# Service difficulty reports: N73259

A list on [N73259](https://openairdocs.org/aircraft/N73259.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 · 77 reports

- [SDR CALA2026081818705](https://openairdocs.org/sdr/CALA2026081818705.md): Proximity Sensor · faulted · Aug 16, 2026 · N73259 · Boeing 737824 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF GEAR UP & OFF NOSE GEAR RED LT ONLY. CHECKLIT RAN NOSE GEAR GREEN RETURN TO AIRPORT THREE FAULTS FOUND IN BITE TEST OF PSEU. ERROR MSG: NOSE LKD A FAULT (MESSAGE#32 - 61003), NOSE LKD B FAULT (MESSAGE# 32-61010), DO NOT DISPATCH (MESSAGE# 32-6400
- [SDR CALA2026070917623](https://openairdocs.org/sdr/CALA2026070917623.md): Pump · faulted · Jul 7, 2026 · N73259 · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC PRESSURE INDICATION BELOW 2800 PSI SYSTEM A LOW PRESSURE LIGHT ON ENG 1 EDP IMMEDIATELY AFTER TAKE OFF. LIGHT STAYED ON. PUMP TURNED OFF IAW CHECKLIST. PUMP SEEMED TO OPS NORMAL. WHEN GEAR HANDLE PLACED UP DURING T/O, LOW PRESSURE LIGHT FOR ELECTR
- [SDR CALA2026051816345](https://openairdocs.org/sdr/CALA2026051816345.md): Fuse · failed · May 14, 2026 · N73259 · Boeing 737824 · Emergency Lighting
  > ROW 7-14 EMERGENCY PROXIMITY LIGHTS INOP. FOUND FAULTY FUSE ON POWER SUPPLY, REPLACED FUSE REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR CALA2026041615416](https://openairdocs.org/sdr/CALA2026041615416.md): Engine · vibration · Apr 13, 2026 · N73259 · Boeing 737824 · Engine (Turbine/Turboprop)
  > RETURN TO IAH FOR VERY HIGH AND AUDIBLE ENGINE VIBRATION IND WAS AS AT TOP OF SCALE MAXED OUT AFTER VISITING WITH THE PILOTS, THE VIBRATION INDICATIONS WERE COMING FROM THE RT ENG ONLY. RESONANCE SOUNDS WERE DISTINCTLY COMING FROM THE RIGHT SIDE. NO VIBRATI
- [SDR CALA2026030614388](https://openairdocs.org/sdr/CALA2026030614388.md): Battery Pack · inoperative · Mar 6, 2026 · N73259 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS, BATTERY PACK M1695 FAILED A CAPACITY CHECK. TEST SWITCH ON POWER SUPPLY INOPERATIVE. REPLACED AND OPS CHKD GOOD CHARGER ASSY ON POWER SUPPLY M1695 IAW AMM 33-51-06-960-806. REINSTALLED DADO PANEL FOR M1695 POWER SUPPLY ACCESS, IAW AMM 21-
- [SDR CALA2025101009895](https://openairdocs.org/sdr/CALA2025101009895.md): A/C Pack · odor · Oct 9, 2025 · N73259 · Boeing 737824 · Cabin Cooling System
  > DANK SMELL COMING FROM PACKS AT LOW ALTITUDES W/ RAM DOORS OPEN RAN THE PACKS FOR DURATION OF 20MIN, SMELL WENT AWAY. REF FIM 21-00 TASK 806.
- [SDR CALA2025082007961](https://openairdocs.org/sdr/CALA2025082007961.md): Girt Bar · out of limits · Aug 17, 2025 · N73259 · Boeing 737824 · Emergency Equipment
  > EXCESS SLIDE MATERIAL ABOVE GIRT BAR DOOR 1R. RETUCKED GIRT Z-FOLD TO PROPER GIRT PAYOUT DIMENSION PER AMM 25-66-01-400-801 D (2)(C)(D).
- [SDR CALA2025041703932](https://openairdocs.org/sdr/CALA2025041703932.md): Potable Water · odiferous · Apr 15, 2025 · N73259 · Boeing 737824 · Potable Water System
  > WATER SUPPLY IN LAVATORY POOR QUALITY AFT RH LAV E DRAINED AND SERVICEDTHE PORTABLE WATER SYSTEM A COUPLE OF TIMES AND RAN THE WATER FAUCETS AT ALL LAVATORIES. NO BAD SMELLS OR SINGS OF WATER CONTAMINATION WERE FOUND. REF AMM 38-10 TASK 810
- [SDR CALA2025022402422](https://openairdocs.org/sdr/CALA2025022402422.md): Light · detached · Feb 22, 2025 · N73259 · Boeing 737824 · Emergency Lighting
  > LAV D AFT LOWER EMERGENCY LIGHT BROKE OFF UPON REMOVAL REMOVED AND REPLACED LAV D EMERGANCY LIGHT. IAW B737 AMM 33-51-14 OPS TEST GOOD NO DEFECTS NOTED.
- [SDR CALA2024122303144](https://openairdocs.org/sdr/CALA2024122303144.md): Elec Connector · damaged · Dec 20, 2024 · N73259 · Boeing 737824 · Light System Wiring
  > SEAT ROW 14ABC EPL HAS EXPOSED WIRE AND ALSO MISSING LOCKING MECHANISM ON THE CONNECTOR. SUPPORT TASK NSA EMX N/R 00120.SECURED SEAT ROW 14ABC EEPL SHIPSIDE WIRING IAW B737-800 SWPM 20-10-11. REMOVED SEAT ROW 14ABC SEAT SIDE EE[PL CONNECTOR IAW B737-800 SWPM 2
- [SDR CALA2024121703099](https://openairdocs.org/sdr/CALA2024121703099.md): Angle · cracked · Dec 5, 2024 · N73259 · Boeing 737824 · Fuselage Miscellaneous Structure
  > STA 663 LEFT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER ANGLE IS CRACKED.
- [SDR CALA2024121603075](https://openairdocs.org/sdr/CALA2024121603075.md): Fitting · cracked · Dec 3, 2024 · N73259 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 IAW B737-800 SRM 51-40-02-0G AND BAC DWG 111A2000 REV ORIGINAL F 7.
- [SDR CALA2024121603074](https://openairdocs.org/sdr/CALA2024121603074.md): Fitting · cracked · Dec 3, 2024 · N73259 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 I IAW SRM 51-40-02-0G AND BAC DWG 111A2000 REV ORIGINAL FO 06.
- [SDR CALA2024121603073](https://openairdocs.org/sdr/CALA2024121603073.md): Fitting · cracked · Dec 3, 2024 · N73259 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 I AW B737-800 SRM 51-40-02-OG AND BAC DWG 111A2000 REV ORIGINAL FO 05.
- [SDR CALA2024121603072](https://openairdocs.org/sdr/CALA2024121603072.md): Fitting · cracked · Dec 3, 2024 · N73259 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00075. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW B737-800 SRM 51-40-02-0G AND BAC DWG 111A2000 REV ORIGINAL F 04.
- [SDR CALA2024071800246](https://openairdocs.org/sdr/CALA2024071800246.md): A/C Pack · none · Jul 14, 2024 · N73259 · Boeing 737824 · Standard Practices/Structures
  > PREVIOUS UPDATES SUGGESTED THIS ITEM CAN BE CLEARED. CONFIRMED THE RH PACK IS OPERATIONAL AND THE MEL CAN BE CLEARED RAN AND OPS CHECKED REF AMM 21-51-00-730-802. RH PACK HAS BEEN RE-ACTIVATED AND OK FOR SERVICE. THIS ITEM WAS FLAGGED BY TECH FLAGGED MAJOR REP
- [SDR CALA2024071602048](https://openairdocs.org/sdr/CALA2024071602048.md): Hose · leaking · Jul 14, 2024 · N73259 · Boeing 737824 · Humidity Control System
  > RIGHT PACK LIGHT ILLUMINATED DDP COMPLIED WITH, DEACTIVATED RT PACK FCV PER MEL 2101B DDP COMPLIED WITH. PLACARDED RT PACK SWITCH INOP. OK TO PLACARDED FLT DECK RT PACK SWITCH. OK TO CONTINUE. CONTINUE. APPROVED CONTROLLERS IN REF WITH AMM-21-62 TASK 801. NO F
- [SDR CALA2024061700011](https://openairdocs.org/sdr/CALA2024061700011.md): Arm · loose · Jun 17, 2024 · N73259 · Boeing 737824 · Autopilot System
  > A SYSTEM AUTO PILOT ARM IS LOOSE. SECURED A SYSTEM AUTO PILOT ARM REF AMM 22-11-25-400-801 CYCLED MANY TIMES AND FOUND BINDING.
- [SDR CALA2024061701823](https://openairdocs.org/sdr/CALA2024061701823.md): Pitot Tube · loose · Jun 13, 2024 · N73259 · Boeing 737824 · Pitot/Static System
  > A SYSTEM AUTO PILOT ARM IS LOOSE. SECURED A SYSTEM AUTO PILOT ARM REF AMM 22-11-25-400-801 CYCLED MANY TIMES AND FOUND BINDING.
- [SDR CALA2024052001530](https://openairdocs.org/sdr/CALA2024052001530.md): Skin · damaged · May 13, 2024 · N73259 · Boeing 737824 · Cargo/Baggage Doors
  > PER S.R, RE-SKIN AFT CARGO DOOR (REF: AAR NR 100008122) REPLAVED AFT CARGO DOOR SKIN IAW B737 800 AMM 51-21-99,51-31-00, 51-21-72,51-21-41, SRM 52-30-01-2R-3, 51-40-08-0G-0,51-40-05-0G- 0,51-40-02-0G-0 AND BOEING DWG:146A6110 REV.C.
- [SDR CALA2024051701497](https://openairdocs.org/sdr/CALA2024051701497.md): Forging · cracked · May 13, 2024 · N73259 · Boeing 737824 · Fuselage Main, Structure
  > AFTER NDT INSPECTION PER EA5310-04554 REV C, OP-003, AT LH #1 WINDOW FRAME FOUND TO BE CRACKED. REMOVED DAMAGE (CRACK) ON #1 LH WINDOW FRAME IAW EA 5310-04554 OP 003, REV C, CONFIG B.
- [SDR CALA2024042501239](https://openairdocs.org/sdr/CALA2024042501239.md): Warning Light · illuminated · Apr 23, 2024 · N73259 · Boeing 737824 · Cabin Pressure Control System
  > AUTO FAIL LIGHT LIGHT ON, ALTN LIGHT NOT ON ALTN LIGHT CAME ON INITIALLY BUT WENT OUT AFTER A FEW SECONDS C URRENTLY ALT IS CONTROL CPC BITE SHOWS OFV LRU FAIL MESSAGE. REF FIM 21-31 801 AND 802 ACCOMPLISHED SUCCESSFUL SYSTEM TESTS OF CPC 1&2. NO FAULTS SHOWN
- [SDR CALA2024041501077](https://openairdocs.org/sdr/CALA2024041501077.md): Skin · delaminated · Apr 12, 2024 · N73259 · Boeing 737824 · Spoilers
  > PDA 1 REF L/P 7625580 #8 SPOILER FOUND DELAMINATED BY PASSENGER DURING FINAL APPROACH. PASSENGER HAD PICTURES PRIOR TO PANEL DELAMINATING. TOP SECTION OF PANEL DELAMINATED AS WELL AS LESS THAN 25% OF THE HONEYCOMB.DELAMINATED PANEL ON RIGHT WING INBOARD SPOILE
- [SDR CALA2024010200002](https://openairdocs.org/sdr/CALA2024010200002.md): Stringer · corroded · Dec 13, 2023 · N73259 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > EVIDENCE OF CORRISION ON STRINGER 25L AT STA 847 IMAGES AT STA 847 ON S-25L REMOVED RIVETS FROM STA 847 TO STA 827 COMMON TO S-25L REF SRM REMOVED HI-LOCKS ON S-25L FROM STATION 847 TO STAION 867 REF. 51-40-02. SRM. 51-40-02 CUT DAMAGED STRINGER MINIMUM AMOUNT
- [SDR CALA2023120603568](https://openairdocs.org/sdr/CALA2023120603568.md): Anti-Ice Valve · faulty · Dec 2, 2023 · N73259 · Boeing 737824 · Ice/Rain Protection System
  > COWL VALVE OPEN LIGHT STAYS ON BRIGHT WHEN THE ENG ANTI-ICE SWIT CH IS MOVED TO ON ENG-2 VALVE, ANTI-ICE OFF 29-3021-9-0002 8336 ON 0000 VALVE, ANTI-ICE OFF 29-3021-9-0002 8336 ON 29-3021-9-0002 0750 REMOVED AND REPLACED #2 ENG ANTI ICE VALVE REF FIM /FAULT IS
- [SDR CALA2023112003425](https://openairdocs.org/sdr/CALA2023112003425.md): Line · leaking · Nov 13, 2023 · N73259 · Boeing 737824 · Hydraulic System, Main
  > AIRCRAFT LANDING BEHIND US NOTICED MORE THAN NORMAL SMOKE FROM L EFT MAIN ON LANDING INBD HYDRAULIC BRAKE DISCONNECT LINE ON #2 BRAKE WAS REPLACED REMOVED AND REPLACED BRAKE DISCONNECT LINE PER AMM 32-41-00. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME. A/C BIS.
- [SDR CALA2022032300757](https://openairdocs.org/sdr/CALA2022032300757.md): Rib · cracked · Mar 22, 2022 · N73259 · Boeing 737800* · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER STA.101.90 RIB HAS 3/4" CRACK ON LOWER HORIZONTAL FLANGE AT VERTICAL STIFFENER # 2. (REF AAR NR 9641753) TO T7075 T6.063", REF BHC 5602 AND OP 84, REINSTALLED REPAIR AT STA 101.90, VERTICAL STIFFNER IN REF B737-800 SRM 55-10-09-2R-5
- [SDR CALA2022032300744](https://openairdocs.org/sdr/CALA2022032300744.md): Rib · cracked · Mar 21, 2022 · N73259 · Boeing 737800* · Empennage Structure
  > L/H HORIZONTAL STAB STA 101.90 RIB CRACKED AT LOWER FWD FLANGE REF AAR N/R 9642208 INSTALLED REPAIR ANGLE AT LT HORIZONTAL STAB STA 101.90 AT LOWER FWD FLANGE OF RIB REF B737 SRM 55-10-09-2R-5 FIG 205 WORK ACCOMPLISHED BY V920314
- [SDR CALA2022032100721](https://openairdocs.org/sdr/CALA2022032100721.md): Rib · cracked · Mar 20, 2022 · N73259 · Boeing 737800* · Empennage Structure
  > R/H HORIZONTAL STAB RIB NO.1 AT STA 82.70 CRACKED AT NO.3 VERTICAL STIFFNER LOWER AREA REF AAR N/R 9642159 REMOVED NO.1 RIB AT STA 92.70 REMOVED T-SCETIOC REPAIR EXTRUSION REPAIR AT RIB NO.1 AND REINSTALLED RIB AT FR STA 92.70 REF B737 FOR HEAT TREAT AND REMOV
- [SDR CALA2022032100720](https://openairdocs.org/sdr/CALA2022032100720.md): Skin · dented · Mar 20, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > REFERENCE LOG PAGE 5529746 (CLOSED).FWD CARGO DOOR CUTOUT TOP R/H AREA HAS DENT REWORKED DAMAGE IAW B SRM 53-00-01-2R-21. INSPECTION THRESHOLD OF 50000 FLIGHT CYCLES. EXTERNAL LFEC AT 3500 FLIGHT CYCLES, INTERNAL HFEC AT 3500 FLIGHT CYCLES AND EXTERNAL DV AT 3
- [SDR CALA2022032100719](https://openairdocs.org/sdr/CALA2022032100719.md): Skin · dented · Mar 20, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > REF ELB LP 8128621 ITEM REPETITIVE INSP PER AMM FOUND BIRD STRIKE DENT ON LT SIDE OF FUSLAGE STA 190 WL 184 3.75IN DIA AND.160 DEEP REF AAR N/R 9641251 CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02855 RE
- [SDR CALA2022032100718](https://openairdocs.org/sdr/CALA2022032100718.md): None · corroded · Mar 20, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM L/H JUST I/B OF L2 CREASE BEAM UPPER SURFACE CORROSION. (REF AAR NR 9641534) CABIN AFT WET AREA STA 986.5 AS PER B737-800 SRM 53-70-51-2R-4 AND EC/RA 5320-02466. REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA ST
- [SDR CALA2022030900611](https://openairdocs.org/sdr/CALA2022030900611.md): Beam · corroded · Mar 8, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > MAIN CABIN AFT WET AREA STA 986.5 RBL 4" FLOOR BEAM UPPER SURFACE CORROSION (REF AAR NR 9641538) REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND EC/RA #5320-02466. INSTALLED NEW T-CHORD AT MAIN CABIN AF
- [SDR CALA2022030700604](https://openairdocs.org/sdr/CALA2022030700604.md): Beam · corroded · Mar 7, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > MAIN CABIN AFT WET AREA STA 986.5 RBL 4" FLOOR BEAM UPPER SURFACE CORROSION (REF AAR NR 9641538) REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND EC/RA #5320-02466. INSTALLED NEW T-CHORD AT MAIN CABIN AF
- [SDR CALA2022030300558](https://openairdocs.org/sdr/CALA2022030300558.md): Skin · none · Mar 3, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > AS PER ECRA 5331-02856 STEP 20 INITIATE A 2ND DIP LOGPAGE WHICH REFERENCES DIP LOGPAGE 9732475 REF AAR N/R 9641301 ENGINEERING FOR THE INPSECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02856. REFERENCE LP 9732475, PER ECRA 5331-02856 UPON
- [SDR CALA2022030300557](https://openairdocs.org/sdr/CALA2022030300557.md): Skin · dented · Mar 3, 2022 · N73259 · Boeing 737800* · Fuselage Structure (General)
  > REF ELB LP 8128621 ITEM REPETITIVE INSP PER AMM FOUND BIRD STRIKE DENT ON LT SIDE OF FUSLAGE STA 190 WL 184 3.75IN DIA AND.160 DEEP REF AAR N/R 9641251 CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02855 RE
- [SDR CALA2022030300556](https://openairdocs.org/sdr/CALA2022030300556.md): Skin · dented · Mar 3, 2022 · N73259 · Boeing 7378 · Fuselage Structure (General)
  > AS PER ECRA 5331-02856 STEP 20 INITIATE A 2ND DIP LOGPAGE WHICH REFERENCES DIP LOGPAGE 9732475 REF AAR N/R 9641301 ENGINEERING FOR THE INPSECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02856. REFERENCE LP 9732475, PER ECRA 5331-02856 UPON
- [SDR CALA2018011200161](https://openairdocs.org/sdr/CALA2018011200161.md): Battery Pack · failed · Jan 12, 2018 · N73259 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEAT ROWS 22 - 37 AND AT THE R2 DOOR INOPERATIVE. FOUND THE BATTERY PACK AND CHARGER BAD. REPLACED BOTH. OPS CHECKED OK.
- [SDR CALA2017090803088](https://openairdocs.org/sdr/CALA2017090803088.md): Power Supply · faulted · Sep 8, 2017 · N73259 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEAT 7ABC TO 14ABC DO NOT ILLUMINATE WHEN TESTED. FOUND THE M1676 POWER SUPPLY AT FAULT. REMOVED AND REPLACED THE POWER SUPPLY IAW MM 33-51-06-960-806, AND THE BATTERY PACK IAW MM 33-51-06-960-805. OPS CHECKED GOOD.
- [SDR CALA2017090203025](https://openairdocs.org/sdr/CALA2017090203025.md): Altimeter · out of tolerance · Sep 2, 2017 · N73259 · Boeing 737824 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER IS 1100 FT LOW AT FL380 AND CATCH T LOW AT FL380 AND HANGS UP. REPLACED STANDBY ALTIMETER & AIRSPEED INDICATOR IAW MM 34-13-01, OPS CHECKED GOOD.
- [SDR CALA2017082502870](https://openairdocs.org/sdr/CALA2017082502870.md): Oven · smoke · Aug 25, 2017 · N73259 · Boeing 737824 · Buffet/Galleys
  > SMOKEY ODOR REPORTED NEAR THE AFT LAVATORY, NO SIGN OF SMOKE OR FIRE. REMOVED AND REPLACED THE OVEN. OPS CHECKED NORMAL IAW AMM 25-34-00.
- [SDR CALA2017072402364](https://openairdocs.org/sdr/CALA2017072402364.md): Girt Bar · loose · Jul 24, 2017 · N73259 · Boeing 737824 · Emergency Equipment
  > L1 DOOR SLIDE GIRT BAR BRACKET LOOSE. ADJUSTED THE GIRT BAR HOLDING CLAMPS, OK TO CONTINUE.
- [SDR CALA2017061201812](https://openairdocs.org/sdr/CALA2017061201812.md): Cover · detached · Jun 12, 2017 · N73259 · Boeing 737824 · Emergency Lighting
  > AFT EMERGENCY EXIT COVER FELL OFF. SECURED LIGHT COVER,LIGHT CKD OK
- [SDR CALA2015062900536](https://openairdocs.org/sdr/CALA2015062900536.md): Position Sensor · faulty · Jun 29, 2015 · N73259 · Boeing 737824 · Leading Edge Slat Position Indicating System
  > LE SLAT IN TRANSIT LIGHT UPON REACHING CRUISE ALTITUDE, DIVERTED. LIGHT SUBSEQUENTLY EXTINGUISHED, LE SLAT NR 7. REPEAT WRITE UP, CHRONIC PROBLEM. REPLACED INBD NR 7 LE SLAT POSITION SENSOR IAW AMM 27-88-11-4 01. FSEU NO FAULTS.
- [SDR CALA2015041600282](https://openairdocs.org/sdr/CALA2015041600282.md): Skin · damaged · Apr 14, 2015 · N73259 · Boeing 737824 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR OUTER SKIN FOUND OUT OF SRM LIMITS, SEE LOG PAGE 973522. R & R FWD CARGO DOOR OUTER SKIN. SEE NR 9735227 FOR FWD DOOR SKIN R & R & SUB STEPS. NR 9 737909 FOR FWD DOOR OUTER SKIN REPAINT & PLACARD MARKINGS & NR 9737158 FOR SUB STEPS WORK
- [SDR CALA2015041600281](https://openairdocs.org/sdr/CALA2015041600281.md): Skin · cracked · Apr 14, 2015 · N73259 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LOWER RT HORIZONTAL STAB SKIN HAS A 1/2" CRACK, LOCATED INBD SIDE OF RIB STATION 147.90 & 24" AFT OF FWD SPAR. CRACK ENDS MARKED IN BLACK MARKER FOUND USING HFEC C-SCAN NTM-UAL PART 6 SECTION 55-10-01. ACCOMPLISHED REPAIR IAW ECRA 5510-02514.
- [SDR CALA2015033000220](https://openairdocs.org/sdr/CALA2015033000220.md): Frame · cracked · Mar 28, 2015 · N73259 · Boeing 737824 · Fuselage Main, Frame
  > CABIN FRAME BRACKET AT STATION 500A RT, BETWEEN STATION 8R & 9R. INSTALLED DOUBLER REPAIR & PRESERVED WITH CORROSION INHIBITING COMPOUND IAW EA 5310-04716 REV I FIG 3 STEPS 8, 9 & 13.
- [SDR CALA2015033000214](https://openairdocs.org/sdr/CALA2015033000214.md): Frame · cracked · Mar 26, 2015 · N73259 · Boeing 737824 · Fuselage Main, Frame
  > FRAME CRACKED AT INBD FASTENER, PSU RAIL STATION 867, BETWEEN STRINGER 8R & 9R. INSTALLED DOUBLER REPAIR, SUPPORT BRACKET & APPLIED CORROSION INHIBITING COMPOUND IAW EA 5310-04716 REV I REPAIR 3 FIG 3, 8, 9, 12 & 13.
- [SDR CALA2015033000210](https://openairdocs.org/sdr/CALA2015033000210.md): Frame · cracked · Mar 26, 2015 · N73259 · Boeing 737824 · Fuselage Main, Frame
  > FRAME CRACKED AT INBD FASTENER PSU RAIL STATION 727B BETWEEN STRINGER 8L & 9L. SEE ALL WIPS PERFORMED BY MECH FOR REPAIRED FRAME IAW 5310-04716 REV I FIGURE 3.
- [SDR CALA2015033000209](https://openairdocs.org/sdr/CALA2015033000209.md): Frame · cracked · Mar 26, 2015 · N73259 · Boeing 737824 · Fuselage Main, Frame
  > FRAME CRACKED AT INBD FASTENER, PSU RAIL STATION 727B, BETWEEN STRINGER 8R & 9R. SEE WIP STEPS FOR WORK PERFORMED. REPAIRED FRAME AT STATION 727B BETWEEN STRINGER 8R - 9R IAW EA 5310-04716 REV I FIGURE 3.

Next page: https://openairdocs.org/aircraft/N73259/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 = 'N73259' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N73259/reports

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