# Service difficulty reports: N76515

A list on [N76515](https://openairdocs.org/aircraft/N76515.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 · 54 reports

- [SDR CALA2026081218531](https://openairdocs.org/sdr/CALA2026081218531.md): Lanyard · exposed · Aug 11, 2026 · N76515 · Boeing 737824 · Escape Slide
  > SLIDE PACK ON DOOR 1L HAS SOMETHING HANGING OUT, APPEARS TO BE A ZIP TIE ATTACHED TO SOMETHING. REMOVED DOOR 1L SLIDE PACK & REINSTALLED SLIDE PACK SAFETY PINS IAW AMM 25-66-01. ACCOMPLISHED RII INSPECTION OF SLIDE PACK 1L COVER LANDYARDS INSTALLATION AND SL
- [SDR CALA2026060116705](https://openairdocs.org/sdr/CALA2026060116705.md): Battery Pack · inoperative · May 29, 2026 · N76515 · Boeing 737824 · Emergency Lighting
  > IN REF. OF LOG PAGE 8804400 REMOVED CEILING ASSY FWD ENTRY FOR ACCESS TO EMERGENCY BATTERY PACK REF. AMM 33-29-00-09 VERIFIED INSTALLATION OF PASSENGER ENTRY FWD CEILING PANEL REF AMM 25-21-71 OPS CHECK GOOD
- [SDR CALA2026060116704](https://openairdocs.org/sdr/CALA2026060116704.md): Lens · broken · May 29, 2026 · N76515 · Boeing 737824 · Emergency Lighting
  > GLASS BROKEN ON EXT EMERGENCY LIGHTING, AT DOOR 1 LEFT REPLACED LENS ON EXTERIOR EMERGENCY LIGHT. DOOR ONE LEFT SIDE WITH NEW P/N 81004-37801. OPS CHECK GOOD, REF AMM 33-51-04-860
- [SDR CALA2026052816608](https://openairdocs.org/sdr/CALA2026052816608.md): Skin Panel · damaged · May 26, 2026 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > PER ECRA 5310-08915 STA 255 LIGHTNING STRIKE BLEND DAMAGE-INTERIM REPAIR ACCOMPLISH INTIAL SUPPLEMENTAL INSPECTION PER PART 2 OF ECRA 5330-07744 (LATEST REVISION) AT OR PRIOR TO 50,000 TOTAL FL IGHT CYCLES. PER ECRA 5310-08915 STA 255 LIGHTNING STRIKE BLEND DA
- [SDR CALA2026052716558](https://openairdocs.org/sdr/CALA2026052716558.md): Skin · damaged · May 26, 2026 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > DURING PHASE TWO INSPECTION FOUND LIGHTNING STRIKE AT CROWN APPROXIMATELY STATION 350BETWEEN S 2R-3RFOUND TWO(2EACH)LIGHTINGAT STRIKE STA 360 LEFT BELOW FLOORBEAM. FASTENER/DAMAGE REMOVED REF SRM 53-00-01-2R. INSPECTION-REJECT,"PIT" WITHIN COUNTERSINK CLEANE
- [SDR CALA2026052516518](https://openairdocs.org/sdr/CALA2026052516518.md): Skin · damaged · May 24, 2026 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > REF LOG PAGE 8761591 LIGHTNING STRIKE ON CROWN APPROX STA 235 BETWEEN STR 1R AND STR 2R EXCESSIVE MATERIAL WAS REMOVED FROM BLENDING REQUIRES REPAIRLAID OUT GRID LAID OUT GRID ULTRASOUND MEASUREMENTS ACCOMPLISHED UT INSPECTION OF BLENDED AREA AND PROVIDED MESS
- [SDR CALA2026060116668](https://openairdocs.org/sdr/CALA2026060116668.md): Power Supply · faulted · May 7, 2026 · N76515 · Boeing 737824 · Emergency Lighting
  > IDT INSPECTION REQUIRED.REMOVED EMERGENCY LIGHT OVERHEAD INSIDE PASSENGER COMPARTMENT ABOVE ROWS 20-21 FOR SHEETMETAL ACCESS RESEARCHED ASSIGNMENT, EMERGENCY LIGHTS ARE NO LONGER IDT INSPECTION, NEED INSPECTION TO CONCUR AND REMOVE IDT. ITEM IS NOT AN IDT TRA
- [SDR CALA2026012013112](https://openairdocs.org/sdr/CALA2026012013112.md): Indicator · faulted · Jan 18, 2026 · N76515 · Boeing 737824 · Autopilot System
  > ON DEPARTURE SPEED TRIM FAIL LIGHT ILLUMINATED TWO TIMES. COULD NOT ENGAGE A/P CMD A OR B. DEBRIEFED CREW, CREW FOUND THE AUTOPILOT STAB TRIM SWITCH IN THE CUTOFF POSITION. THEY STATED THEY MUST OF MISSED IT ON THEIR PREFLIGHT CHECK. BUT THE SPEED TRIM INOP CA
- [SDR CALA2025112811564](https://openairdocs.org/sdr/CALA2025112811564.md): Sensor · faulty · Nov 24, 2025 · N76515 · Boeing 737824 · Trailing Flap Position Indicating System
  > FLAPS WONT EXTEND TO 1LOCK BY TOMC DEBREIFED CREW. LEADING EDGE SLATS DEPLOYED AND WENT GREEN HOWEVER TRAILING EDGE FLAPS WOULD NOT GO TO FLAPS 1 POSITION. INSPECTED WHEEL WELL FLAP TRANSMISSIONS AND NIETHER IS TRIPPED. INSPECTED AREA IN WHEEL WELL AND FOUND N
- [SDR CALA2025112611493](https://openairdocs.org/sdr/CALA2025112611493.md): Transmitter · faulted · Nov 23, 2025 · N76515 · Boeing 737824 · Trailing Flap Position Indicating System
  > TRAILING EDGE FLAPS DISAGREE. EXTENDED TO FLAPS 1 AND FLAPS STOPPED EXTENDING HALFWAY BETWEEN UP AND FLAPS 1. LE FLAPS TRANSIT LIGHT ILLUMINATED. ALTERNATE FLAPS EXTENSION USED TO EXTEND FLAPS TO 15. AS FLAP INDICATOR MOVED FROM FLAPS 10 TO 15 LE FLAPS EXT GRE
- [SDR CALA2025112011368](https://openairdocs.org/sdr/CALA2025112011368.md): Slide · unpacked · Nov 19, 2025 · N76515 · Boeing 737824 · Escape Slide
  > L1 DOOR EXCESS SLIDE PACK MATERIAL HANGING OUT AFTER ARMING SLIDE SECURED EXCESS SLIDE PACK MATERIAL IAW AMM 25-66-01-200-802. SLIDE PACK OPS NORMALLY. C/W INSPECTION OF FWD L1 DOOR SLIDE PACK. REF GMM09-25-05. OK TO CONTINUE. ADDED SDR INSPECTION
- [SDR CALA2025101410044](https://openairdocs.org/sdr/CALA2025101410044.md): Slide · unpacked · Oct 11, 2025 · N76515 · Boeing 737824 · Escape Slide
  > MAIN CABIN DOOR EMERG. SLIDE HAS MORE MATERIAL EXPOSED THAN USU AL. RESECURED MATERIAL ON MAIN CABIN DOOR SLIDE AS REQUIRED. ADD EMP: U422054
- [SDR CALA2025092409220](https://openairdocs.org/sdr/CALA2025092409220.md): Computer · faulty · Sep 23, 2025 · N76515 · Boeing 737824 · Autopilot System
  > NEITHER AUTOPILOT WOULD ENGUAGE 15000 FEET DEBRIEFED CREW. PILOT STATED AT 15K FEET NEITHER AUTOPILOT WOULD ENGAGE. AFTER PRESSING RECALL GOT SPEED TRIM LIGHT. RAN DFCS BITE CHECK AND GOT THE FOLLOWING FCC A AND FCC B FLIGHT FAULTS FOR LEG 1. SEE PICS MORE PIC
- [SDR CALA2025090308422](https://openairdocs.org/sdr/CALA2025090308422.md): Warning Light · false activation · Aug 30, 2025 · N76515 · Boeing 737824 · Door Warning System
  > AFT ENTRY DOOR LIGHT ON TAKEOFF LIGHT WENT OUT FEW SECONDS AFTER PRES NORMAL. PERFORMED AMM 52-13-00-860-803, OPERATED AFT ENTRY DOOR, INDICATION AND DOOR OPS CHECKS NORMAL. OK FOR SERVICE.
- [SDR CALA2025081207644](https://openairdocs.org/sdr/CALA2025081207644.md): Windshield · cracked · Aug 9, 2025 · N76515 · Boeing 737824 · Flight Compartment Windows
  > DURING BIRD STRIKE INSPECTION FOUND L1 WINDSHIELD CRACKED. REMOVED AND REPLACED THE L1 WINDSHEILD PER AMM 56-11-11-000-801 AND AMM 56-11-11-400-801. OPS CHECK COMPLETE PER AMM 30-42-31-400-801.
- [SDR CALA2025073107179](https://openairdocs.org/sdr/CALA2025073107179.md): Lamp · no test · Jul 31, 2025 · N76515 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK, LEFT OVERWING EXIT AFT EMERGENCY LIGHT INOP. RELAMPED LEFT OVERWING EXIT AFT EMERGENCY LIGHT IAW AMM 33-51-04-960-801. OPS NORMAL. OK TO CONTINUE.
- [SDR CALA2025042804283](https://openairdocs.org/sdr/CALA2025042804283.md): Sensor · no discrepancy · Apr 22, 2025 · N76515 · Boeing 737824 · Door Warning System
  > DURING T/O ROLL AT ABOUT 60KTS AFT ENTRY LT ILLUM INATED...ABORT ED T/O LT OUT DRNG TAXI BACK VERIFIED AFT ENTRY CLOSED AND LOCKED. PERFORMED AFT ENTRY DOOR INDICATION TEST OF S200 REF AMM TASK 52-71-11-710-801. OPS CHECK GOOD. CHECKED S200 SENSOR STATUS ON
- [SDR CALA2025042104093](https://openairdocs.org/sdr/CALA2025042104093.md): Door · unsecure · Apr 18, 2025 · N76515 · Boeing 737824 · Passenger/Crew Doors
  > RTO 80 KNOTS AFT ENTRY DOOR LIGHT. FA CONFIRMED HANDLE WAS NOT A LL THE WAY DOWN.LIGHT OUT NOW. FLIGHT CREW REPORTED TO TOMC DOOR 2L WAS NOT CLOSED PROPERLY, ONCE DOOR HANDLE WAS CLOSED ALL THE WAY, LIGHT EXTINGUISHED, NO MAINTENANCE REQUIRED. CREW COMPLIED WI
- [SDR CALA2025031902966](https://openairdocs.org/sdr/CALA2025031902966.md): Slide · loose · Mar 16, 2025 · N76515 · Boeing 737824 · Escape Slide
  > 1R DOOR SLIDE HAS SLACK AND IS TOUCHING THE AIRCRAFT FLOOR REMOVED AND REPLACED R 1 DOOR SLUDE REF AMM 26-66-01-400-803 PARTS USED: 29-2566-9-0007, QTY:1 ADD EMP:385164 ROTABLE PARTS CHG:TT # 1425402 SN OFF 5903 PN OFF 29-2566-9-0007.SLIDE, FWD/AFT OFF 29
- [SDR CALA2025012702064](https://openairdocs.org/sdr/CALA2025012702064.md): Lamp · inoperative · Jan 23, 2025 · N76515 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LIGHT NOT ARMED LIGHT INOP RELAMPED NOT ARMED LIGHT.
- [SDR CALA2024102502728](https://openairdocs.org/sdr/CALA2024102502728.md): Skin · damaged · Oct 19, 2024 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > REMOVED DAMAGE SKIN AREA ON AFT CARGO DOOR LOWER FWD CORNER, AND INSTALLED REPAIR STA 796.98-811 REF AAR ESR-WI NO. 2022816- 29-109935 REV IR AND UNITED EC/RA NO. 5231-01158. WORK ACCOMPLISHED BY V894534.REFER LP9607861
- [SDR CALA2024101802675](https://openairdocs.org/sdr/CALA2024101802675.md): Support Bracket · cracked · Oct 16, 2024 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR BILGE SUPPORT CLIP CRACKED AT FASTNER HEAD AT S-26L STA 500I REF AAR N/R 9907424 REMOVED AND REPLACED FWD CARGO STRINGER CLIP AT STA 500I S-26L P ER SRM 51-40-02-0G-0 WORK ACCOMPLISHED BY V947695
- [SDR CALA2024101802674](https://openairdocs.org/sdr/CALA2024101802674.md): Channel · corroded · Oct 16, 2024 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORROSION ON Z CHANEL AFT CARGO L/H FROM STA 727I TO 727D REF AAR N/R 9907021 REMOVED AND REPLACED NEW L/H SIDE Z CHANEL AT AFT CARGO COMP FRO M STA 727J-5 TO 727 PER SRM 51-40-02-0G-0 AND DWG 146A7500 WORK ACCOMPLISHED BY V937871
- [SDR CALA2024101602663](https://openairdocs.org/sdr/CALA2024101602663.md): Support Angle · cracked · Oct 15, 2024 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FLOOR BILGE SUPPORT CLIP CRACKED AT FASTNERS HEAD AT S-26L STA 500G REF AAR N/R 9907422 REMOVED AND REPLACED FWD CARGO SUPPORT CLIP AT S-26L STA 500G PER SRM 51-40-02-0G-0.
- [SDR CALA2024102302709](https://openairdocs.org/sdr/CALA2024102302709.md): Skin · dented · Oct 10, 2024 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > EXISTING DENT AT STA 196.5 FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1. REF AAR N/R 9907416 AS PER ECRA 5331-03130 STEP 3 INITIATE A DIP LP TO READ AS FOLLOWS AFTER THE ACCUMULATION OF 49,000TOTAL F/C BUT BEFORE 50,000 PERFORMED AN INSP OF THE FUSELAGE SKI
- [SDR CALA2024100102534](https://openairdocs.org/sdr/CALA2024100102534.md): Rib · cracked · Sep 29, 2024 · N76515 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > REMOVE AND REPAIR THE RIGHT HORIZONTAL STAB RIB 5 STIFFENER 2 EVIDENCE OF CRACK FOR SCEPTER TRACKING PURPOSE REPAIRED RIGHT HORIZONTAL STAB RIB 5,STIFFENER 2 AS PER SRM 55-10-09-2R-4,REPAIT 4 FIGUER 202
- [SDR CALA2024101702672](https://openairdocs.org/sdr/CALA2024101702672.md): Fitting · corroded · Sep 21, 2024 · N76515 · Boeing 737824 · Vertical Stabilizer Miscellaneous Structure
  > FOUND CORROSION AT VERTICAL STAB.FWD RIGHT BULKHEAD FITTING ON THE AFT SURFACE AS PER SCEPTER TRACKING PURPOSE REPAIRED VERTICAL STAB FRONT SPAR RH FUSELAGE AT TUCH FITTING AT B51016 AS PER REF ESF-W1 2022816-12-10802 REV IR AND EC/RA 5380-01403 AS PER AAR WOR
- [SDR CALA2024092302470](https://openairdocs.org/sdr/CALA2024092302470.md): Skin · cracked · Sep 20, 2024 · N76515 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN STA 157.10.8. 5 FROM FRONT SPAR, I/B LENGTH OF CRACK 0.312 TRIMMED CRACKED AREA AT RT HORIZONTAL STAB LOWER SKIN STA 157.10,8.5 FROM SPAR I/B ROW FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AS PER B737
- [SDR CALA2024092302468](https://openairdocs.org/sdr/CALA2024092302468.md): Floorbeam · corroded · Sep 20, 2024 · N76515 · Boeing 7378 · Fuselage Main, Floor Beam
  > SURFACE CORROSION AT FLOOR BEAM STA947.5 LBL5 CORROSION AT FLOOR BEAM STA 947.5 LB2.5 REPAIRED AS PER REF AAR MIA ESR-W1 2022816-6-10775 REV IR AND EC/RA #5321-02152
- [SDR CALA2024091602432](https://openairdocs.org/sdr/CALA2024091602432.md): Floor Support · corroded · Sep 13, 2024 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORROSION AT CABIN FWD WET AREA FLOOR STRUCTURE STA 294+13 LBL 11 WL 208.1 INTERCOSTAL FASTNER HOLE. REMOVED AND REPLACED THE INTERCOSTAL AT FWD WET AREA STA 294.5 TO STA 312 PER DWG 141A5600 AND SRM 51-40-02-0G-0.
- [SDR CALA2023031300731](https://openairdocs.org/sdr/CALA2023031300731.md): Probe · unknown · Mar 13, 2023 · N76515 · Boeing 7378 · Engine Indicating System
  > ENGINE 1 HIGH EGT NUMEROUS TIMES ERRATIC INDICATIONS EGT SIGNAL OUT OF RANGE. MAYBE REFER TO LOGPAGE 4027334 EGC. REPORT FROM CREW: #1 ENG BACK TO IDLE. NOT SHUT DOWN. HIGHEST UPLOAD PIC OF T49.5 SENSOR READINGS, S4 IS READING DASHES. EGT WAS AROUND 850 AND DR
- [SDR CALA2022101002759](https://openairdocs.org/sdr/CALA2022101002759.md): Actuator · inoperative · Oct 10, 2022 · N76515 · Boeing 737824 · Drag Control Actuator
  > AILERON TRIM AT RIGHT CRUISE ALT AUTOPILOT WOULD NOT ENGAGE ADJUST TO LIMITS. ROTABLE PARTS CHANGE WAS INDICATED. ACCOMP CATIII PER AMM 22-11-00, TEST PASSED. NR 2 SPOILER IS STUCK. REMOVED NR 2 FLT SPOILER ACTUATOR IAW AMM 27-61-51. INSTALLED NR 2 SPOILER
- [SDR CALA2022032300764](https://openairdocs.org/sdr/CALA2022032300764.md): Hmu · failed · Mar 23, 2022 · N76515 · Boeing 737800* · Fuel Control/Turbine Engines
  > NO 1 ENG FAILED AT 340. ATTEMPT RESTART. NOEGT NO RESTART SECTION. REPLACED GASKET REF AMM 73-21-10. RAN ENGINE NO LEAKS NOTED, BUT FUEL WAS SEEPING FROM HMU SIDE CASE COVER. REQUIRES HMU REPLACMENT. ADDED PICTURES. T/S FOUND MSG 73-21551. PERFORMED EEC BITE T
- [SDR CALA2021111002076](https://openairdocs.org/sdr/CALA2021111002076.md): Fastener · missing · Nov 10, 2021 · N76515 · Boeing 737824 · Lighting System
  > PDA 3 FASTNER MISSING LH LANDING LIGHT LENS COVER REF LOG 7382710 DIP MADE, REF GNMM 02-30-95.
- [SDR CALA2020062901026](https://openairdocs.org/sdr/CALA2020062901026.md): Aoa · reads high · Jun 27, 2020 · N76515 · Boeing 737824 · Stall Warning System
  > EEC ALTN MODE ON TAKEOFF... AIRSPEED UNRELIABLE PER FLIGHT CREW VERBAL REPORT, CAPTAINS AIRSPEED INDICATION READS APPROXIMATELY 40KNOTS SPLITS BETWEEN THE STANDBY AND THE FO AIRSPEED INDICATOR. PERFORMED ALPHA VANE RIGGING TEST IAW AMM 22-11-00-820-809, FOUN
- [SDR CALA2019032500469](https://openairdocs.org/sdr/CALA2019032500469.md): Unknown · malfunctioned · Mar 25, 2019 · N76515 · Boeing 737824 · Navigation System
  > CA AIRSPEED INDICATED AN OVERSPEED AT 260 KIAS UPON SELECTION OF ECON CLIMB. FO FLEW RTB. THIS ITEM HAS TOO MUCH HISTORY. LOG PAGE WILL BE UNLOCKED ONCE A DEFINITE FIX IS C/W UNLOCKED REPLACED LT AOA SENSOR T433 REF AMM 34-21-05-400-801. REPLACED NR 1 SMYD COM
- [SDR CALA2018101502124](https://openairdocs.org/sdr/CALA2018101502124.md): Lens · missing · Oct 15, 2018 · N76515 · Boeing 737824 · Emergency Lighting
  > EEL LIGHT LENS MISSING SEAT 38C. REPLACED EEL LIGHT ASSY 38C OPS CHECK OK ACP'D IDT INSPECTION REF GMM 09-10-05.
- [SDR CALA2017072802420](https://openairdocs.org/sdr/CALA2017072802420.md): Slide · partial deploy · Jul 28, 2017 · N76515 · Boeing 737824 · Escape Slide
  > PARTIAL SLIDE DEPLOYMENT AT 1L.. REMOVED AND REPLACED L1 SLIDE ASSY PER AMM 25-66-01-000-801, -4 00-803, 25-66-01-000-802, -400-801. CHECKS GOOD. A/C OK FOR SERVICE
- [SDR CALA2017031000557](https://openairdocs.org/sdr/CALA2017031000557.md): Pump · faulty · Mar 10, 2017 · N76515 · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > LOST HYD B SYSTEM. EMERGENCY DECLARED. SERVICED B SYSTEM HYDRAULICS TO FULL 7 GALLONS. WITH ENGINE NR 2 RUNNING FOR 30 MIN AND THEN WITH B SYSTEM ELECTRIC PUMP NO EXTERNAL HYDRAULIC LEAKS FOUND. B SYSTEM FLUID STARTED AT 105% BEFORE ENGINE RUN AND DROPPED TO
- [SDR CALA2016080400498](https://openairdocs.org/sdr/CALA2016080400498.md): Fuse · inoperative · Aug 4, 2016 · N76515 · Boeing 737824 · Emergency Lighting
  > RT EXTERIOR EMERGENCY LIGHT JUST AFT OF FLAP FOUND INOPERATIVE. REPLACED THE FUSES IN THE POWER SUPPLY M1671. CHECKED GOOD.
- [SDR CALA2016041800230](https://openairdocs.org/sdr/CALA2016041800230.md): Skin · cracked · Apr 17, 2016 · N76515 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN AT STATION 157.10 AT APPROX 9.5 INCHES FROM REAR SPAR. REMOVED DAMAGE & INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2016041800229](https://openairdocs.org/sdr/CALA2016041800229.md): Skin · cracked · Apr 17, 2016 · N76515 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION ON RT HORIZONTAL STABILIZER LOWER SKIN, AT STATION 101.90, AT APPROX 11.5 INCHES FROM REAR SPAR. REMOVED DAMAGE & INSTALLED EXTERNAL REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT REPAIR AT INITIAL THRESHOLD OF 56,000 TO
- [SDR CALA2016033100203](https://openairdocs.org/sdr/CALA2016033100203.md): Skin · not reported · Mar 30, 2016 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > INSTALL DOUBLER REPAIR IAW STEPS 14 - 15. INSTALLED DOUBLER IAW AVO4991 STEPS 14 PARA 15.
- [SDR CALA2015112300950](https://openairdocs.org/sdr/CALA2015112300950.md): Structure · cracked · Nov 23, 2015 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > IN COMPLIANCE WITH AD2013-23-04 1 CRACK WAS NOTED AT LBL 24.75 OTBD FLANGE AT STATION 727B. REAMED DAMAGE HOLES, TRIMMED AREAS, FABRICATED REPAIR SPLICES & FILLERS. INSTALLED IAW ECRA 5320-02635 & RES 2009774-2.
- [SDR CALA2015112300949](https://openairdocs.org/sdr/CALA2015112300949.md): Structure · cracked · Nov 23, 2015 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > IN COMPLIANCE WITH AD 2013-23-04, THREE EACH CRACKS NOTED AT STATION 727B, RBL 24.75 ONE EACH INBD FLANGE, OTBD FLANGE. REAMED DAMAGE HOLES, TRIMMED AREAS, FABRICATED REPAIR SPLICES, FILLERS, TREATED, PRIMED & INSTALLED IAW ECRA 5320-02635 & RES 2009474-3.
- [SDR CALA2015112300948](https://openairdocs.org/sdr/CALA2015112300948.md): Structure · cracked · Nov 23, 2015 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > IN COMPLIANCE WITH AD 2013-23-04, TWO EACH CRACKS NOTED AT STATION 727B, RBL 45.50, ONE EACH INBD FLANGE, ONE EACH OTBD FLANGE. REAMED DAMAGE HOLES, TRIMMED AREAS, FABRICATED REPAIR SPLICES, FILLERS, TREATED, PRIMED & INSTALLED IAW ECRA 5320-02635 & RES 20094
- [SDR CALA2015112300947](https://openairdocs.org/sdr/CALA2015112300947.md): Structure · cracked · Nov 23, 2015 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > IN COMPLIANCE WITH AD 2013-23-04, FOUR EACH CRACKS FOUND AT STATION 727B, LBL 45.5 AT BOTH OTBD & INBD FLANGES. REAMED DAMAGE HOLES. TRIMMED AREAS, FABRICATED REPAIR SPLICES, FILLERS, TREATED, PRIMED & INSTALLED IAW ECRA 5320-02635 & RES 2009474-1 AT STATION
- [SDR CALA2013091800687](https://openairdocs.org/sdr/CALA2013091800687.md): Eec · malfunctioned · Sep 18, 2013 · N76515 · Boeing 737824 · Fuel Control/Turbine Engines
  > NR 2 ENGINE OVERHEAT ON CLIMB OUT, TEMP 768. OAT 10^, ALTITUDE 10000. NO ALARMS, NO ENGINE OVERHEAT LIGHT ON CENTER PANEL, NO ENGINE SURGE SOUNDS. TROUBLE SHOT TO NR 2 ENGINE EEC, REPLACED EEC IAW AMM 73-21-60. ACCOMPLISHED POWER ASSURANCE RUN IAW AMM 71-00
- [SDR CALA2013081400562](https://openairdocs.org/sdr/CALA2013081400562.md): Skin · damaged · Aug 13, 2013 · N76515 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FWD RT CLEVIS HAS A FASTENER STUCK IN OTBD HOLE AND THE FASTENER IS MISDRILLED, REPLACES ALL MISDRILLED PARTS AND INSTALLED FREEZE PLUG REPAIR IN SKIN REF ECRA 5330-04690
- [SDR CALA2013080500535](https://openairdocs.org/sdr/CALA2013080500535.md): Floor Support · cracked · Aug 3, 2013 · N76515 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT FASTNER HOLE STA 312 TO STA 328 APPROX LBL 45. INSTALLED NEW FLOOR SUPPORT, REF-SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N76515/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 = 'N76515' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N76515/reports

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