# Service difficulty reports: N29129

A list on [N29129](https://openairdocs.org/aircraft/N29129.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 · 78 reports

- [SDR CALA2026010812806](https://openairdocs.org/sdr/CALA2026010812806.md): Wire · damaged · Jan 7, 2026 · N29129 · Boeing 757224 · Fuel System Wiring
  > RIGHT WING, DURING REMOVAL OF W150 0-0095-20 DAMAGE ON CONNECTOR D6878. REMOVED AND REPLACED L MAIN TANK INDICATOR WIRE W1500-0096029 AT CONNECTOR 06878 WITH NEW WIRE IAW SWPM 20-10-11 AND SW PM 20-61-00, WDM 28-41-11 AND FUEL QTY IND SYST OPERATIONAL TEST W
- [SDR CALA2026010812799](https://openairdocs.org/sdr/CALA2026010812799.md): Web · gouged · Jan 4, 2026 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > EA 5311-01827 REV G, DURING PERFORM EA STEP 2.B FOUND GOUGE IN EXISTING REPAIR AT BS 1640, S14R TO S15R, REMOVED DAMAGED WEB AND REPLACED BY NEW IAW SRM 51-40-02-0G, AND DWG:1 46N8713, REV, P SH 1. REF NRC 139492.
- [SDR CALA2026010812798](https://openairdocs.org/sdr/CALA2026010812798.md): Bracket · gouged · Jan 3, 2026 · N29129 · Boeing 757224 · Fluid Service Doors
  > POTABLE WATER SERVICE PANEL, HAS 2EA LATCH BRACKETS WITH GOUGES. REPAIRED POTABLE WATER SERVICE PANEL LATCH BRACKETS PER EC/RA# 5 360-02082. REF NRC 139021. INSPECTION APPROVED
- [SDR CALA2026010712740](https://openairdocs.org/sdr/CALA2026010712740.md): Skin · dented · Dec 30, 2025 · N29129 · Boeing 757224 · Leading Edge Devices
  > LEFT WING, NR 4 SLAT LEADING EDGE HAS 2 DENTS. REPAIRED THE LT WING NR 4 SLAT LEADING EDGE IAW SRM 51-70-10-2R-2.
- [SDR CALA2026010612696](https://openairdocs.org/sdr/CALA2026010612696.md): Control Panel · corroded · Dec 26, 2025 · N29129 · Boeing 757224 · Wing Main, Frame Structure
  > RIGHT WING FUELING STATION, THE CON TROL PANEL HAS CORRODED. REMOVED AND REPLACED FUELING CONTROL PANEL (P28) IAW AM M 28-21-08-004-001 AND AMM 28-21-08-404-031 TEST PASS AND SEVERA L SWITCHES WERE REPLACED IAW SWPM 20-83-11 AND SWPM 20- 84-20.
- [SDR CALA2025122412413](https://openairdocs.org/sdr/CALA2025122412413.md): Intercostal · cracked · Dec 22, 2025 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > E & E BAY, ADJACENT TO CUTOUT DOOR 119BL, RT SIDE, SHIELD PANEL HAS GOUGE. FABRICATED PART IAW PL284N1038. REMOVED, FABRICATED, AND INSTALLED THE TWO PARTS INTERCOSTAL & STIFFNER LOCATED & DRILLED IAW SRM 51-40-05, TREATED, PRIMED IAW SRM 51-20-01 AND INSTAL
- [SDR CALA2026010612695](https://openairdocs.org/sdr/CALA2026010612695.md): Intercostal · corroded · Dec 21, 2025 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FR 860 AND FR 900 R/H SIDE OF CENTER HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED INTERCOSTAL BETWEEN FR860 AND FR900 RH SIDE IAW SRM 51-40-02-OG-0.
- [SDR CALA2025122412401](https://openairdocs.org/sdr/CALA2025122412401.md): Intercostal · corroded · Dec 21, 2025 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN BS 860 - 900 LT SIDE OF CENTER HAD EVIDENCE OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL BETWEEN BS 860 - 900 IAW SRM 51-40-02-0G-0.
- [SDR CALA2025122412399](https://openairdocs.org/sdr/CALA2025122412399.md): Angle · corroded · Dec 21, 2025 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY, BS 1420 - 1440, RBL 7, ANGLES SUPPORT, TWO EACH ON WEB CORRODED. REMOVED THE TWO STIFFENERS IAW SRM 51-40-02, FABRICATED THE STIFFENERS IAW DWG 146N5378, PL 146N5448 -33 AND BAC 1490-2743. RESTORED PROTECTIVE SURFACE AND INSTALLED THE STIFFE
- [SDR CALA2025122312365](https://openairdocs.org/sdr/CALA2025122312365.md): Skin · gouged · Dec 20, 2025 · N29129 · Boeing 757224 · Leading Edge Devices
  > LEFT WING NR 3 SLAT INNER INBD EDGE HAS A GOUGE. PERFORMED A REPAIR ON THE LT WING NR 3 SLAT INNER INBD EDGE IAW SRM 57-43-02-2R-1, AND SRM 51-70-10, REPAIR 04.
- [SDR CALA2025122312357](https://openairdocs.org/sdr/CALA2025122312357.md): Floor Support · cracked · Dec 20, 2025 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE BS 1320-1340, BL 0 WEB HAS ONE CRACK. FABRICATED IAW DWG 146N5180. REMOVED WEB, LOCATED & DRILLED WEB IAW SRM 51-40-05-OG-0, TREATED, PRIMED, TOP COAT AT WEB IAW SRM 51-20-01-OG-0, AMM 51-21-14-270- 801, AND AMM 51-21-15-370-80
- [SDR CALA2025122312356](https://openairdocs.org/sdr/CALA2025122312356.md): Support Bracket · cracked · Dec 20, 2025 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > MAIN MID CABIN FLOOR UNDER FLOOR PANEL 241 GF BETWEEN BS 1160 & 1180, BL 0, SUPPORT BRACKET HAS 2 CRACKS. FABRICATED IAW DRAWING. REMOVED REPLACED IAW SRM 51-70-11-OG-0, AND REINSTALLED MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR CALA2025122212296](https://openairdocs.org/sdr/CALA2025122212296.md): Frame · corroded · Dec 18, 2025 · N29129 · Boeing 757224 · Fuselage Main, Frame
  > FRAME 900 LT SIDE, HAD EVIDENCE OF CORROSION. ACCOMPLISHED FRAME WAS REPAIRED ON BS 900 LT SIDE IAW SRM 51-70-11-OG-0, AND BRACKET GUSSETS AND STOP FITTINGS WERE REMOVED AND IN STALLED IAW SRM 51-90-02-OG-0.
- [SDR CALA2025112711512](https://openairdocs.org/sdr/CALA2025112711512.md): Skin · within limits · Nov 25, 2025 · N29129 · Boeing 757224 · Passenger/Crew Doors
  > L1 DOOR EXTERNAL SKIN ADJACENT TO UPPER EXT HANDLE HAS DENT. UPON FURTHER INVESTIGATION OF THE L1 DOOR EXTERNAL SKIN, FOUND TO BE WITHIN LIMITS IAW ESFR 2456 WC:139023.
- [SDR CALA2025092309159](https://openairdocs.org/sdr/CALA2025092309159.md): Girt Bar · out of adjust · Sep 20, 2025 · N29129 · Boeing 757224 · Emergency Equipment
  > R1 DOOR WILL NOT ARM. ADJUSTED GIRT BAR MECHANISM OF THE SLIDE RAFT. ACCOMPLISHED IAW AMM SUB TASK 25-66-10-712-031. CYCLED ARM LEVER DOOR OPENED/CLOSED PROPERLY IS TIME.CHECK GOOD.
- [SDR CALA2025091909063](https://openairdocs.org/sdr/CALA2025091909063.md): Girt Bar · fod · Sep 17, 2025 · N29129 · Boeing 757224 · Emergency Equipment
  > DOOR 1R NOT ARMING, REMOVED DEBRI BETWEEN GIRT BAR AND FLOOR. PERFORMED OPS CK PER AMM 52-11-00, OPS CK GOOD
- [SDR CALA2025080507294](https://openairdocs.org/sdr/CALA2025080507294.md): Unknown · odor · Aug 4, 2025 · N29129 · Boeing 757224 · Air Distribution System
  > STRONG FUEL SMELL IN ACFT DURING APU OPERATION. PERFORMED INSPECTION OF AC AND APU COMPARTMENT FOR FUEL LEAKS. NO LEAKS FOUND. NO SMELL OF FUEL FOUND. RAN THE PACKS FOR 45 MINS. NO FUEL SMELL. OK TO CONTINUE.
- [SDR CALA2025071106452](https://openairdocs.org/sdr/CALA2025071106452.md): Lanyard · unsecure · Jul 8, 2025 · N29129 · Boeing 757224 · Emergency Equipment
  > ROPE HANGING OUT OF SLIDE AT DOOR 1R ROPE SECURED AS REQUIRED. NO OTHER DEFECTS NOTED AS THIS TIME. DOOR ARMED AND DISARMED SEVERAL TIMES, FOUND SATISFACTORY. OPERATIONAL CHECK OF DOOR CARRIED OUT, FOUND SATISFACTORY.
- [SDR CALA2025040103403](https://openairdocs.org/sdr/CALA2025040103403.md): Regulator Valve · faulted · Mar 30, 2025 · N29129 · Boeing 757224 · Pneumatic Distribution System
  > L ENG BLEED OFF EICAS MSG DISPLAYED DURING TAKEOFF RTO AT AAPR OX 80KTS. REMOVED AND REPLACED #1 ENG PRSOV REF AMM 36-11-09-002-047-001 UP TO AND INCLUDING STEP 4.H.1(T) PERFORMED OPS CHECK FOR L/ENG PRSOV INSTALLATION REF AMM 36-11-09-002-047-001 OPS CHEC
- [SDR CALA2025031402840](https://openairdocs.org/sdr/CALA2025031402840.md): Cover · damaged · Mar 14, 2025 · N29129 · Boeing 757224 · Escape Slide
  > DOOR 4L SLIDE COVER SHOWS DAMAGE DAMAGE IS 2.5 INCHES BY 2.5 INCHES DAMAGE HAS NOT GONE ALL WAY THRUE BUSTLE. SEE PICS PERFORMED ECRA 2560-03395 PART 1 B REQUIRES REPETITIVE INSPECTION EVERY 3 CALENDAR DAYS PERMINENT REPAIR WITHIN 15 DAYS. 4L DOOR SLIDE BUSTL
- [SDR CALA2024120301394](https://openairdocs.org/sdr/CALA2024120301394.md): Shutoff Valve · faulty · Nov 30, 2024 · N29129 · Boeing 757224 · Pneumatic Distribution System
  > LH ENG BLEED OFF CAUTION MESSAGE INTMT. REMOVED & REPLACED #1 ENG PRESSURE REGULATING & SHUTOFF VALVE IAW AMM 36-11-09. U026317 U246260. U070317 PERFORMED LOW IDLE RUN & HIGH POWER RUN ON #1 ENG, PERFORMED LEAK AND OPS CHK GOOD IAW AMM 36-11-09/201.
- [SDR CALA2024090502387](https://openairdocs.org/sdr/CALA2024090502387.md): Support Bracket · cracked · Sep 4, 2024 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > B757-06-3-0239: RH W/W MLG, FWD EDGE OF THE CUTOUT, SUPPORT BRAC KETS HAVE CRACKED (2EA). REMOVED AND REPLACED SUPPORT BRACKETS (2EA) IN RH WW MLG FWD EDG E OF THE CUTOUT P/N UA149N7550-172024-0.040C IAW B757-200 SRM 5 1-40-02-0G-0.
- [SDR CALA2024090502385](https://openairdocs.org/sdr/CALA2024090502385.md): Stringer · dented · Sep 4, 2024 · N29129 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > B757-06-3-0241: AFT CARGO COMPARTMENT LEFT SIDE FR 1420 S-25L TO S-26L HAS (01EA) DENT. PERFORMED REPAIR ON STA 1420 S-25L TO S-26L IAW B757-200 SRM 53- 00-07-2R-5 DETAIL III.
- [SDR CALA2024090402377](https://openairdocs.org/sdr/CALA2024090402377.md): Skin · dented · Sep 3, 2024 · N29129 · Boeing 757224 · Fuselage Main, Plate/Skin
  > PROTRUDING DENT AT STA 710 AT S23 RT LWR FUSELAGE. PERFORMED REPAIR SKIN FUSELAGE AT STA 700 TO 720 BETWEEN S23 R/H TE S24 RH IAW B757-200 SRM 53-00-01-2R-29.
- [SDR CALA2024090302363](https://openairdocs.org/sdr/CALA2024090302363.md): Skin · dented · Sep 2, 2024 · N29129 · Boeing 757224 · Fuselage Main, Plate/Skin
  > NEW DENT DAMAGE WAS LOCATED AT STA 221.5 AND 1 5 INCHES BELOW S-20L. DENT MEASURE OUT AT.068" DEEP WITH LENGTH OF 4.00" (REPAIR PER SRM). PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN AT STA 221.5 AND 15 INCHES BELOW S-20L IAW B757-200 SRM 53-00-01-2R-29.
- [SDR CALA2024053101652](https://openairdocs.org/sdr/CALA2024053101652.md): Metering Valve · inoperative · May 19, 2024 · N29129 · Boeing 757224 · Landing Gear Steering System
  > ON TAXI AND T/O ROLL AIR CRAFT HAD STRONG LEFT TU RN BIAS. T/O R OLL REQRD ABNORM AMT RT RUDR/0WI PER FIM 32-51 FAULT TREE 802 STEP 1 LUBRICATED THE NOSE LANDING TAXIED AIRCRAFT WHEN TILLER IS RELEASED AC DRIFTS TO THE LEFT STEERING COLLAR, AND CHECKD ALL LAN
- [SDR CALA2024052001517](https://openairdocs.org/sdr/CALA2024052001517.md): Warning Message · illuminated · May 18, 2024 · N29129 · Boeing 757224 · Pneumatic Distribution System
  > L ENG BLEED OFF CAS AFTER ENG START BLEED PSI PULSING UP AND DO WN 15 PSI DEBRIEF CREW. LEFT ENG BLEED PULSING AT ENG START WITH BLEED OFF INDICATION. EVEN WHEN ADDING POWER STILL PULSING. EVENTUALLY BLEED OFF INDICATION EXTINGUISHED BUT ENGINE BLEED STILL FL
- [SDR CALA2024030400620](https://openairdocs.org/sdr/CALA2024030400620.md): Controller · faulted · Mar 1, 2024 · N29129 · Boeing 757224 · Cabin Pressure Controller
  > CAB ALT EICAS FL360 AUTO 1. EMERG DESCENT 10K. CA B ALT LESS 12K. OPS NOR M AUTO2. R/R CABIN PRESSURE CONTROLLER 1. REF AMM 21-31-02. OPS CHECK GOOD PARTS USED: 19-2131-9-0004,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1588665 SN OFF 0507 CONTROLLER, CA
- [SDR CALA2024020700341](https://openairdocs.org/sdr/CALA2024020700341.md): Connector · disconnected · Feb 5, 2024 · N29129 · Boeing 757224 · Light System Wiring
  > SEAT FLOOR PROX EMER LT AT 3B, 4B, AND LAV S MONUMENT LIGHT INOP. FOUND CANNON PLUG UNDER 2B DISCONNECTED. RESECURED CANNON PLUG. OPS CK OF 3B, 4B, AND LAV S MONUMENT LIGHT GOOD REF AMM 33-51-11. INSPECTION TO FOLLOW INSPECTED EMERGENCY LIGHTS FOR PROPER REPAI
- [SDR CALA2023011600129](https://openairdocs.org/sdr/CALA2023011600129.md): Bracket · cracked · Jan 16, 2023 · N29129 · Boeing 757224 · Fuselage Main, Attach Fittings
  > DURING FRAME REPAIR PER SRM 53-00-07-2R-8, REPAIR 8 - A/C BRKT LOCATION STA 1540 LT SIDE, A CRACK INDICATION WAS FOUND AT STR 9LT STR TIE I/B FASTENER LOCATION. AT THE STR 8LT STR TIE LOCATION, THE O/B FASTENER LOCATION WAS DRILLED IN ERROR TO.430. THIS LOG
- [SDR CALA2023011100088](https://openairdocs.org/sdr/CALA2023011100088.md): Frame · cracked · Jan 10, 2023 · N29129 · Boeing 757200 · Fuselage Main, Frame
  > STATION 760 LEFT CABIN FRAME CRACKED AT I/B RIVET FOR PSU RAIL ATTACH BRACKET. PLEMENTAL INSPECTIONS PER SRM 53-00-07-2R-8 PART 5.A. TABLE 203 TIONS AS GIVEN IN TABLE 203/REPAIR 8 AT 12000 FLIGHT CYCLES FROM E INTERVALS. REPAIR METHOD IS DETAILED VISUAL INSPEC
- [SDR CALA2023011100087](https://openairdocs.org/sdr/CALA2023011100087.md): Frame · cracked · Jan 10, 2023 · N29129 · Boeing 757200 · Fuselage Main, Frame
  > STATION 640 RIGHT CABIN FRAME CRACKED AT I/B RIVET FOR PSU RAIL ATTACH BRACKET. INSPECTIONS PER PART 5.A. TABLE 203 AND FIGURE 203 SHEET 2 FOR ZO EPAIR 8 AT 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION AND REPE DETAILED VISUAL INSPECTION. NE 3 REPAIR. NEED TO
- [SDR CALA2023011100086](https://openairdocs.org/sdr/CALA2023011100086.md): Frame · cracked · Jan 10, 2023 · N29129 · Boeing 757200 · Fuselage Main, Frame
  > STATION 1580 LEFT CABIN FRAME CRACKED AT I/B RIVET FOR PSU RAIL ATTACH BRACKET. INSPECTIONS PER PART 5.A. TABLE 203 AND FIGURE 203 SHEET 6 FOR ZO EPAIR 8 AT 50000 AIRFRAME FLIGHT CYCLES AND REPEAT INSPECTIONS A SUAL INSPECTION. NE 2 REPAIR. NEED TO PERFORM INS
- [SDR CALA2023011100085](https://openairdocs.org/sdr/CALA2023011100085.md): Frame · cracked · Jan 10, 2023 · N29129 · Boeing 757200 · Fuselage Main, Frame
  > STATION 1580 RIGHT CABIN FRAME CRACKED AT I/B RIVET FOR PSU RAIL ATTACH BRACKET. INSPECTIONS PER PART 5.A. TABLE 203 AND FIGURE 203 SHEET 6 FOR ZO EPAIR 8 AT 50000 AIRFRAME FLIGHT CYCLES AND REPEAT INSPECTIONS A SUAL INSPECTION. NE 2 REPAIR. NEED TO PERFORM IN
- [SDR CALA2023011100084](https://openairdocs.org/sdr/CALA2023011100084.md): Frame · cracked · Jan 10, 2023 · N29129 · Boeing 757200 · Fuselage Main, Frame
  > STATION 760 RIGHT CABIN FRAME CRACKED AT I/B RIVET FOR PSU RAIL ATTACH BRACKET.INSPECTIONS PER PART 5.A. TABLE 203 AND FIGURE 203 SHEET 2 FOR ZO EPAIR 8 AT 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION AND REPE DETAILED VISUAL INSPECTION. NE 3 REPAIR. NEED TO P
- [SDR CALA2023011100083](https://openairdocs.org/sdr/CALA2023011100083.md): Frame · cracked · Jan 10, 2023 · N29129 · Boeing 757200 · Fuselage Main, Frame
  > STATION 1120 LEFT CABIN FRAME CRACKED AT I/B RIVET FOR PSU RAIL ATTACH BRACKET. INSPECTIONS PER PART 5.A. TABLE 203 AND FIGURE 203 SHEET 4 FOR ZO EPAIR 8 AT 50000 AIRFRAME FLIGHT CYCLES AND REPEAT INSPECTIONS A UAL INSPECTION. NE 1 REPAIR. NEED TO PERFORM INSP
- [SDR CALA2023010600049](https://openairdocs.org/sdr/CALA2023010600049.md): Floorbeam · corroded · Jan 5, 2023 · N29129 · Boeing 757224 · Fuselage Main, Floor Beam
  > L/P GENERATED FOR ESFR REPORTING-FWD WET AREA FLOOR BEAM CHORD HAS CORROSION STA 365.25 RBL61. SEE NR 001094009 FOR FLOOR BEAM CHORD REPAIR-REPAIRED FLOOR BEAM REF SRM 53-00-51-2R-8.
- [SDR CALA2023010600048](https://openairdocs.org/sdr/CALA2023010600048.md): Floorbeam · corroded · Jan 5, 2023 · N29129 · Boeing 757200 · Fuselage Main, Floor Beam
  > L/P GENERATED FOR ESFR REPORTING-FWD WET AREA FLOOR BEAM UPPER CHORD HAS CORROSION STA 395 RBL 61. SEE N/R 001094012 FOR REPAIR-REPAIRED FLOOR BEAM UPPER CAP REF SRM 53-00-51-2R-8.
- [SDR CALA2020020300310](https://openairdocs.org/sdr/CALA2020020300310.md): Unknown · unknown · Jan 26, 2020 · N29129 · Boeing 757224 · Landing Gear Brake System
  > #6 BRAKE REQUIRES CHANGE DUE ANTI SKIP REMOVED AND REPLACED #6 BRAKE IAW AMM 32-41-10 NO DEFECTS NOTED AIRCRAFT OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1015201 SN OFF 0901 BRAKE, MLG, ATA OFF 53-3241-9-0002 0901 ON 53-3241-9-0002 1120 INSPE
- [SDR CALA2020011300144](https://openairdocs.org/sdr/CALA2020011300144.md): Charger · inoperative · Jan 11, 2020 · N29129 · Boeing 757224 · Emergency Lighting
  > EMERGENCY ESCAPE PATH AISLE LIGHTING IS INOPERATIVE FROM SEAT 07C TO 20C. FOUND BATTERY PACK POWER SUPPLY INOPERATIVE FOR LEFT SEAT SECTION ROW 07 TO 20. REPLACED POWER SUPPLY BATTERY CHARGER ASSY PER AMM 33-51-07-862-054. OPS CHECK OF EMERGENCY LIGHTS NOW N
- [SDR CALA2019071501203](https://openairdocs.org/sdr/CALA2019071501203.md): Idg · failed · Jul 15, 2019 · N29129 · Boeing 757224 · AC Generator-Alternator
  > RIGHT GEN FAILED - 1 RESET ATTEMPTED WIT NO SUCCESS REMOVED AND REPLACED #2 ENG IDG REF AMM 24-11-01-424-002 ACP''D STEPS A.THRU H.(10) NEED TO START FROM (11)TO END. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1233393 SN OFF 0755 GENERATOR, INTE OFF 19-2420-9
- [SDR CALA2018111202357](https://openairdocs.org/sdr/CALA2018111202357.md): Line · chafed · Nov 12, 2018 · N29129 · Boeing 757224 · Hydraulic System, Main
  > CREW REPORTS LOST LH HYDRAULIC FLUID FOUND IN LH WHL WELL TWO HYDRAULIC LINES CHAFING. ONE A RETURN LINE 271N6441-1429 M&E 19-2911-3-0209. THE OTHER LINE IS FROM AUTOPLT LATERAL CONTROL GUIDANC SERVO 271N6441-1147 M&E 19-2911-3-0184 SEE IPC 29-11-51-39B ITEM
- [SDR CALA2018043001211](https://openairdocs.org/sdr/CALA2018043001211.md): Strap · cracked · Apr 26, 2018 · N29129 · Boeing 757224 · Fuselage Miscellaneous Structure
  > STABILIZATION STRAP CRACKED BELOW MAIN CABIN FLOORBEAM AT BS 1380, RBL 45. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-51, REPAIR 12, PARA 4, DETAIL VIII.
- [SDR CALA2018043001210](https://openairdocs.org/sdr/CALA2018043001210.md): Skin · dented · Apr 26, 2018 · N29129 · Boeing 757224 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND ON THE LT FUSLAGE SKIN AT BS 223.5 BELOW STRINGER 23L. FOUND TO BE OUT OF LIMITS. COMPLIED WITH ECRA 5330-06354.
- [SDR CALA2018043001209](https://openairdocs.org/sdr/CALA2018043001209.md): Skin · dented · Apr 26, 2018 · N29129 · Boeing 757224 · Auxiliary Power Unit (APU) Doors
  > LEFT APU DOOR EXTERIOR HAS THREE DENTS. BS 1925, 7.5 INCHES FROM UPPER EDGE, A SMALL CRACK LOCATED IN THE DENT, REPAIRED IAW SRM 52-40-01, ADS, FIG 101.
- [SDR CALA2018041301164](https://openairdocs.org/sdr/CALA2018041301164.md): Skin · chafed · Apr 12, 2018 · N29129 · Boeing 757224 · Leading Edge Devices
  > LEFT WING, NR 3 SLAT LOWER SKIN, WS 537 AND 453 CHAFED. FOUND TO BE OUT OF LIMITS IAW 57-43-02, FIG 101. REPAIRED THE SKIN IAW EC/RA 5740-02861, REV-, AND REV A.
- [SDR CALA2018041201151](https://openairdocs.org/sdr/CALA2018041201151.md): Skin · chafed · Apr 10, 2018 · N29129 · Boeing 757224 · Leading Edge Devices
  > LEFT WING NR 2 SLAT HAS TWO CHAFES ON THE BOTTOM SIDE OF THE SLAT AT WS 623 AND 590. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101, REPAIRED IAW EC/RA 5740-02862, REV.
- [SDR CALA2018041201150](https://openairdocs.org/sdr/CALA2018041201150.md): Skin · chafed · Apr 10, 2018 · N29129 · Boeing 757224 · Leading Edge Devices
  > LEFT WING NR 4 SLAT LOWER SIDE, UPPER EDGE CHAFED AT WS 397.5. FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101. REPAIRED IAW EC/RA 5740-02860, REV.
- [SDR CALA2018041001145](https://openairdocs.org/sdr/CALA2018041001145.md): Skin · cracked · Apr 10, 2018 · N29129 · Boeing 757224 · Leading Edge Devices
  > NR 10 SLATHAS A CRACK IN THE SKIN. REPAIRED THE SLAT IAW SRM 57-43-01, PG 201-205.
- [SDR CALA2018041201149](https://openairdocs.org/sdr/CALA2018041201149.md): Skin · dented · Apr 9, 2018 · N29129 · Boeing 757224 · Fuselage Main, Plate/Skin
  > DENT FOUND ON THE LT FUSELAGE SKIN, AFT OF ANGLE OF ATTACK AT APPROXIMATELY BS 254 ABOVE STRINGER 20L, FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL 3. REPAIRED IAW ECRA 5330- 06357, REV-ORIGINAL.

Next page: https://openairdocs.org/aircraft/N29129/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 = 'N29129' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N29129/reports

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