# Service difficulty reports: N33294

A list on [N33294](https://openairdocs.org/aircraft/N33294.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 · 62 reports

- [SDR CALA2026060816874](https://openairdocs.org/sdr/CALA2026060816874.md): Battery Pack · inoperative · Jun 5, 2026 · N33294 · Boeing 737824 · Emergency Lighting
  > EMERGENCY PATH LIGHT - SEAT 7,8,10,11,12,14 INOPERATIVE T/S PER FIM: 33-50 TASK 801, R & R BATTERY PACK M1676 & CLEANED CONNECTORS, OPS CHECK GOOD REF AMM 33-51-06-960-805.
- [SDR CALA2026031114489](https://openairdocs.org/sdr/CALA2026031114489.md): Skin · dented · Mar 8, 2026 · N33294 · Boeing 737824 · Cargo/Baggage Doors
  > RESKIN FWD CARGO DOOR (REF AAR N/R 99998525). REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN PER REF SRM 51-40-02-0G-0 AND DWG 143A6110.
- [SDR CALA2026031014471](https://openairdocs.org/sdr/CALA2026031014471.md): Skin · dented · Mar 8, 2026 · N33294 · Boeing 737824 · Cargo/Baggage Doors
  > RESKIN AFT CARGO DOOR. REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN PER REF SRM 51-40-02-0G-0 AND DWG 146A6110. REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN PER REF SRM 51-40-02-0G-0 AND DWG 146A6110.
- [SDR CALA2026030914427](https://openairdocs.org/sdr/CALA2026030914427.md): Doubler · cracked · Mar 6, 2026 · N33294 · Boeing 737824 · Fuselage Main, Structure
  > EXTERNAL POWER RECEPTACLE DOOR CUTOUT CRACKED AT LWR FLANGE. ACCOMPLISHED REPAIR OF EXTERNAL POWER DOUBLER AT LOWER EDGE AS PER 53-10-15-2R-4.
- [SDR CALA2026030314254](https://openairdocs.org/sdr/CALA2026030314254.md): Rib · cracked · Mar 1, 2026 · N33294 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STAB RIB NR 9, STIFFENER NR 3 FOUND CRACKED ON THE INBD LOWER SIDE OF THE RIB. ACCOMPLISHED A REPAIR OF THE RIB IAW SRM 55-10-09-2R-4,
- [SDR CALA2026030214159](https://openairdocs.org/sdr/CALA2026030214159.md): Floorbeam · corroded · Feb 27, 2026 · N33294 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR STRUCTURE WITH CORROSION AT BS 986, RBL 44. ACCOMPLISHED A REPAIR OF BS 986.5 FLOORBEAM AT RBL 44 IAW ECRA 5370-01217, AND SRM 53-70-51-2R-4.
- [SDR CALA2026022614074](https://openairdocs.org/sdr/CALA2026022614074.md): Angle · cracked · Feb 23, 2026 · N33294 · Boeing 737824 · Wing Main, Frame Structure
  > FOUND CRACK IN THE RT WING REAR SPAR FIXED T/E DEFLECTION CONTROL RIB, FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB SUPPORT OTBD END RIVET TAIL. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.
- [SDR CALA2026031714622](https://openairdocs.org/sdr/CALA2026031714622.md): Skin · cracked · Feb 22, 2026 · N33294 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STAB LOWER SKIN, AT STAB STA 111.10, 11" FROM REAR SPAR, I/B ROW. CRACK LENGTH - 0.25". ACCOMPLISHED REPAIR ON RT STAB LOWER SKIN AT STA 111.10 IAW SRM 55-10-01-2R-11,
- [SDR CALA2026021713830](https://openairdocs.org/sdr/CALA2026021713830.md): Attach Angle · cracked · Feb 15, 2026 · N33294 · Boeing 737824 · Fuselage Main, Attach Fittings
  > CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT BS 663.75 AND APPROX LBL 9 HAS A CRACK. ACCOMPLISHED REPAIR OF CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE IAW SRM 57-10-10-2R-5.
- [SDR CALA2026021813855](https://openairdocs.org/sdr/CALA2026021813855.md): Angle · corroded · Feb 12, 2026 · N33294 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > CORROSION AT VERTICAL STABILIZER T/E AREA INTERNAL CAVITY OF BALANCE WEIGHT. ACCOMPLISHED REPLACEMENT OF ANGLE (STIFFENER) IAW SRM 51-40-02-0G-0.
- [SDR CALA2026021313758](https://openairdocs.org/sdr/CALA2026021313758.md): Structure · corroded · Feb 10, 2026 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR STRUCTURE WITH COOROSION AT L-2 DOOR. REPAIRED THE STRUCTURE BTWN BS 1006 - 887+7", LBL 53 IAW SRM 51-40-02-0G-0, & DWG 147A8501.
- [SDR CALA2026021313756](https://openairdocs.org/sdr/CALA2026021313756.md): Angle · corroded · Feb 10, 2026 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORRODED AFT WET AREA FLOOR ZEE ANGLE, RBL 37, BS 986+7. R & R ZEE ANGLE AT RBL 37 STA 986.5 AS PER SRM: 51-40-02.
- [SDR CALA2026021313754](https://openairdocs.org/sdr/CALA2026021313754.md): Floor Support · corroded · Feb 10, 2026 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORRODED AFT WET AREA FLOOR SUPPORT BTWN BS 947 - 967, LBL 25. R & R THE FLOOR SUPPORT SRM 51-40-02-0G-0.
- [SDR CALA2026021313752](https://openairdocs.org/sdr/CALA2026021313752.md): Angle · corroded · Feb 10, 2026 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORRODED AFT WET AREA FLOOR ZEE ANGLE, LBL 33, BS 986+7. R & R THE ZEE ANGLE IAW SRM 51-40-02-0G-0, & DWG 147A5700.
- [SDR CALA2026030214146](https://openairdocs.org/sdr/CALA2026030214146.md): Skin · dented · Feb 9, 2026 · N33294 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FOUND DENT BETWEEN BS 727J AND 747, BETWEEN STRINGER 21R AND 22R. ACCOMPLISHED SKIN REPAIR BETWEEN STA 727J &747 IAW SRM 53-00-01-2R-3,
- [SDR CALA2025102710567](https://openairdocs.org/sdr/CALA2025102710567.md): Wire Harness · broken · Oct 26, 2025 · N33294 · Boeing 737824 · Light System Wiring
  > ECONOMY PASSENGER SEAT EMERGENCY PATH LIGHTING (EPL) INSPECTION. SEATS 32 ABC EMERGENCY PATH LIGHT INOP REQUST TO DEFER SEAT 32ABC REF MEL 3319E. ALL SPEC NOTES FOR EMERG LIGHT ARE OPERABLE. INSTALLED PLACARD, REPLACED EPL SEAT HARNESS IAW IFM 25-22-55, OPS
- [SDR CALA2025072806981](https://openairdocs.org/sdr/CALA2025072806981.md): Power Supply · faulted · Jul 27, 2025 · N33294 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. RH AFT EMERGENCY LIGHTS WILL NOT STAY ON DURING TEST. REMOVED AND REPLACED RH (DR-R2) AFT EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06. OPS TEST NORMAL. OKAY FOR SERVICE.
- [SDR CALA2025071706673](https://openairdocs.org/sdr/CALA2025071706673.md): Static Inverter · faulted · Jul 14, 2025 · N33294 · Boeing 737824 · DC Generating System
  > REJECTED T/O DURING T/O ELEC LIGHT ILLUMINATED. PER FLT CREW VIA DISPATCH, RTO AT 30 KTS. STATIC INVERTER WAS REPLACED TWICE AND SPCU WAS REPLACED ONPERFORMED POWER CHECK ON FRONT OF STATIC INVERTER WITH 27.29V DC. POWER CHECK BETWEEN PIN 1 AND PIN 3 OF D46
- [SDR CALA2025060305219](https://openairdocs.org/sdr/CALA2025060305219.md): Transceiver · faulty · May 31, 2025 · N33294 · Boeing 737824 · Weather Radar System
  > WX RADAR + PWS FAIL. NO RESET REMOVED AND REPLACED WXR RADAR TRANSCEIVER REF AMM 34-43-41. OPS TEST GOOD. CLEANED BLOWER FAN, FOUND DIRTY. PARTS USED: 99-3443-9-0007,QTY:1 ADD EMP:U347678,U226537 ROTABLE PARTS CHG:TT # 1445633 SN OFF 9591 PN OFF 99-3443-9-0
- [SDR CALA2024090500574](https://openairdocs.org/sdr/CALA2024090500574.md): Controller · faulty · Sep 3, 2024 · N33294 · Boeing 737824 · Pneumatic Distribution System
  > DUCT PRESSURE INDICATION L AND R POINTERS NOT THE SAME (SPLIT), WITH EITHER POINTER BELOW 18 PSIG DURING TAKEOFF, CLIMB AND CRUI SE; THE ENGINE IS THE BLEED SOURCE REMOVED AND REPLACED THE #2 ENG BLEED AIR REGULATOR (BAR) COMPLIED WITH. IAW AMM 36-11-03. STILL
- [SDR CALA2024081400430](https://openairdocs.org/sdr/CALA2024081400430.md): Fire Detector · faulty · Aug 11, 2024 · N33294 · Boeing 737824 · Fire Detection
  > FLT CREW NOTED, EGT IS NOT INDICATED HI, ONLY LH ENG OVER HEAT LIGHT SHOWN. ENG IS NOT SHUTDOWN DURING FLT. PER FIM 26-10 TASK 811. USING APU BLEED, DID FAULT ISOLATION PROCEDURE. INSPECTED ANY HEAT DAMAGE,PNEUMATIC DUCTING FOR CLAMP AND DUCT. HARNESS ASSEMBL
- [SDR CALA2024053101656](https://openairdocs.org/sdr/CALA2024053101656.md): Autopilot Sys · malfunctioned · May 27, 2024 · N33294 · Boeing 737824 · Auto Flight System
  > AUTOPILOT DOES NOT ENGAGE WHEN CMD SWITCH IS PUSHED, SWITCH LIGH TS DO NOT COME ON AND CMD STATUS DOES NOT SHOW ON THE FLIGHT MOD E ANNUNCIATOR CMD A OR CMD B PERFORM LAND VERIFY TEST PER MM 22-11-00-700-801, TEST PASS.
- [SDR CALA2022102802992](https://openairdocs.org/sdr/CALA2022102802992.md): Fairing · missing · Oct 28, 2022 · N33294 · Boeing 737824 · Fuselage Main, Structure
  > PDA 3 ON WALK AROUND FOUND RT BODY FAIRING PANEL 194CR MISSING FROM AIRCRAFT UPDATED WITH PICTURES INSTALLED NEW PANEL 194CR. RETURN TO SERVICE.
- [SDR CALA2022081602107](https://openairdocs.org/sdr/CALA2022081602107.md): Antenna · faulted · Aug 15, 2022 · N33294 · Boeing 737824 · Central Warning
  > TAKEOFF WARNING HORN REMAINED ON AFTER GO AROUND AND ONLY SILENCED AFTER PUTTING GEAR DOWN REF LOG PAGE 9309820 FOR REPAIR AND COMPLETION OF LAND VERIFY.....RADIO ALTIMETER AT FAULT RADIO ALTIMETER ANTENNAS REPLACED ALL DOCUMENTED ON LOG PAGE 9309820 REF PSEU
- [SDR CALA2022041400985](https://openairdocs.org/sdr/CALA2022041400985.md): Position Sensor · failed · Apr 14, 2022 · N33294 · Boeing 737824 · Trailing Flap Position Indicating System
  > FLAPS ASSYMETRY AT ABOUT 2. FSEU BITE 27-51 TASK 801 NO FALTS NOTED FLAPS SLATS OPS CHECKS GOOD A/C OK TO CONTINUE WANG, CHANG-CHOU (V923950) PERFORMED FSEU BITE 27-51 TASK 801 NO FALTS NOTED FLAPS SLATS OPS CHECKS GOOD A/C OK TO CONTINUE ADD EMP:V923950. REPL
- [SDR CALA2022041400982](https://openairdocs.org/sdr/CALA2022041400982.md): Fseu · failed · Apr 14, 2022 · N33294 · Boeing 737824 · Trailing Flap Position Indicating System
  > FLAP DISAGREE 7 INDICATE D WITH 15 SELECTED USED ALT FLAP EXTENS ION TO MANUALLY SELECT FLAPS 15 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN ACCOMPLISH FSEU BITE, CONTACT TOMC. R/R FSEU AMM 27-51-00. OPS CHECK GOOD ADD EMP:U155442 ROTABLE PARTS CHANGE WAS IN
- [SDR CALA2022040800922](https://openairdocs.org/sdr/CALA2022040800922.md): Control Valve · leaking · Apr 7, 2022 · N33294 · Boeing 737800* · Leading Edge Slat Position Indicating System
  > LEADING EDGE SLATS 4 AND 5 FAILED TO RETRACT CAUSING SUBSEQUENT FLAP BYPASS VALVE ACTIVATION AND AIR RETURN. DFD DATA SHOWS THAT THEY NEVER MADE IT BACK TO THE MID EXTEND POSITION MET THE CREW AFTER AIR RETURN. THEY SHOWED ME THAT ALL LEADING EDGE DEVICES DID
- [SDR CALA2021042200515](https://openairdocs.org/sdr/CALA2021042200515.md): Housing · gouged · Apr 20, 2021 · N33294 · Boeing 737824 · Cargo/Baggage Doors
  > FWD CARGO DOOR EXTERIOR HANDLE MOUNT HOUSING GOUGED REF AAR N/R 9614520 MEASURED GOUGE ON FWD CARGO DOOR HANDLE HOUSING AND FOUND OUT OF LIMITS PER ECRA 5232-01071 REV B MAT LOSS.068 MAX MAT LOSS ALLOWED.060 REMOVED AND RPELACED HOUSING P/N 103654-1 PER B737
- [SDR CALA2021041600484](https://openairdocs.org/sdr/CALA2021041600484.md): Skin · cracked · Apr 16, 2021 · N33294 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON R/H HORIZ STAB LWR IN-SPAR SKIN PANEL RIB STA 147.90, 16" FWD ON T/E INBD OF INBD RIVET LINE (CRACK LENGTH 1") REPAIRED LOWER INSPAR SKIN PANEL RIB STA 147.90 AS PER REF B737 SRM 55-10-01 REPAIR 11 FIG 204 F THIS IS CATEGORY B REPAIR THAT REQ. S
- [SDR CALA2021041600470](https://openairdocs.org/sdr/CALA2021041600470.md): Skin · cracked · Apr 14, 2021 · N33294 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON R/H HORIZ STAB LWR IN-SPAR SKIN PANEL RIB STA 147.90, 16" FWD ON T/E INBD OF INBD RIVET LINE (CRACK LENGTH 1") REPAIRED LOWER INSPAR SKIN PANEL RIB STA 147.90 AS PER REF B737 SRM 55-10-01 REPAIR 11 FIG 204 F THIS IS CATEGORY B REPAIR THAT REQ. S
- [SDR CALA2021040800438](https://openairdocs.org/sdr/CALA2021040800438.md): Skin · cracked · Apr 8, 2021 · N33294 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON L/H HORIZONTAL STAB LOWER IN-SPAR SKIN PANEL RIB STA 147-90 18IN FWD OF THE T/E I/B RIVET LINE CRACK LENGTH 1IN REF AAR N/R 9614381 REPAIRED L/H HORIZONTAL STAB LOWER IN-SPAR SKIN PANEL RIB STA 147-90 18IN FWD OF T/E AS PER REF B737 SRM 55-10-01
- [SDR CALA2021040600432](https://openairdocs.org/sdr/CALA2021040600432.md): Pressure Web · cracked · Apr 6, 2021 · N33294 · Boeing 737824 · Fuselage Main, Bulkhead
  > 2EA CRACKS FOUND AT EXTERNAL CENTER WING REAR SPAR VERTICAL PRESSURE WEB CRACK NO.1 LOCATED BETWEEN LBL 45.64 TO LBL 40.00 LENGTH OF CRACK APPROX 1IN. CRACK NO.2 LOCATED BETWEEN LBL 31.83 TO LBL 24.92 LENGTH OF CRACK APPROX.400IN REF AAR N/R 9614270 REAPAIRED
- [SDR CALA2021032200354](https://openairdocs.org/sdr/CALA2021032200354.md): Floor Support · cracked · Mar 20, 2021 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > INTERCOASTAL CRACKED BETWEEN STA 380 AND STA 400 LBL 13 REF AAR N/R 9614549 REMOVED AND REPLACED UPPER CHORD INTERCOSTAL BETWEEN STA 380 AND 400 LBL 13 I.A.W B737 SRM 51-40-02 AND DWG 143A5400 WORK ACCOMPLISHED BY V894481
- [SDR CALA2021032200349](https://openairdocs.org/sdr/CALA2021032200349.md): Floor Support · cracked · Mar 19, 2021 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > INTERCOASTEL CRACKED AT BL0 BETWEEN STA 294 AND STA 277 REF AAR N/R 9614545 REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FLOOR STRUCTURE BL 0 BETWEEN STA 294 AND STA 277 PER REF B737 SRM 51-40-02, 51-10-02 AND DWG 141A5400 WORK ACCOMPLISHED BY V894481
- [SDR CALA2021031600322](https://openairdocs.org/sdr/CALA2021031600322.md): Intercostal · cracked · Mar 16, 2021 · N33294 · Boeing 737824 · Fuselage Miscellaneous Structure
  > INTERCOASTAL CRACKED JUST I/B OF L-1 DOOR THRESHOLD BETWEEN STA 312 AND STA 329 REF AAR N/R 9614516 REMOVED AND REPLACED THE INTERCOASTAL AT I/B OF L-1 DOOR THRESHOLD BETWEEN STA 312 TO STA 328 PER REF B737 SRM 51-40-02 AND DWG 141A5400 AND UNITED ECRA 5310-06
- [SDR CALA2020021700458](https://openairdocs.org/sdr/CALA2020021700458.md): Module · malfunctioned · Feb 17, 2020 · N33294 · Boeing 737824 · Waste Disposal System
  > TOILET FLUSH SYSTEM DOES NOT FLUSH FWD LH LAV A THIS IS 2ND LAV NOT OPERATING. INDIC. IS RED ON TANK ON FA SCRE EN AFT. SERVICED LAV SYSTEM, RESET LAV FLUSH MODULE ON BOWL. SYSTEM OPS CHECK NORMAL 10 CONSECETIVE FLUSHES. REF AMM 38-32-00
- [SDR CALA2020020300316](https://openairdocs.org/sdr/CALA2020020300316.md): Lens · inaccurate · Feb 1, 2020 · N33294 · Boeing 737824 · Emergency Lighting
  > EXIT IDENTIFIERS AT SEATS 21A AND 20A INSTALLED WITH ARROWS POINTING IN WRONG DIRECTION. REMOVED AND REPLACED EXIT IDENTIFIERS WITH CORRECT ARROWS AT SEATS 20A AND 21A. REF IPC 33-51-01-16.
- [SDR CALA2019122102253](https://openairdocs.org/sdr/CALA2019122102253.md): Power Supply · inoperative · Dec 20, 2019 · N33294 · Boeing 737824 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS ON IN ARMED POSITION FOUND CB P18-3 B10 POPPED CAUSED BY BATTERY CHARGER AT DATO PANEL 27F INOP AND SMOKING, WILL NEED TO BE REPLACED, LEFT TWO NEW BATTERIES IN COCKPIT FOR BAD BATTERY CHARGER. REPLACED POWER SUPPLY AT SEAT ROW 27 RE
- [SDR CALA2019032500475](https://openairdocs.org/sdr/CALA2019032500475.md): Adiru · failed · Mar 25, 2019 · N33294 · Boeing 737824 · Inertial Guidance System
  > RT ADIRU FAULT LIGHT ILLUMINATED, AC DIVERTED IN. PILOTS INDICATED BOTH AP INOP. REMOVED AND REPLACED NR 2 ADIRU REF AMM 34-21-01-400-801 DFCS AND LAND VERIFY TEST PASSED. OPS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1184821 SN OFF 2251 UNIT, ADI
- [SDR CALA2018102902219](https://openairdocs.org/sdr/CALA2018102902219.md): Transceiver · failed · Oct 29, 2018 · N33294 · Boeing 737824 · Weather Radar System
  > AIR RETURN FOR WEATHER RADAR FAILURE. REMOVED FAULTY TRANSCEIVER BLOWER PER AMM 34-43-51. REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER PER AMM 34-43-41. OPS CHECKED GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1597514 SN OFF 9106 TRANSCEIVER, WX OFF 99-
- [SDR CALA2017090102984](https://openairdocs.org/sdr/CALA2017090102984.md): Unknown · odor · Sep 1, 2017 · N33294 · Boeing 737824 · Air Distribution System
  > SMOKE OR FUMES IN CABIN, SOURCE UNKNOWN. SMELLED FUMES/ODOR DURING DESCENT BELOW 18000 THRUST LEVER IDLE CREW DEBRIEF REVEALS, ODOR MORE OILY AND SMOKEY. ONLY DURING INITIAL DECENT. PERFORMED SMOKE ODOR IN FLT DECK/CABIN CHECK PER AMM 05-51-26. NO DEFECTS.
- [SDR CALA2017090102967](https://openairdocs.org/sdr/CALA2017090102967.md): Engine · contaminated · Sep 1, 2017 · N33294 · Boeing 737824 · Engine (Turbine/Turboprop)
  > SMOKE OR FUMES IN CABIN, SOURCE UNKNOWN. FUMES ODOR IN COCKPIT DURING DECENT POWER AT IDLE. ALSO AFTER TAKEOFF. CHECKED BOTH ENGS ON ARRIVAL. FOUND THE NR 1 ENGINE EXCESSIVE FAN BLADE LUBRICANT AND ENGINE OIL LEVEL IS HIGH. WIPED OFF EXCESSIVE LUBRICANT ON
- [SDR CALA2017081802783](https://openairdocs.org/sdr/CALA2017081802783.md): Power Supply · inoperative · Aug 18, 2017 · N33294 · Boeing 737824 · Emergency Lighting
  > EMERGENCY AISLE LIGHTS ROW 36,37,38 ABC INOP. REMOVED AND REPLACED ''M1672'' EMERGENCY POWER SUPPLY W/ BATTERY PACK PER WDM REF 33-51-12 AMM REF 33-51-06. OPERATIONALLY TEST NORMAL AT THIS TIME.
- [SDR CALA2017081802782](https://openairdocs.org/sdr/CALA2017081802782.md): Light · inoperative · Aug 18, 2017 · N33294 · Boeing 737824 · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED BULB OPS CHECK OK.
- [SDR CALA2017042101102](https://openairdocs.org/sdr/CALA2017042101102.md): Lamp · inoperative · Apr 21, 2017 · N33294 · Boeing 737824 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AFT OF THE R2 DOOR FOUND INOPERATIVE. REPLACED THE LAMPS, OPS NORMAL.
- [SDR CALA2016090600633](https://openairdocs.org/sdr/CALA2016090600633.md): Lamp · inoperative · Sep 6, 2016 · N33294 · Boeing 737824 · Emergency Lighting
  > EXTERIOR R1 EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR CALA2016062700384](https://openairdocs.org/sdr/CALA2016062700384.md): Power Supply · inoperative · Jun 24, 2016 · N33294 · Boeing 737824 · Emergency Lighting
  > SEATS 36C THROUGH 38C AISLE FLOOR EMERGENCY PATH LIGHTING INOPERATIVE. R & R POWER SUPPLY/CHARGER ASSY EQUIPMENT M1672 IAW AMM 33-51-06. NOW OPS CKS GOOD.
- [SDR CALA2015071500571](https://openairdocs.org/sdr/CALA2015071500571.md): Seat Track · cracked · Jul 14, 2015 · N33294 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 727B, RBL 45.50 IS CRACKED AT FASTENER HOLES COMMON TO SPLICE STRAP. THE REPAIR IAW EA 5320-02076 REV I, DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. SEE WIPS FOR DETAILS OF WORK ACCOMPLISHED. TRIM
- [SDR CALA2015071500570](https://openairdocs.org/sdr/CALA2015071500570.md): Seat Track · cracked · Jul 14, 2015 · N33294 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 727B, RBL 24.75 IS CRACKED AT FASTENER HOLES COMMON TO SPLICE STRAP. THE REPAIR IAW EA 5320-02076 REV I, DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. SEE WIPS FOR DETAILS OF WORK ACCOMPLISHED. TRIM
- [SDR CALA2015071500569](https://openairdocs.org/sdr/CALA2015071500569.md): Seat Track · cracked · Jul 14, 2015 · N33294 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STATION 727B, LBL 45.50 IS CRACKED AT FASTENER HOLES COMMON TO SPLICE STRAP. THE REPAIR IAW EA 5320-02076 REV I, DOES NOT ALLOW FOR PROPER EDGE DISTANCE OF THE 4 FASTENER HOLES IN THE SEAT TRACK. SEE WIPS FOR DETAILS OF WORK ACCOMPLISHED. TRIMM

Next page: https://openairdocs.org/aircraft/N33294/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 = 'N33294' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N33294/reports

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