# Service difficulty reports: N7715E

A list on [N7715E](https://openairdocs.org/aircraft/N7715E.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 4 · 200 reports

- [SDR SWAA2026091755360](https://openairdocs.org/sdr/SWAA2026091755360.md): Stud · missing · Sep 13, 2026 · N7715E · Boeing 7377BD · Emergency Equipment
  > DURING 5340-I-16918-NG (AD - EXTERNAL DVI AND NDT INSPECTIONS AT BS 663.75 FAILSAFE STRAP (PICKLE FORK). FOUND RH OVERWING EMERGENCY EXIT WINDOW DOOR IS MISSING STUDS FOR THE ROPE STOWAGE HOUSING INSTALLED STUDS TO RT OVER WING EXIT DOOR EMERGENCY ROPE STOWAGE
- [SDR SWAA2026070718909](https://openairdocs.org/sdr/SWAA2026070718909.md): Break Over · inoperative · Jul 5, 2026 · N7715E · Boeing 7377BD · Passenger Compartment Equipment
  > SEATS 15ABC WILL NOT STAY UP RIGHT WHEN OCCUPIED, REMAIN UP RIGHT WHEN UNOCCUPIED. SEATS 15ABC WILL NOT STAY UP RIGHT WHEN OCCUPIED REMAIN UPRIGHT WHEN UNOCCUPIED. ADJUSTED SEAT BACK BREAK OVER ROW 15 SEATS ABC IAW AMM 25-22-00.
- [SDR SWAA2026032482726](https://openairdocs.org/sdr/SWAA2026032482726.md): Slide · out of alignment · Mar 23, 2026 · N7715E · Boeing 7377BD · Escape Slide
  > L1 DOOR SLIDE PARTIALLY FELL OUT. REINSTALLED SLIDE IAW AMM 25-66-01 AND MT 725-61-06. A/C OK FOR SERVICE.
- [SDR SWAA2026011961786](https://openairdocs.org/sdr/SWAA2026011961786.md): Light · odor · Jan 15, 2026 · N7715E · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ILLUMINATED THE EMERGENCY EXIT LIGHTS IN THE CABIN ILLUMINATED WITHOUT A LOSS OF AIRCRAFT POWER. THIS EVENT WAS ACCOMPANIED SIMULTANEOUSLY WITH AN ODOR IN THE COCKPIT & FORWARD GALLEY. AFTERWARDS ONLY SOME OF THE EMERGENCY EXIT LIGHTS REM
- [SDR SWAA2026011962036](https://openairdocs.org/sdr/SWAA2026011962036.md): Assist Handle · loose · Jan 15, 2026 · N7715E · Boeing 7377BD · Passenger/Crew Doors
  > FORWARD ASSIST HANDLE LOOSE. SECURED FWD ENTRY DOOR ASSIST HANDLE REF MM 52-11-31
- [SDR SWAA2025101323837](https://openairdocs.org/sdr/SWAA2025101323837.md): Tat Probe · out of tolerance · Oct 11, 2025 · N7715E · Boeing 7377BD · Outside Air Temperature Indicator/Sensor
  > IAS DISAGREE ON TAKEOFF. R+R TOTAL AIR TEMPERATURE PROBE PER MM 34-21-06.
- [SDR SWAA2025063085509](https://openairdocs.org/sdr/SWAA2025063085509.md): Isolator · cracked · Jun 26, 2025 · N7715E · Boeing 7377BD · Emergency Equipment
  > FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED <[01]. R&R FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.; [02] C/W.
- [SDR SWAA2025040720796](https://openairdocs.org/sdr/SWAA2025040720796.md): Lamp · inoperative · Apr 2, 2025 · N7715E · Boeing 7377BD · Emergency Lighting
  > AFT LEFT SVC DOOR OUTSIDE EMERGENCY LIGHT INOP<[01] RELAMPED LH AFT EXTERIOR SLIDE LIGHT PER AMM 33-51-04.
- [SDR SWAA2025032508744](https://openairdocs.org/sdr/SWAA2025032508744.md): Wire · loose · Mar 24, 2025 · N7715E · Boeing 7377BD · Flight Control System Wiring
  > LE FLAP TRANSIT LIGHT ILLUMINATED; FLAP 2 AMBER TRANSIT LIGHT REMAINED ILLUMINATED ON OVERHEAD. PERFORMED QRH. LE FLAP 2 RETRACT SENSOR S170<[01] RESECURED RETRACT SENSOR S170 WIRING PER AMM 27-88-11. ACCOMPLISHED FSEU BITE PER FIM 27-51 TASK 801; NO ACTIVE FA
- [SDR SWAA2025013090851](https://openairdocs.org/sdr/SWAA2025013090851.md): Sign · missing · Jan 29, 2025 · N7715E · Boeing 7377BD · Emergency Lighting
  > L2 DOOR LOWER EMERGENCY EXIT SIGN DIRECTIONAL ARROW MISSING. <[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)].
- [SDR SWAA2025011384958](https://openairdocs.org/sdr/SWAA2025011384958.md): Light · inoperative · Jan 10, 2025 · N7715E · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1670 BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025011384299](https://openairdocs.org/sdr/SWAA2025011384299.md): Fuse · inoperative · Jan 9, 2025 · N7715E · Boeing 7377BD · Emergency Lighting
  > LOCATOR SIGN ON FWD LAV INOP<[01] REMOVED AND REPLACED INOP FUSE ON M1674 BATTERY CHARGER AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-804.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025011384300](https://openairdocs.org/sdr/SWAA2025011384300.md): Battery Pack · inoperative · Jan 9, 2025 · N7715E · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1673 BATTERY PACK INOP<[01] REPLACED BATTERY PACK EMERGENCY EXIT TO M1673 PER AMM 33-51-06-960-805. GOOD TEST.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025011383122](https://openairdocs.org/sdr/SWAA2025011383122.md): Megaphone · damaged · Jan 5, 2025 · N7715E · Boeing 7377BD · Emergency Equipment
  > FWD MEGAPHONE DAMAGED<[01] REMOVED AND REPLACED FWD MEGAPHONE IAW AMM 25-64-00-SWA-804.;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025011381907](https://openairdocs.org/sdr/SWAA2025011381907.md): Light · damaged · Dec 30, 2024 · N7715E · Boeing 7377BD · Emergency Lighting
  > AFT ENTRY CEILING EXIT LIGHT HOUSING DAMAGED<[01] REMOVED AND REPLACED AFT ENTRY CEILING EXIT LIGHT HOUSING IAW AMM 33-51-01-960-802. OPS CHECK GOOD.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
- [SDR SWAA2025011379643](https://openairdocs.org/sdr/SWAA2025011379643.md): Intercostal · cracked · Dec 20, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FOUND CRACK ON INTERCOSTAL B.S. 400-420 RBL 25 WL 152<[01] REMOVED AND REPLACED INTERCOSTAL ON BS 40-420 RBL 25 WL 152 IAW SRM 51-40-02 AND DWG 143A7505 ID: 0002 REV: B;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLET
- [SDR SWAA2025011379642](https://openairdocs.org/sdr/SWAA2025011379642.md): Link · cracked · Dec 19, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > PASSENGER MAIN CABIN FLOOR SUPPORT LINK IS CRACKED AT BS520 TO BS540 BL0 WL208<[01] REMOVED AND REPLACED PASSENGER MAIN CABIN FLOOR SUPPORT LINK BS-520 TO BS-540; BL-0; WL-208 IAW SRM 51-40-02-0G-0 AND DWG# 143A0060 REV-B;[02] RII VERIFIED CORRECTIVE ACTIONS;
- [SDR SWAA2025011377988](https://openairdocs.org/sdr/SWAA2025011377988.md): Vapor Barrier · cracked · Dec 16, 2024 · N7715E · Boeing 7377BD · Wing Main, Frame Structure
  > R/H VAPOR BARRIER BS 663 HAS CRACK ON UPPER EDGE 9.75 INCHES FROM I/B EDGE.<[01] R/H VAPOR BARRIER BS; 663; WITH CRACK ON THE UPPER EDGE; 9.75 INCHES FROM THE I/B EDGE; WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025011376867](https://openairdocs.org/sdr/SWAA2025011376867.md): Frame · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Frame
  > CRACKED FRAME AT PAX CABIN BS827 JUST BELOW S-8R. MARKED<[01] REPAIRED PER EA 24-153-03521;[02] CARD COMPLETE; AMT HAS ONE MEASUREMENT FIELD INCOMPLETE.;[03] ADDRESSED CORRECTIVE ACTION 2: COMPLETED MEASUREMENT FIELD.;[04] VERIFIED CORRECTIVE ACTION ITEMS; CAR
- [SDR SWAA2025011376872](https://openairdocs.org/sdr/SWAA2025011376872.md): Stringer · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-25R WL156. MARKED<[01] 'REPAIRED PER EA 24-153-03470. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06.';[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025011376876](https://openairdocs.org/sdr/SWAA2025011376876.md): Stringer · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26L WL153. MARKED<[01] REPAIRED S-26L BETWEEN BS 510 TO BS 540 PER SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
- [SDR SWAA2025011376877](https://openairdocs.org/sdr/SWAA2025011376877.md): Stringer · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED<[01] REMOVED AND REPLACED NEW SECTION OF STRINGER 26 RH PER REF SRM 53-00-03-2R-2-;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025011376870](https://openairdocs.org/sdr/SWAA2025011376870.md): Stringer · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-24L WL162. MARKED<[01] REPAIRED STR-24L WL 162 BETWEEN BS 510 TO BS 540 PER SRM 53-00-03-2R-1.;[02] APPLIED REPAIR AT S-24L BETWEEN BS 510 TO BS 540 PER SRM 53-00-03-2R-1 REPAIR 1;[03] VERIFIED ALL STEPS; C
- [SDR SWAA2025011376886](https://openairdocs.org/sdr/SWAA2025011376886.md): Intercostal · corroded · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT MAIN EBAY BS312 - BS323 LBL3 WL50. MARKED<[01] REMOVED AND REPLACED NEW INTERCOSTAL ASSY ON BS312 TO BS323 LBL3 IAW SRM 51-40-02; DWG 141A0650 ID:0004 REV: E AND DWG 141A0650 ID: 0009 REV: D;[02] VERIFIED ALL STEPS; CORRECTION ACTIO
- [SDR SWAA2025011376887](https://openairdocs.org/sdr/SWAA2025011376887.md): Web · corroded · Dec 12, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Structure
  > CORROSION ON WEB AT MAIN EBAY BS320 LBL46 WL171. MARKED<[01] REMOVED AND REPLACED WEB ON MAIN EBAY BS320 LBL46 WL 171 IAW SRM 51-40-02 AND DWG 141A1180 ID:0011 REV: B;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
- [SDR SWAA2025011376424](https://openairdocs.org/sdr/SWAA2025011376424.md): Seal · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Horizontal Stabilizer Miscellaneous Structure
  > RT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025011376597](https://openairdocs.org/sdr/SWAA2025011376597.md): Seal · cracked · Dec 12, 2024 · N7715E · Boeing 7377BD · Horizontal Stabilizer Miscellaneous Structure
  > LT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025011475721](https://openairdocs.org/sdr/SWAA2025011475721.md): Stiffener · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 157.10; 3RD VERTICAL STIFFENER IS CRACKED. RIB 8<[01] UPON FURTHER INVESTIGATION (HFEC INSPECTED IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.) NO CRACK NOTED. NO FURTHER ACTION REQUIRED.;[02] VER
- [SDR SWAA2025011475423](https://openairdocs.org/sdr/SWAA2025011475423.md): Sidewall Support · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727D - 727E+10 LBL 25<[01] THIS FAULT WILL BE ACCOMPLISHED ON TASK [TTG8Q00XHZNF];[02] VERIFIED FLOOR TO SIDEWALL SUPPORT HAS BEEN REMOVED FROM STA 727 - 847 LBL 25 AND WILL BE REPLACED ON TTG8Q00XHZNF
- [SDR SWAA2025011376007](https://openairdocs.org/sdr/SWAA2025011376007.md): Pressure Deck · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Structure
  > CRACK FOUND ON HORIZONTAL PRESSURE DECK AT BS 663+2; RBL 45+16; LENGTH: 0.7' CRACK FOUND ON HORIZONTAL PRESSURE DECK AT BS 663+2 RBL 24+16 WL 202 LENGTH: 0.7'<[01] REPAIRED THE HORIZONTAL PRESSURE DECK BETWEEN BS 663 AND BS 675; RBL 30 TO RBL 60 AND APPLIED A
- [SDR SWAA2025011375422](https://openairdocs.org/sdr/SWAA2025011375422.md): Support · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727A+18; 727B+17; 727E+8 - 767 RBL 25<[01] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR TO SIDEWAL SUPPORT FROM BS727 TO BS767 RBL25 WL156 <BR>IAW SRM 51-40-02 AND DWG 146A7500 REV: A;[02] VERIFIED RII CORRECTI
- [SDR SWAA2025011375425](https://openairdocs.org/sdr/SWAA2025011375425.md): Angle · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON NUTPLATES AT AFT CARGO BAY FWD SHIELD SUPPORT ANGLE STA 767-787; RBL 25<[01] REMOVED AND REPLACED ANGLE & SHIELD IAW SRM 51-40-02; DWG 146A8123 & DWG 146A0081<BR>AFT CARGO BAY BS767-BS794; RBL 25;[02] RII VERIFIED CORRECTIVE ACTIONS COMPLETE;[03]
- [SDR SWAA2025011385491](https://openairdocs.org/sdr/SWAA2025011385491.md): Shield · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON NUTPLATES AT AFT CARGO BAY FWD SHIELD SUPPORT ANGLE STA 767-787; RBL 25<[01] REMOVED AND REPLACED ANGLE & SHIELD IAW SRM 51-40-02; DWG 146A8123 & DWG 146A0081<BR>AFT CARGO BAY BS767-BS794; RBL 25;[02] RII VERIFIED CORRECTIVE ACTIONS COMPLETE;[03]
- [SDR SWAA2025011375994](https://openairdocs.org/sdr/SWAA2025011375994.md): Support · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500+10 - BS500A LBL23 WL156. MARKED<[01] REMOVED AND REPLACED SIDEWALL SUPPORT BS395-BS500D FCB LBL23 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A7500.;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT F
- [SDR SWAA2025011375989](https://openairdocs.org/sdr/SWAA2025011375989.md): Gusset · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Bulkhead
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED<[01] REMOVED AND REPLACED FCB AFT BULKHEAD GUSSET; P/N 143A9481-6; BS500D S19L WL193 IAW SRM 51-40-02 AND DWG 143A7902 REV C.;[02] JOB COMPLETE.;[03] VERIFIED ALL RII STEPS COMPLET
- [SDR SWAA2025011375981](https://openairdocs.org/sdr/SWAA2025011375981.md): Gusset · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Main, Bulkhead
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED<[01] REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET AT BS500D S-19R;WL193;IAW SRM 51-40-02 AND DWG#143A7902.;[02] VERIFIED ALL STEP; CORRECTION ACTION ITEM 1; MEASUREMENT
- [SDR SWAA2025011375990](https://openairdocs.org/sdr/SWAA2025011375990.md): Angle · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500C FWD SIDE LBL25 WL152.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500C FWD SIDE LBL25 WL152 IAW SRM 51-40-02 AND DWG#143A7505 REV B.;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025011375983](https://openairdocs.org/sdr/SWAA2025011375983.md): Angle · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B FWD SIDE LBL25 WL152.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE; AT FCB BS500B FWD SIDE LBL25 WL152 IAW SRM 51-40-02 AND DWG 143A7505 REV: B;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025011375984](https://openairdocs.org/sdr/SWAA2025011375984.md): Angle · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B FWD SIDE RBL25 WL152.<[01] REMOVED AND REPLACED ATTACH ANGLE AT FCB BS500B FWD SIDE RBL25 WL152 IAW SRM 51-40-02 AND DWG#143A7505 REV D;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025011375991](https://openairdocs.org/sdr/SWAA2025011375991.md): Angle · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500A FWD SIDE LBL25 WL152.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500A FWD SIDE LBL25 WL152 IAW SRM 51-40-02 AND DWG 143A7505 REV: -.;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025011375992](https://openairdocs.org/sdr/SWAA2025011375992.md): Angle · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 AFT SIDE LBL25 WL152.<[01] REMOVED AND REPLACED ANGLE AT FCB BS400 LBL25 WL152 (CLIP) P/N: 143A7502U5 IAW B737-700 SRM 51-40-02-0G-0. AND DRW 143A7505 REV: B ID: 0002;[02] JOB COMPLETE.;[03] VERIFIED STEP 1; CORREC
- [SDR SWAA2025011375985](https://openairdocs.org/sdr/SWAA2025011375985.md): Angle · cracked · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 AFT SIDE RBL25 WL152.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS400 AFT SIDE RBL25 WL152 IAW SRM 51-40-02 AND DWG 143A7505 ID: 0060 REV:-;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASURE
- [SDR SWAA2025011375993](https://openairdocs.org/sdr/SWAA2025011375993.md): Shield · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SHIELD AT FCB BS500+14 RBL23 WL156.<[01] UPDATED MEASUREMENT FIELD;[02] REMOVED AND REPLACED AFT SHIELD AT FCB BS492 TO BS 500A RBL23 WL156 IAW SRM 51-40-02 AND DWG#143A0080 REV: -;[03] VERIFIED CORRECTIVE ACTION #2
- [SDR SWAA2025011375424](https://openairdocs.org/sdr/SWAA2025011375424.md): Support · corroded · Dec 10, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727E+10 - 787 LBL 25<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT ACB P/N 146A7502-27 LOT# 1583867-1; BS727 TO BS 847 LBL25 IAW SRM 51-40-02 AND DWG 146A7500 REV B.;[02] JOB COMPLETE.
- [SDR SWAA2025011374941](https://openairdocs.org/sdr/SWAA2025011374941.md): Vapor Barrier · cracked · Dec 7, 2024 · N7715E · Boeing 7377BD · Wing Main, Frame Structure
  > CRACKED UPPER ANGLE ATTACH VAPOR BARRIER BS 663.5 RBL 48.5 (MARKED)<[01] REMOVED AND INSTALLED NEW ATTACH ANGLE ON VAPOR BARRIER BS663 RBL33-RBL64; PER SRM 57-10-10-2R-5 AND DWG 111A1000; ID: 178; REV: B;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLET
- [SDR SWAA2025011483538](https://openairdocs.org/sdr/SWAA2025011483538.md): Inlet · pulled · Dec 6, 2024 · N7715E · Boeing 7377BD · Nacelle/Pylon, Main Frame
  > #2 ENGINE INLET COWL LIP SKIN OUTER AFT ROW MULTIPLE FASTENERS DO NOT FLUSH WITH THE SKIN AT POSITION FROM 1 O'CLOCK TO 2 O'CLOCK POSITION.<[01] RECIEVED NEW/SERVICEABLE #2 ENGINE INLET COWL PN: 314M2100-503 SN: 3117001. INLET COWL INSTALLED ON CARD #TTG8Q00S7
- [SDR SWAA2025011374478](https://openairdocs.org/sdr/SWAA2025011374478.md): Panel · cracked · Dec 6, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > STA 540 BREAK PANEL IS CRACKED AT LBL 1; WL 208.<[01] REMOVED AND REPLACED NEW BREAK PANEL ON BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID: 0014 REV: B;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025011374479](https://openairdocs.org/sdr/SWAA2025011374479.md): Panel · cracked · Dec 6, 2024 · N7715E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > STA 540 BREAK PANEL IS CRACKED AT RBL 1; WL 208.<[01] REMOVED AND REPLACED NEW BREAK PANEL ON BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID: 0014 REV: B;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024111859859](https://openairdocs.org/sdr/SWAA2024111859859.md): Clamp · loose · Nov 14, 2024 · N7715E · Boeing 7377BD · Air Intake Anti/De-Ice System
  > ENG 1 OVERHEAT LIGHT AT CLEANUP REDUCED THRUST PER CHECKLIST; LIGHT OUT AFTER APROX 40-50 SECONDS. LANDED REDUCED THRUST; ENGINE INDICATION NORMAL REST OF FLIGHT AND DURING INCIDENT<[01] T/S FOUND #1 ENG TAI VALVE BYPASSING AIR AT AFT CLAMP. RESECURED CLAMP AN
- [SDR SWAA2024090533756](https://openairdocs.org/sdr/SWAA2024090533756.md): Skirt · worn · Sep 4, 2024 · N7715E · Boeing 7377BD · Escape Slide
  > FWD ENTRY DOOR ESCAPE SLIDE SKIRT WORN<[01] R&R FWD ENTRY DOOR ESCAPE SLIDE IAW AMM 25-66-01.<BR>REF BARCODE: TTG8Q00V9VPL.;[02] INSPECTION C/W R&R FWD ENTRY DOOR ESCAPE SLIDE IAW AMM 25-66-01.<BR>REF BARCODE: TTG8Q00V9VPL.

Next page: https://openairdocs.org/aircraft/N7715E/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 = 'N7715E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7715E/reports

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