BARRIER CRACKED AT APPROX RBL 43 AND RBL 33....TEMP REPAIR INSTALLED IN REF TO ECRA5710-02658 AND FLEET CYCLE N/R# 9729278 REPAIRED DAMAGE IN REF TO SRM 57-10-10 REPAIR 3 ALTERNATIVE 2....GENERATED DIP PER TABLE 205 PG 217...INSPECTI
- [SDR CALA2020022980505](https://openairdocs.org/sdr/CALA2020022980505.md): Frame · cracked · Feb 21, 2020 · N33289 · Boeing 737824 · Fuselage Main, Frame
  > STATION 480 RIGHT FRAME CRACKED AT PSU RAIL ATTACH BRACKET, LOCA TED BETWEEN S-8RT AND S-9RT IN CABIN. INSTALLED REPAIR AT FRAME STA 480 RIGHT PER ECRA 5310-07665. SEE WIPS BELOW FOR ALL PARTIAL WORK ACCOMPLISHED. SEE HANGAR FLEET CYCLE 9729175 FOR ALL WORK PE
- [SDR CALA2018022100726](https://openairdocs.org/sdr/CALA2018022100726.md): Oxygen Mask · damaged · Feb 21, 2018 · N33289 · Boeing 737824 · Passenger Oxygen System
  > OXYGEN MASK IN REAR OF AIRCRAFT RIPPED. REPLACED THE OXYGEN MASK ASSY, OK FOR SERVICE.
- [SDR CALA2018012900390](https://openairdocs.org/sdr/CALA2018012900390.md): Light · odor · Jan 29, 2018 · N33289 · Boeing 737824 · Passenger Compartment Lighting
  > UPON ARRIVAL CREW REPORTED AC BURNING SMELL COMING FROM EMERGENCY EXIT MIDDLE AREA OF THE MAIN CABIN, REMOVED 6 CEILING PANELS TO FIND SOURCE OF SMELL. NIGHT LIGHT ON TOP OF OVERHEAD BIN AT ROW 23 LEFT IS NOT SECURED DUE TO BROKEN BRACKET/LAMP HOLDER. BULB IS

Next page: https://openairdocs.org/aircraft/N33289/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 = 'N33289' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N33289/reports

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