# Service difficulty reports: N71411

A list on [N71411](https://openairdocs.org/aircraft/N71411.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 · 69 reports

- [SDR CALA2026101920461](https://openairdocs.org/sdr/CALA2026101920461.md): Hmu · faulty · Oct 14, 2026 · N71411 · Boeing 737924 · Fuel Controlling System
  > REJECTED TAKEOFF AT APPROX 90 KIAS DUE TO E2 NOT ACHIEVING REQD T/O THRUST. REMOVED HMU, REMOVED FUEL PUMP PACKAGE IAW AMM 73-11-01-000-801-F00. INSTALLED NEW HMU & FUEL PUMP.
- [SDR CALA2026101920450](https://openairdocs.org/sdr/CALA2026101920450.md): Shaft · sheared · Oct 14, 2026 · N71411 · Boeing 737924 · Engine Fuel Pump
  > ENGINE 2 NEVER ACHIEVED REQUIRED T/O THRUST. 90.6 REQUIRED. 90.0 ACHIEVED. FOUND ENG 2 FUEL PUMP DRIVE SHAFT SHEARED. REPLACEMENT OF FUEL PUMP PERFORMED. ENG 2 ACHIEVED 99.9% N1 AFTER PUMP WAS REPLACED. OPS CHECK NORMAL.
- [SDR CALA2026041315318](https://openairdocs.org/sdr/CALA2026041315318.md): Pitot Head · clogged · Apr 12, 2026 · N71411 · Boeing 737924 · Rate of Climb Indicator
  > IAS DISAGREE ON PFD DURING TAKEOFF AROUND 120 KIAS. PROBLEM WAS INTERRMITENT IN FLIGHT. DURING T/S FOUND HEAD OF MUD DAUBER WASP AND REMOVED FROM CAPT'S PITOT PROBE. SEE PIC. BLEW OUT CAPT'S AND F/O'S PITOT LINES FROM ADM'S NO OTHER RESTRICTIONS FOUND. REC
- [SDR CALA2026021813886](https://openairdocs.org/sdr/CALA2026021813886.md): Lens · detached · Jan 19, 2026 · N71411 · Boeing 737924 · Emergency Lighting
  > EMERGENCY LIGHT AT ROW 22DEF HANGS DOWN REQUESTING MEL 3315A. COVER IS SECURED. REPLACED 22DEF AREA EMERGENCY LIGHT LENS IAW AMM 33-51-03. OPS CHECKED NORMAL, PLACARD REMOVED.
- [SDR CALA2025120811875](https://openairdocs.org/sdr/CALA2025120811875.md): Battery Pack · inoperative · Dec 5, 2025 · N71411 · Boeing 737924 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE SEAT ROW 12DEF INOPERATIVE. REMOVED UNSERVICEABLE BATTERY PACK AT BATTERY SUPPLY UNIT M1695 IAW AMM 33-51-06. INSTALLED SERVICEABLE BATTERY PACK IAW AMM 33-51-06. PERFORMED OPS TEST OF NEW SERVICEABLE BATTERY PACK IAW AMM 33-51-06, SU
- [SDR CALA2025120511801](https://openairdocs.org/sdr/CALA2025120511801.md): Battery Pack · inoperative · Dec 4, 2025 · N71411 · Boeing 737924 · Emergency Lighting
  > FIRST CLASS EEPL LIGHTING AND R1 DOOR EMERGENCY LIGHTING INOP. SUPPORT TASK NSA EMX N/R 00159. REMOVED FWD ENTRY PANEL IAW AMM 25-21-71-000-807 SUBTASK 25-21-71-010-010. REMOVED BATTERY PACK AT BATTERY SUPPLY UNIT M1674 IAW AMM 33-51-06. INSTALLED SERVICEABL
- [SDR CALA2025120411765](https://openairdocs.org/sdr/CALA2025120411765.md): Attach Angle · cracked · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Main, Attach Fittings
  > STATION 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROXIMATELY LBL 9.0. REPAIRED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.
- [SDR CALA2025120411756](https://openairdocs.org/sdr/CALA2025120411756.md): Attach Angle · cracked · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROX RBL 9.0. REPAIRED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.
- [SDR CALA2025120411754](https://openairdocs.org/sdr/CALA2025120411754.md): Fitting · cracked · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540, RBL 15.04 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000 REV ORIGINAL.
- [SDR CALA2025120411752](https://openairdocs.org/sdr/CALA2025120411752.md): Fitting · cracked · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540, LBL 15.04 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.
- [SDR CALA2025120411749](https://openairdocs.org/sdr/CALA2025120411749.md): Fitting · cracked · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540, LBL 40.87 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.
- [SDR CALA2025120411747](https://openairdocs.org/sdr/CALA2025120411747.md): Fitting · corroded · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540, LBL 32.40 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.
- [SDR CALA2025120411745](https://openairdocs.org/sdr/CALA2025120411745.md): Fitting · cracked · Dec 2, 2025 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT BS 540, LBL 6.14 CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02, AND DWG 111A2000, REV ORIGINAL
- [SDR CALA2025112711508](https://openairdocs.org/sdr/CALA2025112711508.md): Stringer · cracked · Nov 25, 2025 · N71411 · Boeing 737924 · Wing, Longeron/Stringer
  > INSIDE FUEL PANEL 532RB STRINGER U9 HAS A CRACK IN END OF STRINGER AND APPEARS TO END IN FASTENER HOLE. REPAIRED L/W U9 STRINGER END IAW UAL ECRA 5720-03581 REV ORIGINAL USING FASTENER OPTION C AND UAL AVO INT-11172025-0411-1 WITH NO DEVIATIONS
- [SDR CALA2025100609611](https://openairdocs.org/sdr/CALA2025100609611.md): Bumper · faulted · Oct 3, 2025 · N71411 · Boeing 737924 · Emergency Lighting
  > OVERWING EXIT SEAT ROW 15ABC, RED EMERGENCY ESCAPE LIGHT BROKEN THROUGH AND INSIDE THE BUMPER ASSY. R & R SEAT 15C BUMPER ASSY PER PINNACLE CMM. EMERGENCY LIGHT OPS CHK OK. PARTS USED: 29-2500-3-0199, QTY:1
- [SDR CALA2025093009445](https://openairdocs.org/sdr/CALA2025093009445.md): Anti-Ice Valve · faulted · Sep 27, 2025 · N71411 · Boeing 737924 · Engine Anti-Icing System
  > COWL ANTI-ICE NR 2 ENG ILLUMINATED AT FL390. QRH FOLLOWED. LIGHT STILL ON. ON ARRIVAL OVERHEAD FAULT LIGHT FOR E2 ANTI-ICE VALVE EXTINGUISHED. IAW AMM 30-21-11/401 REPLACED COWL ANTI ICE VALVE AS PRECAUTION. ENGINE IDLE LEAK CHECK GOOD. BONDING TEST GOOD AT
- [SDR CALA2025050804562](https://openairdocs.org/sdr/CALA2025050804562.md): Idg · faulted · May 6, 2025 · N71411 · Boeing 737924 · AC Generator-Alternator
  > RT SOURCE OFF LIGHT AND DRIVE LIGHT ILLUMINATED ON GEN2 DRIVE DISCONNECT GEN2 HAD ZERO VOLTS PART VERIFICATION FOR GENERATOR ASSY- INTEGRATED DRIVE PART # 761574B M&E 29-2411-9-0001 S/N AAAH010035 REF AIPC 24-11-11-01A FIG ITEM 5. REMOVED AND REPLACED NUMBER
- [SDR CALA2025042904304](https://openairdocs.org/sdr/CALA2025042904304.md): Slide · not reported · Apr 29, 2025 · N71411 · Boeing 737924 · Escape Slide
  > R2 DOOR SLIDE REQUIRES REPLACEMENT. REMOVED AND REPLACED R2 DOOR MOUNTED SLIDE REF AMM 25-66-01-400-801. (LOG PAGE FOR PARTS TRACKING ONLY). ROTABLE PARTS CHG:TT # 1450279 SN OFF 0469 PN OFF 29-2566-9-0007.SLIDE, FWD/AFT OFF 29-2566-9-0007 0469 ON 29-2566-9-
- [SDR CALA2024122601658](https://openairdocs.org/sdr/CALA2024122601658.md): Target · faulty · Dec 23, 2024 · N71411 · Boeing 737924 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 1 LOCKED BY TOMC DURING VISUAL INSPECTION FOUND SL1 OUTBD PROX SENSOR TARGET BROKEN. REMOVED AND REPLACED SL1 OUTBD PROX SENSOR TARGET BRACKET REF SRM 51-40-02 ADJUSTED SLAT 1 PROX SENSOR S994 PER AMM TASK 27-88-11-40
- [SDR CALA2024090600581](https://openairdocs.org/sdr/CALA2024090600581.md): Transmitter · faulty · Sep 3, 2024 · N71411 · Boeing 737924 · Trailing Flap Position Indicating System
  > FLAPS- TRAILING EDGE FLAPS ASYMMETRY ON LANDING SEE ATTACHED PHOTO ADDING PICTURE OF DFD REPORT. DFD SHOWING LEFT T/E FLAP POSITION XMITTER LAGGING. REMOVED AND REPLACED LH FLAP POSITION TRANSMITTER PER AMM FLAP POSITION TRANSMITTER - REMOVAL/INSTALLATION REFE
- [SDR CALA2024050801409](https://openairdocs.org/sdr/CALA2024050801409.md): None · none · Apr 29, 2024 · N71411 · Boeing 737924 · Standard Practices/Structures
  > BIRDSTRIKE NOSE AREA, CLEANED UP BIRD STRIKE AREA AND PERFORMED INSPECTION PER AMM 05-51-18-210-802-C1 AND 05-51-18-210-801. NO DAMAGE FOUND. NO FURTHER DEFECTS NOTED. AC OKAY FOR SERVICE. INSPECTED F/O WINDSHIELD WIPER FOR DAMAGE REF AMM TASK 30-42-31-820-801
- [SDR CALA2023062802045](https://openairdocs.org/sdr/CALA2023062802045.md): Fastener · missing · Jun 27, 2023 · N71411 · Boeing 7379 · Wing Structure
  > PDA 1 PASSENGER REPORTS MISSING FASTENERS RIGHT WING LEADING EDGE INBOARD OF THE NO.2 ENGINE. INSPECTED RIGHT WING INBOARD FIXED LEADING EDGE UPPER SKIN. FOUND LOOSE AND DAMAGED FASTENERS AND NO MISSING FASTENERS. REMOVED AND REPLACED LOOSE AND DAMAGED FASTENE
- [SDR CALA2023040601053](https://openairdocs.org/sdr/CALA2023040601053.md): Fuse · faulty · Apr 6, 2023 · N71411 · Boeing 737900 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - RED EMERGENCY LIGHTS INOP AT SEAT ROWS 15ABC, 20ABC, & 21ABC. R & R FAULTY FUSE AT POWER SUPPLY M1694 JUST FWD OF LH FWD OVERWING EMERGENCY DOOR. ALL EMERGENCY LIGHTS OPS CHK OK. PARTS USED: 00-0
- [SDR CALA2022121903421](https://openairdocs.org/sdr/CALA2022121903421.md): Stop Fitting · damaged · Dec 17, 2022 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > PDA 3 LEFT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED & MISSING A SECTION ENTIRE LENGTH -- SEE PHOTO PHOTO ADDED PARTS ADDED REF IPC 21-51-03-06A AND IPC 21-51-03-05A
- [SDR CALA2022102402939](https://openairdocs.org/sdr/CALA2022102402939.md): None · none · Oct 24, 2022 · N71411 · Boeing 737 · Flight Control System
  > LE FLAP TRANSIT LT ON REPLACED #1SLAT INBOARD SENSOR. OPS CHECK GOOD.
- [SDR CALA2022090702290](https://openairdocs.org/sdr/CALA2022090702290.md): None · cracked · Sep 7, 2022 · N71411 · Boeing 737 · Horizontal Stabilizer Structure
  > LH HORZ STAB STA 92.70 VERTICAL RIB STIFFENER #3 CRACKED. LH HOR Z STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STI FFENER #3 CRACK REPAIR.CUTOUT SKIN STA 92.70 AT VERTICAL STIFFEN ER #3 IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11 STEP 4.(2). VERI
- [SDR CALA2022090702289](https://openairdocs.org/sdr/CALA2022090702289.md): None · none · Sep 7, 2022 · N71411 · Boeing 737 · Horizontal Stabilizer Structure
  > L/H HORIZONTAL STAB LOWER SKIN AT STA 92.70 REQUIRES LOWER SKIN CUTOUT FOR ACCESS TO REPAIR THE #3 RIB STIFFENER. ER. REPEATINSPECTIONS EVERY 9,000 FLIGHT CYCLES THERE AFTER SEE PLISHED ON MAIN TASK (REFERENCE SUB TASK ST-001: PERFORMED 737 N 1-2R.REFERENCE
- [SDR CALA2022090702288](https://openairdocs.org/sdr/CALA2022090702288.md): None · none · Sep 7, 2022 · N71411 · Boeing 737 · Empennage Structure
  > L/H HORIZONTAL STAB LOWER SKIN REQUIRES CUTOUT AT STA. 92.70 #1 VERTICAL RIB STIFFENER REPAIR. 41437 ACCOMPLISHED TASKS AND PARTIAL WORK ACCOMPLISHED (HFEC INS TE JULY 6 2022 06:54. HFEC COMPLETED ON UPDATED ENTRY SUB TASK 0 T-76511 PO: 123199. 2.) 7075 T-62 P
- [SDR CALA2022083102229](https://openairdocs.org/sdr/CALA2022083102229.md): Skin · none · Aug 30, 2022 · N71411 · Boeing 737 · Empennage Structure
  > R/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL L
- [SDR CALA2022082902203](https://openairdocs.org/sdr/CALA2022082902203.md): None · cracked · Aug 28, 2022 · N71411 · Boeing 737 · Empennage Structure
  > RIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0
- [SDR CALA2022082902202](https://openairdocs.org/sdr/CALA2022082902202.md): Web · cracked · Aug 28, 2022 · N71411 · Boeing 737 · Wing Main, Frame Structure
  > CENTER WING BOX REAR SPAR PRESSURE WEB ALONG VERTICAL PRESSURE DECK, AROUND RBL 33.5 APPROXIMANELY, WEB IS CRACKED. 1" CRACK AT RBL 33.5 AND A 1" CRACK AT RBL 40.0 REF. BAM N/R 000852241 AND 000852243. THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION.
- [SDR CALA2022082402151](https://openairdocs.org/sdr/CALA2022082402151.md): Skin · damaged · Aug 24, 2022 · N71411 · Boeing 737924 · Empennage Structure
  > R/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL L
- [SDR CALA2022082402150](https://openairdocs.org/sdr/CALA2022082402150.md): Stabilizer · cracked · Aug 24, 2022 · N71411 · Boeing 737924 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0
- [SDR CALA2022081602096](https://openairdocs.org/sdr/CALA2022081602096.md): Skin · cracked · Aug 13, 2022 · N71411 · Boeing 737900 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB LOWER SKIN - CRACK FOUND (2 IN LENGTH) BE TWEEN STAB STA 120.50 AND 129.50 AND 1 INCH FWD OF THE REAR SPAR. (6 INCHES FROM THE AFT INBOARD CORNER OF THE EXISTING REPAIR). REF NON-ROTUINE 000803467. EXISTING REPAIR DOUBLER AT STAB STA. 129
- [SDR CALA2022081602095](https://openairdocs.org/sdr/CALA2022081602095.md): Skin · interference · Aug 13, 2022 · N71411 · Boeing 737900 · Horizontal Stabilizer, Plate/Skin
  > LH HORZ STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STIFFENER #1 CRACK REPAIR( N/R 000814111)AND N/R 000841437. THRESHOLD 56,000 FLIGHT CYCLES FOR A DETAIL VISUAL INSPECTION AN INSPECTIONS EVERY 9,000 FLIGHT CYCLES THERE AFTER SEE SRM 55-10- REF
- [SDR CALA2022081602094](https://openairdocs.org/sdr/CALA2022081602094.md): Skin · interference · Aug 13, 2022 · N71411 · Boeing 737924 · Horizontal Stabilizer, Plate/Skin
  > LH HORZ STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STIFFENER #3 CRACK REPAIR( N/R 000841433)AND N/R 000841447. REPAIR DOUBLER INSTALLED ISSUED DIP TO READ " INSPECTION THRESS EXTERNAL (LFEC) INSPECTION OF REPAIR DOUBLER. REPEAT INSPECTIONS REPA
- [SDR CALA2019121602218](https://openairdocs.org/sdr/CALA2019121602218.md): Unknown · abnormal · Dec 16, 2019 · N71411 · Boeing 737924 · Cargo Compartments
  > FWD CARGO PIT MAGIC CARPET DISCHARGING STATIC DURING OPERATION ACROSS FWD L/H EXTENSION ARM AND ROLLER GUIDE PANEL. INVESTIGATING AND CLEANED MOUNTING HARDWARE. UNKNOWN REASON FOR STATIC DISCHARGE. CONTACTED TECH SUPPORT. NEED MORE GROUND TIME TO TROUBLESHOO
- [SDR CALA2017090803089](https://openairdocs.org/sdr/CALA2017090803089.md): Sign · loose · Sep 8, 2017 · N71411 · Boeing 737924 · Emergency Lighting
  > EMERGENCY EXIT SIGN OVER THE WINDOW FOUND LOOSE. SECURED THE LIGHT.
- [SDR CALA2017072802382](https://openairdocs.org/sdr/CALA2017072802382.md): Window · failed · Jul 28, 2017 · N71411 · Boeing 737924 · Flight Compartment Windows
  > NO. 2 RIGHT WINDOW SHATTERED. FLAMES OBSERVED OUTSIDE WINDOW FRONT NEAR BOTTOM. POWER OFF EXT FIRE. REMOVED AND REPLACED R2 SLIDING WINDOW ASSY IAW AMM 56-12-11. OPS CHECKED GOOD.
- [SDR CALA2017062301965](https://openairdocs.org/sdr/CALA2017062301965.md): Light · inoperative · Jun 23, 2017 · N71411 · Boeing 737924 · Emergency Lighting
  > EMERGENCY LIGHT OVERHEAD ROW 11ABC INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW MM 33-51-03.
- [SDR CALA2017020600269](https://openairdocs.org/sdr/CALA2017020600269.md): Power Supply · inoperative · Feb 4, 2017 · N71411 · Boeing 737924 · Emergency Lighting
  > EMERGENCY EXIT AREA LIGHT AT SEAT 14ABC AN D 21ABC ARE INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-51-06-960-806. OPS CHECKED GOOD.
- [SDR CALA2017010600011](https://openairdocs.org/sdr/CALA2017010600011.md): Control Panel · faulty · Jan 6, 2017 · N71411 · Boeing 737924 · Fire Detection
  > ENG 1 OVERHEAT LIGHT IS ON ENG1 OVERHEAT ON CLIMB THROTTLE AT IDLE FOR AT LEAST 5 MINS BEFORE LIGHT WENT OUT SMOOTH. EMERGENCY DECLARED. CAPT REPORTED THAT EGT WAS NOT EXCEEDED NOR DID HE GET AN ENGINE FIRE INDICATION. ALL PARAMETERS WERE NORMAL. PERFORMED ENG
- [SDR CALA2015072100591](https://openairdocs.org/sdr/CALA2015072100591.md): Structure · corroded · Jul 21, 2015 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LT CHORD 23L, SEVERAL SPOTS STATION 288 - 351. REPAIR PERFORMED IAW ECRA 5310-06549.
- [SDR CALA2015072100590](https://openairdocs.org/sdr/CALA2015072100590.md): Gusset · corroded · Jul 21, 2015 · N71411 · Boeing 737924 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STRINGER 21 LT, BETWEEN STATION 297 - 308 ON GUSSET. REPAIR PERFORMED IAW ECRA 5310-0659.
- [SDR CALA2015072100589](https://openairdocs.org/sdr/CALA2015072100589.md): Stringer · corroded · Jul 20, 2015 · N71411 · Boeing 737924 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 25L AT STATION 360. REPAIR WORK COMPLETED IAW ECRA 5310-06551.
- [SDR CALA2015071700578](https://openairdocs.org/sdr/CALA2015071700578.md): Frame · cracked · Jul 16, 2015 · N71411 · Boeing 737924 · Fuselage Main, Frame
  > LEFT CABIN FRAME 500J HAS CRACK INDICATION AT INBD RADIUS, NEAR INBD RIVET AT 4 O CLOCK POSITION. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER IAW ECRA 5310-0654 5. DIP INITIATED TO ACCOMPLISH REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL AIRFRAME FL
- [SDR CALA2015071700576](https://openairdocs.org/sdr/CALA2015071700576.md): Frame · cracked · Jul 16, 2015 · N71411 · Boeing 737924 · Fuselage Main, Frame
  > MFEC FRAME STATION 400R BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV I, FOUND CRACK AT INBD FASTENER. PERFORMED INTERIM REPAIR IAW ECRA 5310-06540 PART 1 IAW STEP 16 OF PART 1.
- [SDR CALA2015071700574](https://openairdocs.org/sdr/CALA2015071700574.md): Frame · cracked · Jul 15, 2015 · N71411 · Boeing 737924 · Fuselage Main, Frame
  > MFEC FRAME STATION 727B RT, BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV L, FOUND CRACK AT INBD FASTENER. REPAIRED RT FRAME IAW EA 5310-04716 REV L. SEE ALL WIPS & TASKS FOR WORK PERFORMED.
- [SDR CALA2015071700573](https://openairdocs.org/sdr/CALA2015071700573.md): Frame · cracked · Jul 15, 2015 · N71411 · Boeing 737924 · Fuselage Main, Frame
  > LEFT CABIN FRAME 727B HAS CRACK INDICATION AT INBD RADIUS NEAR INBD RIVET, AT 4 O CLOCK POSITION. REPAIRED LT CABIN FRAME AT STATION 727B BETWEEN STRINGER 8 & 9 IAW EA 5310-04716 REV L. SEE WIPS & TASKS FOR WORK PERFORMED.
- [SDR CALA2015062900533](https://openairdocs.org/sdr/CALA2015062900533.md): Frame · cracked · Jun 27, 2015 · N71411 · Boeing 737924 · Fuselage Main, Frame
  > LEFT CABIN FRAME 500E HAS A CRACK AT INBD RADIUS NEAR INBD RIVET AT 4 O CLOCK POSITION, FRAME 500E BETWEEN STRINGER 8L & 9L. REPAIRED IAW EA 5310-04716 REV L OP 3.

Next page: https://openairdocs.org/aircraft/N71411/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 = 'N71411' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N71411/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.