# Service difficulty reports: Boeing 737-7AD

A list on [Boeing 737-7AD](https://openairdocs.org/model/boeing-737-7ad.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 312 reports

- [SDR SWAA2022012161755](https://openairdocs.org/sdr/SWAA2022012161755.md): Light · inoperative · Jan 17, 2022 · N798SW · Boeing 7377AD · Emergency Equipment
  > EMERGENCY EXIT LIGHT ARMED POSITION INOP; / [01] REPLACED EMERGENCY LIGHT GUARD SWITCH PER CMM 33-10-05. OPS CHECK GOOD AS PER AMM 33-51-00.
- [SDR SWAA2021120148898](https://openairdocs.org/sdr/SWAA2021120148898.md): Cover · missing · Nov 28, 2021 · N798SW · Boeing 7377AD · Emergency Lighting
  > EMERGENCY LIGHT COVER MISSING OVER PAX SEATS 2D. EMERGENCY LIGHT COVER WAS FOUND TO BE CABIN TEMP SCREEN. OK TO CONTINUE PER MEL 25-10-01. SP1
- [SDR SWAA2021102532194](https://openairdocs.org/sdr/SWAA2021102532194.md): Slide · out of position · Oct 20, 2021 · N798SW · Boeing 7377AD · Escape Slide
  > AFT SERVICE DOOR ESCAPE SLIDE SAGS; / [01] ACCOMPLISHED MT 725-61-06 TO REPOSITION AFT SERVICE DOOR SLIDE AS REQUIRED.
- [SDR SWAA2021080298470](https://openairdocs.org/sdr/SWAA2021080298470.md): Battery Pack · no test · Jul 27, 2021 · N798SW · Boeing 7377AD · Emergency Lighting
  > NUMEROUS EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. 6 LEFT AND LEFT OVERWING; LEFT 14;17;20;23. L2 DOOR SMALL SIGN; R2 DOOR BIG SIGN; / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS @ CONNECTORS; M1674; M1675;M1669;M1668;M1670;M1672;
- [SDR SWAA2021070892392](https://openairdocs.org/sdr/SWAA2021070892392.md): Rib · cracked · Jul 7, 2021 · N798SW · Boeing 7377AD · Trailing Edge Flaps
  > RIGHT WING I/B MAIN FLAP O/B L/E RIB CRACKED O/B OF AFT FLAP DRIVE ARM. REMOVED CRACKED RIB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW RIB IAW SRM 51-40-05-0G-0 AND DWG 113A2213 REV- AND 113A2100 REV E. TREATED AND PRIMED NEW RIB IAW AMM 51-21-41 51-21-9
- [SDR SWAA2021060980382](https://openairdocs.org/sdr/SWAA2021060980382.md): Cover · out of position · Jun 5, 2021 · N798SW · Boeing 7377AD · Galley Doors
  > MANUAL PULL HANDLE AFT GALLEY DOOR (FO SIDE) EXPOSED; / REPOSITION AFT GALLEY (R-2) DOOR SLIDE MANUAL HANDLE COVER IAW SIP
- [SDR SWAA2020120733314](https://openairdocs.org/sdr/SWAA2020120733314.md): Battery Pack · no test · Dec 1, 2020 · N798SW · Boeing 7377AD · Emergency Lighting
  > AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK, PER M/M 33-51-06.
- [SDR SWAA2020112732166](https://openairdocs.org/sdr/SWAA2020112732166.md): Sign · broken · Nov 23, 2020 · N798SW · Boeing 7377AD · Emergency Lighting
  > EMERGENCY EXIT SIGN AT R1 DOOR IS CRACKED & BROKEN. REPLACED R1 DOOR EMERGENCY EXIT SIGN, REF AMM 33-51-01.
- [SDR SWAA2020061190472](https://openairdocs.org/sdr/SWAA2020061190472.md): Light · inoperative · Jun 7, 2020 · N798SW · Boeing 7377AD · Emergency Lighting
  > AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW AMM 33-51-04.
- [SDR SWAA2020060184913](https://openairdocs.org/sdr/SWAA2020060184913.md): Battery Pack · discharged · May 27, 2020 · N798SW · Boeing 7377AD · Emergency Lighting
  > FORWARD RT CABIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD RT BATTERY PACK IAW AMM 33-51-09. OPS CHECK GOOD.
- [SDR SWAA2020051274972](https://openairdocs.org/sdr/SWAA2020051274972.md): Hydraulic Line · cracked · Apr 25, 2020 · N798SW · Boeing 7377AD · Hydraulic System, Main
  > WHILE CONFIGURING FOR LANDING; LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH TRAILING EDGE FLAPS AT 30. LE DEVICE PANEL ON OVERHEAD SHOWED ALL GREEN WITH LE FLAPS EXTENDED AND LE SLATS IN EXT. AFTER LANDING HYD SYSTEM B SHOWED RF AND 60%. ON INSPECTION; RIG
- [SDR SWAA2020042944965](https://openairdocs.org/sdr/SWAA2020042944965.md): Hydraulic Line · leaking · Apr 25, 2020 · N798SW · Boeing 7377AD · Hydraulic System, Main
  > REF LOG PAGE # 1391847. L/E IND / HYD LEAK / HYD QTY / SERVICED B SYSTEM HYD PER AMM 12-12-00. FOUND LINE LEAKING @ #7 SLAT ACTUATOR. REF AMM 29-00-00. REF LOG PAGE # 1391847 FOR CORRECTIVE ACTION
- [SDR SWAA2021081842584](https://openairdocs.org/sdr/SWAA2021081842584.md): Pad · cracked · Apr 15, 2020 · N798SW · Boeing 7377AD · Cargo/Baggage Doors
  > AFT CARGO DOOR STOP FITTING PAD CRACKED; AFT SIDE 2ND FROM BOTTOM / REMOVED AND REPLACED AFT CARGO DOOR STOP FITTING PAD AFT SIDE 2ND FROM BOTTOM IAW AMM 52-31-01
- [SDR SWAA2021080539584](https://openairdocs.org/sdr/SWAA2021080539584.md): Nut Plate · broken · Apr 9, 2020 · N798SW · Boeing 7377AD · Fuselage Main, Attach Fittings
  > BROKEN FLOOR PANEL NUT PLATE AT BS360 RBL25 WL208. / REMOVED FLOOR PANEL NUT PLATE; BS 360; RBL 25; WL 208; REPLACED WITH NEW PER AMM 53-21-00-400-801
- [SDR SWAA2021082035272](https://openairdocs.org/sdr/SWAA2021082035272.md): Splice · corroded · Mar 30, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CARGO BAY FLOOR PNL SPLICE TEE IS CRACKED BS 727D WL 156 RBL10 / NO ALLOWABLE DAMAGE GIVEN FOR SPLICE STRIP ASSY IN AFT CARGO BAY AT BS 727D; WL 156; RBL 10 PER SRM 53-00-53-1A-2; REPAIR BY REPLACEMENT PER SRM 51-10-02-0G-0. RECEIVED A NEW SPLICE STRIP ASS
- [SDR SWAA2021062435273](https://openairdocs.org/sdr/SWAA2021062435273.md): Scuff Plate · cracked · Mar 30, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > AFT CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED AND INSTALLED SCUFF PLATE ACB AFT CORNER IAW EA 1-A53-2076 R11
- [SDR SWAA2020041335271](https://openairdocs.org/sdr/SWAA2020041335271.md): Stud · damaged · Mar 28, 2020 · N798SW · Boeing 7377AD · Fuselage Main, Structure
  > RH EMERGENCY DOOR EXIT CUT OUT FWD MID AND LOWER STUD COMMON TO SURROUND PANEL INSTALL DAMAGED / REMOVED AND REPLACED RH EMERGENCY DOOR EXIT CUT OUT FWD MID AND LOWER STUDS IAW SOPM 20-50-01. 59908U 28MAR20.
- [SDR SWAA2020041334520](https://openairdocs.org/sdr/SWAA2020041334520.md): Support Angle · cracked · Mar 24, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > APU POWER CABLE SUPPORT ANGLE CRACKED BS 867 BETWEEN STR 2 AND 3 R/H. / REMOVED AND REPLACED APU POWER CABLE SUPPORT ANGLE BS 867 BETWEEN STR 2-3 R/H PER SRM 51-40-02; MM 25-80-00 AND DWG# 146A7901 REV A
- [SDR SWAA2020041326642](https://openairdocs.org/sdr/SWAA2020041326642.md): Floor Panel · damaged · Mar 12, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > CABIN FLOOR PANEL 222AF HAS UPPER SURFACE FIBER DAMAGE. / UPPER SURFACE FIBER DAMAGE TO CABIN FLOOR PANEL 222AF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1; AND SRM 53-00-50-2R-4. 59198U 3.20.20.
- [SDR SWAA2020032442781](https://openairdocs.org/sdr/SWAA2020032442781.md): Strap · cracked · Mar 9, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > INTERCOSTAL STRAP IS CRACKED AT BS 302 STR 4L REMOVED AND REPLACMENT INTERCOSTAL. STRAP. FROM STR 4L AT B.S. 300-318 IAW. SRM. 51-40-05- AND SRM 51-40-02-0G-0 AND DWG NO: 141A0742 ID: 0004 REV:- & DWG NO: 141A8130 ID: 0008 REV: B 59826U MAR.10.2020
- [SDR SWAA2020041326633](https://openairdocs.org/sdr/SWAA2020041326633.md): Web · damaged · Mar 6, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > INSTALLED REPAIR AT BS 336; STRINGER 5R; FASTENERS DO NOT MEET SRM CRITERIA FOR SPACING AND PROPER INSTALLATION. / REMOVED AND REPLACED WEB ASSY AT BS 328-344 R/H STR 5R IAW SRM CH 51-40-02 AND DRAWING # 141A8330.
- [SDR SWAA2020032442780](https://openairdocs.org/sdr/SWAA2020032442780.md): Gusset · cracked · Mar 6, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > FCB GUSSET CRACKED BS 500D STR 19R WL 195 FCB GUSSET AT BS 500D STR 19R REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 143A7902.
- [SDR SWAA2020032442779](https://openairdocs.org/sdr/SWAA2020032442779.md): Gusset · cracked · Mar 6, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > FCB GUSSET CRACKED BS 500D STR 19L WL 195 FCB GUSSET AT BS 500D STR 19L REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR SWAA2020041326594](https://openairdocs.org/sdr/SWAA2020041326594.md): Floor Panel · damaged · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > DAMAGE TO UPPER SURFACE OF FLOOR PANEL 231YF. / DUE TO EXTENT OF DAMAGE; OPTED TO FABRICATE NEW PANEL PER SRM 53-00-50-2R-0 PARA 1A USING BMS 4-23 TY2 LOT# 1399953-1 FLOORBOARD MATERIAL. INSTALLED ALL THRU INSERTS USING BMS5-107 CLASS 1 LOT# AK9FP3008K ADHESIV
- [SDR SWAA2020041326596](https://openairdocs.org/sdr/SWAA2020041326596.md): Floor Panel · damaged · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > DAMAGE TO UPPER SURFACE OF FLOOR PANEL 241BF. / FLOOR PANEL 241BF WITH DAMAGE TO UPPER SURFACE HAS BEEN REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A. (1). 59812U 03/06/2020
- [SDR SWAA2020032442742](https://openairdocs.org/sdr/SWAA2020032442742.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, 727D+5, RBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL, B/S 727D+5 RBL 8 WL 156 IAW SRM 51-40-02-0G-0, PARAGRAPH 7D AND SRM 53-00-53-2R-2, REPAIR 2, ALTERNATIVE 5. 59900U 12MAR20
- [SDR SWAA2020032442741](https://openairdocs.org/sdr/SWAA2020032442741.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727D+5, RBL 3 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL, B/S 727D+5 RBL 3 WL 156 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5 59900U 11MAR20
- [SDR SWAA2020032442740](https://openairdocs.org/sdr/SWAA2020032442740.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727D+5, LBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED ACB FLOOR RAIL B/S 727D+5 LBL 8 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2- REPAIR 2. 59900U 12MAR20.
- [SDR SWAA2020032442739](https://openairdocs.org/sdr/SWAA2020032442739.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727D+5, LBL 12.5 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL B/S 727D+5 LBL 12.5 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2, REPAIR 2, ALTERNATIVE 5. 59900U 12MAR20
- [SDR SWAA2020032442801](https://openairdocs.org/sdr/SWAA2020032442801.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, RBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL, B/S 767+5, RBL 8 AND WL 156 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 4.
- [SDR SWAA2020032442800](https://openairdocs.org/sdr/SWAA2020032442800.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, RBL 3 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL B/S 767+5 RBL 3 WL 156 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5 59900U 11MAR20
- [SDR SWAA2020032442778](https://openairdocs.org/sdr/SWAA2020032442778.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 727+8 AND 727B, LBL 3, WL 156 (MARKED) REPAIRED FLOOR RAIL, B/S 727 TO B/S 727C+6" LBL 3 WL 156 IAW SRM 53-00-53-2R-2. REPAIR 2 ALTERNATIVE 1 AND DWG 146A7500 REV: B 59900U 17MAR20
- [SDR SWAA2020032442777](https://openairdocs.org/sdr/SWAA2020032442777.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** MULTIPLE POINTS OF CORROSION ON ACB FLOOR RAIL UPPER, LOWER SURFACES, BS 727+8 TO 727C, RBL 3, WL 156 REPAIRED FLOOR RAIL, B/S 727 TO B/S 727B+16" RBL 3 WL 156 IAW SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 1 AND DWG 146A7500 REV: B 5990
- [SDR SWAA2020032442744](https://openairdocs.org/sdr/SWAA2020032442744.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, LBL 3 (AT STRAP ATTACH POINT) WL 156 REPAIRED FLOOR RAIL ON ACB B/S 767+5" LBL 3 IAW SRM 51-40-02 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5. 59900U 11MAR20
- [SDR SWAA2020032442743](https://openairdocs.org/sdr/SWAA2020032442743.md): Seat Track · corroded · Mar 5, 2020 · N798SW · Boeing 7377AD · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** CORROSION ON ACB FLOOR RAIL, BS 767+5, LBL 8 (AT STRAP ATTACH POINT) WL 156 REPAIRED ACB FLOOR RAIL, B/S 767+5 LBL 8 IAW SRM 51-40-02-0G-0 PARAGRAPH 7D AND SRM 53-00-53-2R-2 REPAIR 2 ALTERNATIVE 5. 59900U 11MAR20.
- [SDR SWAA2020041326537](https://openairdocs.org/sdr/SWAA2020041326537.md): Floor Panel · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241ABF HAS DAMAGED INSERTS / REPLACED ALL DAMAGED INSERTS; & REPAIRED DAMAGE TO PANEL IAW SRM 53-00-50-2R-1 & SRM 53-00-50-2R-6. 57885U 03-23-2020
- [SDR SWAA2020041326536](https://openairdocs.org/sdr/SWAA2020041326536.md): Floor Panel · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 242UF HAS DAMAGED INSERTS / REPLACED DAMAGED INSERTS & REPAIRED ALL DAMAGE TO FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1 & SRM 53-00-50-2R-6. 57885U; 03-25-2020.
- [SDR SWAA2020041326549](https://openairdocs.org/sdr/SWAA2020041326549.md): Splice · cracked · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Main, Bulkhead
  > DURING COMPLETION OF CCN: 14539 FOUND BS 1016 BULKHEAD S-23L WEB SPLICE TO BE CRACKED ON AFT SIDE FROM EDGE TERMINATING AT FASTENER NEAREST APEX IN OTBD ROW; AREA MARKED. ENGINEERING DISPOSITION REQUIRED. / CUT OUT DAMAGED SECTION OF 1016 BULKHEAD STR 23L AND
- [SDR SWAA2020041326532](https://openairdocs.org/sdr/SWAA2020041326532.md): Threshold · corroded · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AED THRESHOLD WEB UPON MOPSILL REMOVAL AT BS 983 LBL45 WL 208 / AED THRESHOLD WEB AT BS 983 LBL 45 FOUND TO BE OUT OF LIMITS AT BS 984 RBL 46 2' X 2' X.012' ORIGINAL THICKNESS.071' REMAINING.059' PER SRM 53-70-15-1A-1. REPLACED THRESHOLD
- [SDR SWAA2020041326533](https://openairdocs.org/sdr/SWAA2020041326533.md): Web · canning · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > FLOOR WEB AT BS 986-1016 LBL 38 IS OIL CANNED. / REMOVED AND REPLACED FLOOR WEB AT BS 986-1016 LBL 38 PER SRM 51-40-02; SRM 51-04-05; DWG 147A0004; AND DWG 147A5600.
- [SDR SWAA2020041326539](https://openairdocs.org/sdr/SWAA2020041326539.md): Floor Panel · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241ACF HAS DAMAGED INSERTS / REPLACED DAMAGED INSERTS AND FIXED ADDITIONAL DAMAGE TO AFT CABIN FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-4; AND SRM 53-00-50-2R-6. 59198U 3.20.20.
- [SDR SWAA2020041326538](https://openairdocs.org/sdr/SWAA2020041326538.md): Floor Panel · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241ADF HAS DAMAGED INSERTS / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL; FABRICATED NEW PANEL IAW SRM 53-00-50-2R-0 PARA 1A NOTE & BFG DWG 2000-048-2. 57885U 03-26-2020
- [SDR SWAA2020041326541](https://openairdocs.org/sdr/SWAA2020041326541.md): Floor Panel · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE SKIN PLIES / DUE TO THE EXTENT OF DAMAGE TO FLOOR PANEL 241AAF; OPTED TO FABRICATE A NEW FLOOR PANEL USING BMS4-17 TYV1 LOT#1420733-1 IAW SRM 53-00-50-2R-0 PARA 1A 'NOTE' & DWG 147A5810-8-M. INSTALLED INSE
- [SDR SWAA2020032442796](https://openairdocs.org/sdr/SWAA2020032442796.md): Intercostal · corroded · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR INTERCOASTAL AT BS 989 RBL 38. WL 208 REMOVED CORROSION ON FLOOR INTERCOSTAL B.S 989 RBL 38 WL 208 2" X 1.5" X.015"D REMAINING THICKNESS 065", ORIGINAL THICKNESS.080" FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 PAR 4A(2) FIG
- [SDR SWAA2020032442795](https://openairdocs.org/sdr/SWAA2020032442795.md): Web · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > FLOOR WEB AT BS 986-1016 RBL 38 IS CREASED. WL 208 REMOVED AND REPLACED FLOOR WEB AT B.S 986-1016 RBL 38 PER SRM 51-40-02-0G-0, DWG 147A0000, REV A.
- [SDR SWAA2020032442738](https://openairdocs.org/sdr/SWAA2020032442738.md): Intercostal · cracked · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Miscellaneous Structure
  > DURING DTIP INSPECTION, FOUND INTERCOSTAL WEB AT BS 303, STRINGER 4L CRACKED. REMOVED. AND. REPLACMENT. INTERCOSTAL. WEB. AT B.S 303. STR.4L. PART NO: 7530155 IAW. SRM. 51-40-05. AND SRM 51-40-02-0G 0 AND DWG. 141A8130 ID: 0001 REV: - & DWG NO: 141A074
- [SDR SWAA2020032442737](https://openairdocs.org/sdr/SWAA2020032442737.md): Floor Panel · damaged · Mar 3, 2020 · N798SW · Boeing 7377AD · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241ZF HAS DAMAGED UPPER SURFACE SKIN PLIES AFT EDGE UPPER SURFACE SKIN DAMAGE ON FLOOR PANEL 241ZF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1, SRM 53-00-50-2R-4 AND DWG 200-048. 59198U 3.10.20.
- [SDR SWAA2020030942265](https://openairdocs.org/sdr/SWAA2020030942265.md): Stiffener · cracked · Mar 3, 2020 · N798SW · Boeing 7377AD · Horizontal Stabilizer Miscellaneous Structure
  > (SKYLINE DTIP) L/H HORIZ. STAB. CRACK ON THIRD STIFFENER, LWR. I/B SIDE STA. 92.70. CUTOUT DAMAGE AREA. DIM: (1.300" X.175") AT L/H HORIZ STAB THIRD STIFFENER STA 92.70 FABRICATED, LOCATED, DRILLED & INSTALLED T-ANGLE, ANGLE, SHIM IAW B737 SRM SRM 55-10-09. (
- [SDR SWAA2020030942264](https://openairdocs.org/sdr/SWAA2020030942264.md): Stiffener · cracked · Mar 3, 2020 · N798SW · Boeing 7377AD · Horizontal Stabilizer Miscellaneous Structure
  > (SKYLINE DTIP) L/H HORIZ. STAB. CRACK ON SECOND STIFFENER, LWR I/B SIDE STA. 92.70. CUTOUT DAMAGE AREA. DIM: (1.630" X.175") AT L/H HORIZ STAB ON SECOND STIFFENER STA 92.70. RABRICATED LOCATED, DRILLED & INSTALLED T-ANGLE, ANGLE, SHIM. IAW B737 SRM 55-10-09.
- [SDR SWAA2020030942263](https://openairdocs.org/sdr/SWAA2020030942263.md): Stiffener · cracked · Mar 3, 2020 · N798SW · Boeing 7377AD · Horizontal Stabilizer Miscellaneous Structure
  > (SKYLINE DTIP) L/H HORIZ. STAB. CRACK AT FIRST STIFFENER, LWR. I/B SIDE STA. 92.70. CUTOUT DAMAGE AREA. DIM: (1.650" X.175") AT L/H HORIZ STAB FIRT STIFFENER. STA 92.70. REPAIR INSTALLED IAW B737 SRM 55-10-09. (Y000421) NO FURTHER EVALUATION IS NECESSA

Next page: https://openairdocs.org/model/boeing-737-7ad/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 aircraft_model_key = '7377AD'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-7ad/reports

---
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