# Service difficulty reports: N73275

A list on [N73275](https://openairdocs.org/aircraft/N73275.md).

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

- [SDR CALA2026061217062](https://openairdocs.org/sdr/CALA2026061217062.md): Skin · damaged · Jun 5, 2026 · N73275 · Boeing 737824 · Fuselage Main, Plate/Skin
  > INSPECTION REQUIREMENTS OF THE LATEST VERSION OF ECRA 5310-08928 PRIOR TO JUNE 03, 2027. PERFORM PART 2 - INSPECTION REQUIREMENTS OF THE LATEST VERSION OF ECRA 5310-08928 PRIOR TO JUNE 03, 2027.
- [SDR CALA2025122312314](https://openairdocs.org/sdr/CALA2025122312314.md): Battery Pack · inoperative · Dec 20, 2025 · N73275 · Boeing 737824 · Emergency Lighting
  > RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. ATTEMPTED TO REMOVE COVER BUT 2 NUT PLATES WERE BROKEN IN THE BACK. COMPLETED UP TO STEP 5 OF THE RH AFT EMERGENCY WING LIGHT ASSEMBLY REF AMM 33-51-04-960-802. COMPLETED LIGHT ASSY INSTALL UP TO STEP G12 AMM 33
- [SDR CALA2025112711522](https://openairdocs.org/sdr/CALA2025112711522.md): Skin · debonded · Nov 26, 2025 · N73275 · Boeing 737824 · Trailing Edge Flaps
  > RIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN DEBONDED SIGNAL NOTED, AREA L=1X1.25 INCHES. CLEANED, PREPPED, REPAIRED & RESTORED PAINT AT RT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN IAW SRM 57-5 3-01-2R-16, SRM 51-70-10-2R-0, AMM 51-21-41-370
- [SDR CALA2025112811574](https://openairdocs.org/sdr/CALA2025112811574.md): Skin · cracked · Nov 18, 2025 · N73275 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED L=0.855INCH APROX. AT STAB STA157.10 AND 9 INCH FROM AFT SPAR (REF AAR NR 1000060368)PERFORMED PERMANENT REPAIR AT RH HORIZONTAL STAB AT STAB STA157.10 AND 9 INCH FROM AFT SPARTHIS REPAIR IS A CATEGORY "B",
- [SDR CALA2025112811573](https://openairdocs.org/sdr/CALA2025112811573.md): Skin · cracked · Nov 18, 2025 · N73275 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED L=1INCH APROX. AT STAB STA147.90 AND 15.600 INCH FROM FWD SPAR (REF AAR NR 1000060354) PERFORMED PERMANENT REPAIR AT LT HORIZONTAL STAB AT STAB STA147.90 AND 15.600 INCH FROM FWD SPAR THIS REPAIR IS A CATEG
- [SDR CALA2025112711501](https://openairdocs.org/sdr/CALA2025112711501.md): Skin · not reported · Nov 18, 2025 · N73275 · Boeing 737824 · Cargo/Baggage Doors
  > RE-SKIN FWD CARGO DOOR. REMOVED AND REPLACED FWD CARGO DOOR SKIN, ALL WORK PERFORMED IAW SRM 52-30-01-2R-3
- [SDR CALA2025112711499](https://openairdocs.org/sdr/CALA2025112711499.md): Skin · deformed · Nov 18, 2025 · N73275 · Boeing 737824 · Cargo/Baggage Doors
  > RE-SKIN AFT CARGO DOOR. REMOVED AND REPLACED AFT CARGO DOOR SKIN, ALL WORK PERFORMED IAW SRM 52-30-01-2R-3.
- [SDR CALA2025093009438](https://openairdocs.org/sdr/CALA2025093009438.md): Cargo Net · torn · Sep 28, 2025 · N73275 · Boeing 737824 · Cargo Compartments
  > FORWARD CARGO COMPARTMENT BIN THREE CARGO NET TORN. REFERENCE AIRCRAFT MAINTENANCE MANUAL FOUND CARGO NET TO BE SERVICEABLE. REPAIR OR REPLACE CARGO NET WITHIN 10 DAYS IN REFERENCE WITH AMM 25-52-04-200-801C1.
- [SDR CALA2025063006079](https://openairdocs.org/sdr/CALA2025063006079.md): Toilet · leaking · Jun 27, 2025 · N73275 · Boeing 737824 · Waste Disposal System
  > LAV D FLUSHES CONTINUE OUSLY REF FIM 38-30 TASK 816 VERIFIED NO CLOG VERIFIED RINSE VALVE OPENS AND CLOSES SUSPECT FLUSH CONTROL ASSEMBLY NEEDS TO BE CHANGED REQUEST MEL 3802D REQUESTING MEL TOILET VALVE MANUALLY CLOSED IN ACCORDANCE WITH MEL. SLAVE IN LAV FL
- [SDR CALA2025040203427](https://openairdocs.org/sdr/CALA2025040203427.md): Switch · faulted · Apr 2, 2025 · N73275 · Boeing 737824 · Door Warning System
  > FWD CARGO DOOR LIGHT WILL NOT EXTINGUISH WHEN DOOR IS CLOSED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN, PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V950348 MAC RELATED WORK ORDER 000000003132931 AND PRTR DOOR CONFI
- [SDR CALA2024100302539](https://openairdocs.org/sdr/CALA2024100302539.md): Strip · missing · Sep 30, 2024 · N73275 · Boeing 737824 · Horizontal Stabilizer Miscellaneous Structure
  > OUTBOARD END OF R ELEVATOR APPEARS TO HAVE SHEET METAL DAMAGE A ND SEPARATION PHOTO UPDATE. DAMAGE IS TO THE RH HORIZONTAL STAB T/E PANEL CONDUCTIVE STRIP. THE DAMAGE EXCEEDS THE ALLOWABLE LIMITS IN SRM 55-10-01 ALLOWABLE DAMGE 3 AND FIG 9. PARTS USED: 99-236
- [SDR CALA2024052301567](https://openairdocs.org/sdr/CALA2024052301567.md): Stringer · cracked · May 16, 2024 · N73275 · Boeing 737824 · Wing, Longeron/Stringer
  > L/H WING BETWEEN RIBS 19 AND 20 UPPER STRINGER # 8 CRACKED AT TIP. SUPPORT TASK NSA EMX N/R 00222 ADDED SDR BLOCK CUT OUT DAMAGED SECTION OF U8 STRINGER AND REPAIRED.
- [SDR CALA2024051701495](https://openairdocs.org/sdr/CALA2024051701495.md): Angle · cracked · May 8, 2024 · N73275 · Boeing 737824 · Fuselage Structure (General)
  > L/H PACK BAY AFT WALL REAR SPAR UPPER ANGLE CRACKED. SUPPORT TASK NSA EMX N/R00196.
- [SDR CALA2024051601489](https://openairdocs.org/sdr/CALA2024051601489.md): Angle · cracked · May 8, 2024 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > R/H PACK BAY AFT WALL REAR SPAR UPPER ANGLE CRACKED.SUPPORT TASK NSA EMX N/R00197.
- [SDR CALA2024051701494](https://openairdocs.org/sdr/CALA2024051701494.md): Fitting · cracked · May 7, 2024 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA. 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00201.
- [SDR CALA2024021500423](https://openairdocs.org/sdr/CALA2024021500423.md): Light · no test · Feb 14, 2024 · N73275 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - AFT SEAT MOUNTED EMERGENCY LIGHT AT ROW 20ABC DAMAGED. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT REF MM 33-51-11. OPS CK OK. PARTS USED: BR9644-12,QTY:1 VERIFIED IDT REQUIREMENTS
- [SDR CALA2023051701550](https://openairdocs.org/sdr/CALA2023051701550.md): Engine · faulted · May 15, 2023 · N73275 · Boeing 737824 · Engine Oil System (Airframe Furnished)
  > ENGINE 2 SHOWED 0 QTY DURING DESCENT ALONG WITH FLUCT PRESS. ENG PARAMETRS NRML. ADDITONAL CREW DEBRIEF: CREW DID NOT SHUT DOWN ENGINE, OIL PRESS URE REMAINED POSITIVE BUT DID FLUCTUATE FROM AMBER TO RED. ALL E NGINE PARAMETERS REMAINED NORMAL. PHOTOS OF LEAKI
- [SDR CALA2023022400536](https://openairdocs.org/sdr/CALA2023022400536.md): Forging · none · Feb 23, 2023 · N73275 · Boeing 7378 · Fuselage Structure (General)
  > FOR ESFR REPORTING ONLY. EA 5310-04554 REV B OP005 ACCOMPLISHED FOR LH #1 WINDOW FRAME. EA 5310-04554 REV B OP005 REPAIR ACCOMPLISHED FOR CONFIG B.
- [SDR CALA2023011600122](https://openairdocs.org/sdr/CALA2023011600122.md): Sensor · defective · Jan 14, 2023 · N73275 · Boeing 737824 · Stall Warning System
  > LOST CAPT VERTICAL F/D SPD LIM INDICATED ON PFD ALL SPD INDS AGG REED THEN LEFT STICKSHAKER LOG UPDATED AS INFO CONTAINED ON TOCS: BITE PERFORMED, SMYD PERFORMED LEFT AND RIGHT ADIRS BITE TEST, NO FAULTS FOUND....BITE ALSO SHOWED MULTIPLE ALTITUDE DISAGREE FA
- [SDR CALA2023011600120](https://openairdocs.org/sdr/CALA2023011600120.md): Sensor · faulted · Jan 14, 2023 · N73275 · Boeing 737824 · Stall Warning System
  > AUTO SLAT FAIL LT ILLUM DURING RECALL. EXTINGUISHES WHEN MC LIGH T PRESSED FSEU BITE SHOWS NO FAULTS, #2 SYMD SHOWS NO FAULTS, #1 SYMD FIM 27-32-809. PLACE #1 AUTOSLAT SYSTEM INOP PER MEL 2712A, DDP PLACED ON MEL 2712A, DDP C/W. SHOWS FAULT MSG 27-31004 AOA SE
- [SDR CALA2022111403128](https://openairdocs.org/sdr/CALA2022111403128.md): Flange · cracked · Nov 13, 2022 · N73275 · Boeing 737824 · Horizontal Stabilizer Structure
  > LT HORIZ STAB INTERNAL HORIZ FLANGE IS CRACKED STA 92.70.5" AFT OF STIFFENER #1 TO LWR SKIN ATTACHMENT. REPAIRED LH HORIZ STAB LOWER CHORD AT STA 92.70 AT STIFFENE #1 I AW SRM 55-10-09-2R5 REPAIR 5 FIG 202 AND 203. DATA WAS TRANSCRIB ED FROM PAPER DOC AERSALE
- [SDR CALA2022110203011](https://openairdocs.org/sdr/CALA2022110203011.md): Skin · cracked · Oct 31, 2022 · N73275 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > DURING C-SCAN INSPECTION AT GYR DURING D-CHECK, A CRACK WAS FOUND ON THE RH HORIZONTAL STABILIZER AT STA 157.10 23" FROM FORWARD SPAR, 17" FROM AFT SPAR. CRACK MEASURED.5". WORK TRANSCRIBED FROM AERSALE NON-ROUTINE 23985. 23 WITH NO DEFECTS NOTED. DOUBLER MAN
- [SDR CALA2022022800523](https://openairdocs.org/sdr/CALA2022022800523.md): Flap · none · Feb 28, 2022 · N73275 · Boeing 737800* · Trailing Flap Position Indicating System
  > *EMERGENCY DECLARED* PRIMARY FLAPS FAILED AT FLAP 1. EXTENDED FLAPS WITH ALTERNATE FLAP SYSTEM INSPECTED PER AMM 27-51-00-210-801. NO DAMAGE NOTED. PERFORMED FSEU BITE REF FIM 27-51 TASK 801. MSG 27-52259. PERFORMED FAULT ISOATION PER FIM 27-51 TASK 813. NO
- [SDR CALA2021052100700](https://openairdocs.org/sdr/CALA2021052100700.md): Lens · damaged · May 19, 2021 · N73275 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHT ON SEAT ROW 36 ABC LENS DAMAGED. REMOVED AND REPLACED WHITE EMERGENCY LIGHT REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS
- [SDR CALA2020072701069](https://openairdocs.org/sdr/CALA2020072701069.md): Engine · unknown · Jul 20, 2020 · N73275 · Boeing 737824 · Engine Indicating System
  > EGT, FF, OIL PRESSURE, AND OIL TEMPERATURE INDICATIONS CONTINUE TO SHOW AFTER ENGINE SHUTDOWN LEFT ENGINE ON MAX THRUST BLDS OFF T/O...EGT ENG 1 EXCEEDED LIMIT TO 988 AT ROTATION UNTIL THRUST REDUCTION CREW REPORTED EXTREMELY HOT DAY IN DEN, EGT SLOWLY CLIMBED
- [SDR CALA2020072701068](https://openairdocs.org/sdr/CALA2020072701068.md): Warning Message · multiple fail · Jul 20, 2020 · N73275 · Boeing 737824 · Central Warning
  > EGT, FF, OIL PRESSURE, AND OIL TEMPERATURE INDICATIONS CONTINUE TO SHOW AFTER ENGINE SHUTDOWN LEFT ENGINE ON MAX THRUST BLDS OFF T/O...EGT ENG 1 EXCEEDED LIMIT TO 988 AT ROTATION UNTIL THRUST REDUCTION CREW REPORTED EXTREMELY HOT DAY, EGT SLOWLY CLIMBED DURING
- [SDR CALA2019110981931](https://openairdocs.org/sdr/CALA2019110981931.md): Skin · cracked · Nov 7, 2019 · N73275 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > EA 5510-01843 REV H HORIZ STAB LOWER IN SPAR SKIN PANEL C-SCAN I NSP REVEALED 3 EA CRACKS LEFT HAND LOWER SURFACE 2 INBD SIDE OF STA 120.3, 9"-9.5" & 17"-18" AND 1 ON INBD SIDE OF STA 129.5 25" TO 26" ALL FWD OF REAR SPAR. REPAIRED 3 EA CRACKS ON HORIZ STAB LO
- [SDR CALA2019040500524](https://openairdocs.org/sdr/CALA2019040500524.md): Proximity Sensor · malfunctioned · Apr 2, 2019 · N73275 · Boeing 737824 · Leading Edge Slat Position Indicating System
  > LEADING EDGE SLATS TRANSIT LIGHT STAYS ON 1 LE TRANSIT LIGHT CYCLING ON/OFF WITH FLAPS UP #1 LE FLAP LIGHT ON OVHD & FWD LE FLAPS TRANSIT LIGHT ARE ON STEADY WITH FLAPS UP. FSEU BITE HAS MSG "F1 PROX RETRACT" 27-81216.F2 PROX RETRACT 27-81218 & F3 PROX RETRACT
- [SDR CALA2018110502303](https://openairdocs.org/sdr/CALA2018110502303.md): Latch · damaged · Nov 5, 2018 · N73275 · Boeing 737824 · Doors
  > PTY OPERATIONS ADVISED PNEUMATIC ACCESS DOOR HAS ONE INOP LATCH PLEASE SPEED TAPE AS PER ECRA AS DISCUSSED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V912214 MAC RELATED WORK ORDER 000000001624161 AND PRTR TECH PERF
- [SDR CALA2017041401011](https://openairdocs.org/sdr/CALA2017041401011.md): Light · inoperative · Apr 14, 2017 · N73275 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEAT ROW 20ABC AND BETWEEN SEAT ROWS 28DEF AND 29DEF IN BULLNOSE INOP. RELAMPED EMERGENCY LIGHTS AT SEAT ROW 20ABC AND BETWEEN SEAT ROWS 28DEF REF 33-42-02-960-801. OPS CHECK NORMAL.
- [SDR CALA2016111400903](https://openairdocs.org/sdr/CALA2016111400903.md): Altimeter · unserviceable · Nov 14, 2016 · N73275 · Boeing 737824 · Altimeter, Barometric/Encoder
  > AT FL310 CAPTAIN AND F/O ALTIMETER READ 3100, STANDBY ALTIMETER READS 30720. R&R STANDBY ALTIMETER PER AMM 34-13-01. A/C OK TO CONTINUE.
- [SDR CALA2016100700727](https://openairdocs.org/sdr/CALA2016100700727.md): Skin · cracked · Oct 6, 2016 · N73275 · Boeing 737824 · Elevator, Plate/Skin
  > LT HORIZONTAL STAB LOWER SKIN CRACKED AT HSS 101.90 AND ABOUT 12 INCHES FWD OF EXISTING REPAIR. INSTALLED REPAIR DOUBLER IAW SRM 55-10 -01 REPAIR 11.
- [SDR CALA2016100700725](https://openairdocs.org/sdr/CALA2016100700725.md): Skin · cracked · Oct 6, 2016 · N73275 · Boeing 737824 · Elevator, Plate/Skin
  > LEFT HORIZONTAL STAB SKIN CRACKED AT REAR SPAR BETWEEN HSS 92.7 AND 101.9. REPAIRED THE SKIN IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2016092700696](https://openairdocs.org/sdr/CALA2016092700696.md): Beam · cracked · Sep 26, 2016 · N73275 · Boeing 737824 · Service Doors
  > PERFORMED ALUMINUM SURFACE INSPECTION IAW SOPM 20-20-02 ON R1 DOOR FOUND LOWER BEAM IS CRACKED. REPAIRED. REMOVED AND REPLACED R1 DOOR LOWER BEAM IAW EC/ RA 5210-02750 AND SRM 51-40-02.
- [SDR CALA2015080700651](https://openairdocs.org/sdr/CALA2015080700651.md): Skin · damaged · Aug 5, 2015 · N73275 · Boeing 737824 · Fuselage Main, Plate/Skin
  > AIRCRAFT DAMAGE, SCRATCH AT RT SIDE STATION 500 D. TOMC CHANGED BACK TO 0275. TOMC CORRECTED ACFT NR TO REFLECT 0411. REMOVED DAMAGED AREA & INSTALLED INTERIM REPAIR IAW ECRA 5331-02041. DIP INITIATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 05 AUG 16
- [SDR CALA2014111901466](https://openairdocs.org/sdr/CALA2014111901466.md): Connector · disconnected · Nov 19, 2014 · N73275 · Boeing 737824 · Light System Wiring
  > LEFT AFT GALLEY EMER PATHWAY LIGHT INOPERATIVE, FOUND CONNECTOR D40044J DISCONNECTED. RECONNECTED CONNECTOR D40044J IAW SWPM 20-72-24 & AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.
- [SDR CALA2014111401447](https://openairdocs.org/sdr/CALA2014111401447.md): Battery Pack · discharged · Nov 13, 2014 · N73275 · Boeing 737824 · Emergency Lighting
  > FORWARD CABIN EMER LIGHTS INOPERATIVE. R & R PAX CABIN LIGHTING EMER CHARGER BATTERY PACK FWD IAW AMM 33-51-06. OPERATIONS CHECKED GOOD IAW AMM 33-51-0 6.
- [SDR CALA2014111401439](https://openairdocs.org/sdr/CALA2014111401439.md): Fitting · cracked · Nov 10, 2014 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SUPPORT TASK CRACK FOUND IN SEAT TRACK BATHTUB FITTING AT RT STATION 727B RBL 24.75. R & R BATHTUB FITTING AT RT STATION 727B RBL 24.75 IAW EA 5320-02076 & SRM 51-40-02.
- [SDR CALA2011091900609](https://openairdocs.org/sdr/CALA2011091900609.md): Bulkhead · dented · Sep 18, 2011 · N73275 · Boeing 737824 · Fuselage Main, Bulkhead
  > SUPPORT TASK - AFT PRESSURE BULKHEAD STA 1016 AFT SIDE AT APPROX STR 22R THERE IS A SHARP DENT FACING AFT (MARKED) AFT PRESS BLKD REPAIRED IAW ECRA 5310-05407. ACCOMP A PERMANENT REPAIR PRIOR TO 46,522 TOTAL FLT CYC'S. PLANNING TO CONTACT ENGINEERING AFTER
- [SDR CALA2011091200586](https://openairdocs.org/sdr/CALA2011091200586.md): Bracket · cracked · Sep 9, 2011 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > A/C BRACKET AT FRAME 380R INBOARD RIVET SHOWS CRACK INDICATION. REPAIRED A/C BRACKET AT FRAME 380R, REF EA 5310-04716 REV C.
- [SDR CALA2011090900583](https://openairdocs.org/sdr/CALA2011090900583.md): Bracket · cracked · Sep 9, 2011 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - A/C BRACKET AT FRAME 440R INBOARD RIVET SHOW CRACK INDICATION (ALSO VISUALLY). REPAIRED AS PER EA 5310-04716 REV C OP 2.
- [SDR CALA2011090800577](https://openairdocs.org/sdr/CALA2011090800577.md): Intercostal · cracked · Sep 7, 2011 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT LBL 44 BETWEEN FUSELAGE STA 328 & 344. REMOVED AND REPLACED CRACK INTERCOSTAL AT INDICATED AREA PER SRM 51-40-02.
- [SDR CALA2011090800576](https://openairdocs.org/sdr/CALA2011090800576.md): Intercostal · cracked · Sep 7, 2011 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT LBL 46 BETWEEN FUSELAGE STA 312 & 328. REMOVED AND REPLACED CRACK INTERCOSTAL AT INDICATED AREA PER SRM 51-40-02.
- [SDR CALA2011090800575](https://openairdocs.org/sdr/CALA2011090800575.md): Intercostal · cracked · Sep 7, 2011 · N73275 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT FUSELAGE FLOOR STA 312 TO 328 AT RBL 30. REMOVED AND REPLACED CRACK INTERCOSTAL AT INDICATED AREA PER SRM 51-40-02.
- [SDR CALA2010120300601](https://openairdocs.org/sdr/CALA2010120300601.md): Battery Pack · discharged · Dec 3, 2010 · N73275 · Boeing 737824 · Emergency Lighting
  > L-1 FWD EMERGENCY LIGHTS OUT. R&R BATTERY PACK REF AMM 33-51-06, OPS CHECKS GOOD.
- [SDR CALA2009121800738](https://openairdocs.org/sdr/CALA2009121800738.md): Power Supply · inoperative · Dec 18, 2009 · N73275 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS AT LEFT AFT OVERWING AND DIRECTLY AFT OF LEFT WING ARE INOPERATIVE. T/S PER WD 33-51-13 AND FOUND EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY PACK BAD, REPLACED BOTH. CHECKS NORMAL.
- [SDR CALA2009092500571](https://openairdocs.org/sdr/CALA2009092500571.md): Battery Pack · discharged · Sep 25, 2009 · N73275 · Boeing 737824 · Emergency Lighting
  > L1 AND L2 DOORS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FRONT LEFT AND AFT LEFT EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS IAW AMM 33-51-06. OPS CHECKS GOOD.
- [SDR CALA2009080600437](https://openairdocs.org/sdr/CALA2009080600437.md): Skin · cracked · Aug 5, 2009 · N73275 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN CRACK STATION SS 101.90 RUNNING FWD AND AFT "1" LENGTH C SCAN. (AFT I/B OF 3RD DRAIN HOLE) PER ECRA 5510-02042. NEED TO ACCOMPLISH AN INITIAL INSPECTION PRIOR TO 17,137 FLIGHT CYCLES AND THEN REPEAT INSPECTION AT INTE

## 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 = 'N73275' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N73275/reports

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