# Service difficulty reports: N962WN

A list on [N962WN](https://openairdocs.org/aircraft/N962WN.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 · 194 reports

- [SDR SWAA2026102227749](https://openairdocs.org/sdr/SWAA2026102227749.md): Hook · loose · Oct 18, 2026 · N962WN · Boeing 7377H4 · Emergency Equipment
  > R1 ESCAPE SLIDE PACK GIRT BAR HOOKS LOOSE. REMARKS: R1 GIRT BAR RETAINING PIN/BOLT IS LOOSE. RE SECURED R1 BIRT BAR RETAINING CLIP PER SRM 51-40-02.
- [SDR SWAA2026092810636](https://openairdocs.org/sdr/SWAA2026092810636.md): Fuse · inoperative · Sep 21, 2026 · N962WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT LOWER WTBF EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED FUSE AND LAMP IAW AMM 33-51-04-960-801 AND B737 AMM 33-51-06-960-804 TEST PASSED. VERIFIED REMOVED AND REPLACED FUSE AND LAMP IAW AMM 33-51-04-960-801 AND AMM 33-51-06-960-804. TEST PASSE
- [SDR SWAA2026092807453](https://openairdocs.org/sdr/SWAA2026092807453.md): Lamp · inoperative · Sep 21, 2026 · N962WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT LOWER WTBF EMERGENCY LIGHT IS INOPERATIVE. R & R THE FUSE AND LAMP IAW AMM 33-51-04-960-801, AND AMM 33-51-06-960-804. TEST PASSED.
- [SDR SWAA2026083127823](https://openairdocs.org/sdr/SWAA2026083127823.md): Floor Panel · cracked · Aug 26, 2026 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > 3 INCH CRACK ON CARGO PIT FLOOR PANEL 120CF IN FWD CARGO PIT._ PERFORMED PERMANENT REPAIR TO 3 INCH CRACK ON CARGO PIT FLOOR PANEL 120CF IN FWD CAR PIT REF AMM25-52-01.
- [SDR SWAA2026070216973](https://openairdocs.org/sdr/SWAA2026070216973.md): Rub Block · broken · Jun 29, 2026 · N962WN · Boeing 7377H4 · Emergency Equipment
  > FO SIDE FWD SERVICE DOOR GIRT BAR RUB CLIP BROKEN. R & R FO SIDE FWD GIRT BAR STOP RELEASE ASSEMBLY IAW AMM 25-66-01. OPS CHECKED GOOD.
- [SDR SWAA2026052605474](https://openairdocs.org/sdr/SWAA2026052605474.md): Seal · cracked · May 22, 2026 · N962WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. R & R RT UPPER HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.
- [SDR SWAA2025110631166](https://openairdocs.org/sdr/SWAA2025110631166.md): Rivet · missing · Nov 3, 2025 · N962WN · Boeing 7377H4 · Emergency Equipment
  > FOUND R1 DOOR RT BOTTOM RIVET MISSING ON GIRT BAR RETAINING CLIP. INSTALLED NEW RIVET ON MISSING R1 DOOR RT BOTTOM CLIP PER SIP.
- [SDR SWAA2025102728361](https://openairdocs.org/sdr/SWAA2025102728361.md): Rivet · missing · Oct 24, 2025 · N962WN · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY SERVICE DOOR SLIDE AFT GIRT BAR RETAINER MISSING 1 RIVET. INSTALLED INTERIM REPAIR PER E.A. M-23-125-01839.
- [SDR SWAA2025070178850](https://openairdocs.org/sdr/SWAA2025070178850.md): Pressure Deck · cracked · Jun 6, 2025 · N962WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FOUND 0N UPPER PRESSURE DECK AT STA 663 RBL 40 WL 204 MARKED IN BLACK. REPAIRED PER SRM 53-40-51-2R-2-A01022, REPAIR 2, BEADED PRESSURE DECK WEB REPAIR BETWEEN STA 663.75 AND STA 675 - PERMANENT.
- [SDR SWAA2025070178372](https://openairdocs.org/sdr/SWAA2025070178372.md): Stub Frame · cracked · Jun 5, 2025 · N962WN · Boeing 7377H4 · Fuselage Main, Frame
  > FWD GALLEY DOOR CUTOUT; FWD FRAME STA 294.5; UPPER STUB FRAME HAS APROX.5' CRACK AT THE TOP END OF SEAL DEPRESSOR. MARKED IN BLACK. REF. CARD TTG8Q00TSZJ9 CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS<[01] REMOVED STA 294.5 FRAME ASSY I.A.W. SRM 51-40-02-0G-0 F
- [SDR SWAA2025070178366](https://openairdocs.org/sdr/SWAA2025070178366.md): Skin · corroded · Jun 4, 2025 · N962WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > 154-33 RIGHT SIDE FUSELAGE SKIN AT WATER SERVICE DOOR CUTOUT HAS EVEIDENCE OF CORROSION. REPAIRED PER EA 25-153-01610.
- [SDR SWAA2025050566135](https://openairdocs.org/sdr/SWAA2025050566135.md): Handle · loose · May 1, 2025 · N962WN · Boeing 7377H4 · Service Doors
  > AFT GALLEY SERVICE DOOR UPPER ASSIST HANDLE LOOSE.<[01] RESECURED AFT GALLEY SERVICE DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.
- [SDR SWAA2025050266136](https://openairdocs.org/sdr/SWAA2025050266136.md): Girt Bar · unsecure · May 1, 2025 · N962WN · Boeing 7377H4 · Emergency Equipment
  > AFT GALLEY SERVICE DOOR GIRT HANGS TOO LOW.<[01] RESECURED AFT GALLEY SERVICE DOOR GIRT REF AMM 25-66-01.
- [SDR SWAA2024101045616](https://openairdocs.org/sdr/SWAA2024101045616.md): Lamp · inoperative · Oct 6, 2024 · N962WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY EMERGENCY SLIDE LIGHT INOP<[01] RELAMPED AFT ENTRY EMERGENCY SLIDE LIGHT REF AMM 33-51-04 OPS CHECK GOOD
- [SDR SWAA2024070809484](https://openairdocs.org/sdr/SWAA2024070809484.md): Lens · missing · Jul 5, 2024 · N962WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN MISSING @ RH EMERGENCYEXIT ROW.<[01] REPLACED EMERGENCY EXIT SIGN LENS @ RH EMERGENCYEXIT ROW. REF AMM 33-51-01.
- [SDR SWAA2024030860442](https://openairdocs.org/sdr/SWAA2024030860442.md): Bracket · cracked · Mar 8, 2024 · N962WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > RIGHT WING FIXED TRAILING EDGE PANEL; BETWEEN SPOILERS 7 AND 8; HAS A CRACKED BRACKET ON OUTBOARD SIDE.<[01] 04 - REPAIRED PER [SRM 57-51-02-2R-3-A01269 (REPAIR 3 - WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACK DAMAGE REPAIR - PERMANE
- [SDR SWAA2023092704121](https://openairdocs.org/sdr/SWAA2023092704121.md): Engine · smoke · Sep 23, 2023 · N962WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > ON DESCENT; APPROXIMATELY 18000; NO. 1 ENGINE SURGED ONCE. N1 WENT TO THE RED LINE; EGT WENT RED; APPROX 813C AND THEN WE SMELLED A SLIGHT BURNT SMELL. RAN QRC AND QRH. IT DID NOT DIRECT A SHUTDOWN. CONTINUING DESCENT WITH BOTH THRUST LEVERS AT IDLE NO. 1 INDI
- [SDR SWAA2023081689200](https://openairdocs.org/sdr/SWAA2023081689200.md): Rivet · loose · Aug 13, 2023 · N962WN · Boeing 7377H4 · Emergency Equipment
  > DOOR R1 GIRT BAR BRACKET LOOSE<[01] SECURED LOOSE RIVIT;SECURED R-1 DOOR SLIDE REF MT 25-66-06;SIP
- [SDR SWAA2023081487274](https://openairdocs.org/sdr/SWAA2023081487274.md): Vapor Barrier · cracked · Aug 9, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Structure
  > RT MLG W/W FWD VAPOR BARRIOR HAS AN 11' CRACK JUST INBD OF B SYSTEM RETURN FILTER<[01] PERFORMED REPAIR ON RH MLG W/W FWD VAPOR BARRIER PER SRM 57-10-10-1A-2; PARAGRAPH 2. C. (4) (B). REINSPECT REQUIRED AT 1200 CYCLES.;[02] ENGINEERING CONCURS REPAIR IS APPLIC
- [SDR SWAA2023071176880](https://openairdocs.org/sdr/SWAA2023071176880.md): Screw · broken · Jul 9, 2023 · N962WN · Boeing 7377H4 · Emergency Exits
  > LEFT OVERWING EMERGENCY EXIT HANDLE COVER BROKEN<[01] REPLACED MISSING SCREWS FOR LIFT HANDLE PER AMM 52-22-51
- [SDR SWAA2023070571112](https://openairdocs.org/sdr/SWAA2023070571112.md): Battery Pack · inoperative · Jun 24, 2023 · N962WN · Boeing 7377H4 · Emergency Lighting
  > AFT EMERGENCY LIGHTS ASSOCIATED WITH M1673 INOP<[01] DURING TROUBLESHOOTING IT FOUND BROKEN GROUND BLOCK (GD03948). OPEN GROUND 1 AND 7 FROM D10746 CONNECTOR CONTINUITY CHECK PERFOMED PER WDM 33-51-11.<BR><BR>TOOL USED:<BR>MULTIMETER ID: ATS1511 SN: UNK DD:05/
- [SDR SWAA2023070559173](https://openairdocs.org/sdr/SWAA2023070559173.md): Scuff Plate · cracked · Jun 15, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE IS CRACKED.<[01] WELDED RADIUS OF AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) (4)<BR>EQUIP USED: WELDING MACHINE E10583; CALIBRATION DUE DAT
- [SDR SWAA2023070555010](https://openairdocs.org/sdr/SWAA2023070555010.md): Stringer · corroded · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-23R WL164.<[01] CUT OUT DAMAGE SECTION FROM BS 500D + 3 TO 540 PER REF SRM 51-10-02;[02] REMOVED SHEAR TIE BETWEEN STR 23-22 ABD BS 520 PER REF SRM 51-40-02;[03] REQUIRE NDI TO VERIFY CRACK FREE CONDIT
- [SDR SWAA2023070555116](https://openairdocs.org/sdr/SWAA2023070555116.md): Fitting · corroded · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION ON STRINGER END FITTING AT AREA AFT OF ACB BS1015 RBL4 WL189.<[01] EVALUATED EXFOLIATION CORROSION AT STRINGER END FITTING FOUND TO BE OUT OF LIMITS NO FOUND LIMITS ON SRM REPAIR BY REPLACEMENT OF THE PART PER SRM 51-10-02-0G-0 STEP 9;[02] REMOVED ST
- [SDR SWAA2023070554705](https://openairdocs.org/sdr/SWAA2023070554705.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242RF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 242RF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2023070554709](https://openairdocs.org/sdr/SWAA2023070554709.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO AMOUNT OF DAMAGE FLOOR PANEL 241AAF WILL BE REPLACED WITH NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A NOTE. <BR><BR>FABRICATED PANEL USING BMS 4-17 TY6 LOT#1526676-1; APPLIED ALL
- [SDR SWAA2023070554719](https://openairdocs.org/sdr/SWAA2023070554719.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF UPPER SKIN HAS PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2023070554721](https://openairdocs.org/sdr/SWAA2023070554721.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221FF UPPER SKIN HAS PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2023070554722](https://openairdocs.org/sdr/SWAA2023070554722.md): Floor Panel · broken · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221GF FWD O/B TANG IS BROKEN.<[01] FWD FLOOR PANEL 221GF WITH BROKEN FWD O/B TANG WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2023070555112](https://openairdocs.org/sdr/SWAA2023070555112.md): Angle · cracked · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CABLE INTERCOSTAL ATTACH ANGLE IS CRACKED IN RADIUS BS 692; RBL 1; WL 206<[01] REMOVED DAMAGED CABLE INTERCOSTAL ATTACH ANGLE BS 692; RBL 1; WL 206 IAW SRM 51-40-02;[02] FORMED NEW INTERCOSTAL ATTACH ANGLE BS 692; RBL 1 WL 206 MATERIAL USED 7075T0; 0.050' CL
- [SDR SWAA2023070565053](https://openairdocs.org/sdr/SWAA2023070565053.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241XF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED 241XF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 6; TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>WILL PERFORM WORK IAW SRM 53-00-50-2R-1<BR>REMOVED 2
- [SDR SWAA2023070554702](https://openairdocs.org/sdr/SWAA2023070554702.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01769;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023070554703](https://openairdocs.org/sdr/SWAA2023070554703.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ADF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01770;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023070554704](https://openairdocs.org/sdr/SWAA2023070554704.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AEF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01781;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023070554713](https://openairdocs.org/sdr/SWAA2023070554713.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242TF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01777;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023070565056](https://openairdocs.org/sdr/SWAA2023070565056.md): Floor Panel · cracked · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ABF LOWER SKIN IS CRACKED AT THE FWD O/B CORNER.<[01] IDENTIFIED PANEL 241ABF IAW SRM 53-00-50-0I-1 FIGURE 6; TABLE 6.<BR><BR>DAMAGE ON PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4 F.<BR><BR>DAMAGE TO BE REPAIRED PER SRM 53-
- [SDR SWAA2023070565057](https://openairdocs.org/sdr/SWAA2023070565057.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242SF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED 242SF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 6; TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>WILL PERFORM WORK IAW SRM 53-00-50-2R-1<BR>REMOVED 1
- [SDR SWAA2023070565058](https://openairdocs.org/sdr/SWAA2023070565058.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 242UF IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6 AND BOEING DWG 147A5810-95.<BR><BR>FOUND DAMAGE TO UPPER SURFACE SKIN PLIES TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PA
- [SDR SWAA2023070554706](https://openairdocs.org/sdr/SWAA2023070554706.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242VF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01779;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023070565052](https://openairdocs.org/sdr/SWAA2023070565052.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 242WF UPPER AND LOWER SKINS HAVE PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 6; <BR>TABLE 6; AND BOEING DWG DOC: 147A5810 ID: 0010.<BR><BR>PANEL DAMAGE TO UPPER SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMI
- [SDR SWAA2023070565062](https://openairdocs.org/sdr/SWAA2023070565062.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221AF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 2; TABLE 2; <BR>AND BOEING DWG DOC: 141A5810 ID: 0728.<BR><BR>PANEL DAMAGE TO UPPER SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM <
- [SDR SWAA2023070565059](https://openairdocs.org/sdr/SWAA2023070565059.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221DF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED PANEL 221DF MATERIAL IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2.<BR><BR>CLEANED PANEL REPAIR AREA IAW SRM 53-00-50-2R-0 PARA 5. A. (1).<BR><BR>FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-
- [SDR SWAA2023070565060](https://openairdocs.org/sdr/SWAA2023070565060.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222AF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED PANEL 222AF IAW SRM 53-00-50-0I-1.<BR>FOUND DAMAGE ON UPPER SURFACE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1.PARA 4.F.<BR>DAMAGE SHOULD BE REPAIRED PER SRM 53-00-50-2R-1.<BR><BR>RE
- [SDR SWAA2023070565061](https://openairdocs.org/sdr/SWAA2023070565061.md): Floor Panel · pulled · Jun 1, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 222BF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 222BF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1 <BR><B
- [SDR SWAA2023070554677](https://openairdocs.org/sdr/SWAA2023070554677.md): Sidewall Support · corroded · May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 767+3; RBL 22; WL 156<[01] REMOVED FWD SHIELD BS 767 -793 I.A.W SRM 51-40-02-0G-0.;[02] CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+3 WL 156; P/N 146A8127-12; AREA OT= 0.050'; RT=0.044'; X=0.006';
- [SDR SWAA2023070554693](https://openairdocs.org/sdr/SWAA2023070554693.md): Support · corroded · May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727A-727A+16; RBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727A-727A+16; RBL 22; WL 156; IN AREA OF 6' X 1' X 0.006' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO
- [SDR SWAA2023070565047](https://openairdocs.org/sdr/SWAA2023070565047.md): Strap · corroded · May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TENSION STRAP AT AFT PASSENGER CABIN BS1016+13 RBL3 WL208.<[01] CORROSION ON TENSION STRAP AT AFT PASSENGER CABIN FROM BS1016+13 RBL3 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM WILL BE REMOVED AND REPLACED
- [SDR SWAA2023070565046](https://openairdocs.org/sdr/SWAA2023070565046.md): Strap · corroded · May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TENSION STRAP AT AFT PASSENGER CABIN BS1016+13 LBL3 WL208.<[01] CORROSION ON TENSION STRAP AT AFT PASSENGER CABIN FROM BS1016+13 LBL3 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM WILL BE REMOVED AND REPLACED
- [SDR SWAA2023070565050](https://openairdocs.org/sdr/SWAA2023070565050.md): Strap · corroded · May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TENSION STRAP AT AFT PASSENGER CABIN BS1016+13 RBL18 WL208.<[01] CORROSION ON TENSION STRAP AT AFT PASSENGER CABIN FROM BS1016+13 RBL18 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM WILL BE REMOVED AND REPLAC
- [SDR SWAA2023070554691](https://openairdocs.org/sdr/SWAA2023070554691.md): Stringer · cracked · May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STR CLIP AT PASSENGER CABIN BS727D S-6L. MARKED.<[01] REMOVED STRINGER CLIP AT BS 727D; STR 6L PER SRM 51-40-02;[02] ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PAR

Next page: https://openairdocs.org/aircraft/N962WN/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 = 'N962WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N962WN/reports

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